├── a ├── avx.dat ├── avx-nitro.dat ├── azavempt.dat ├── azavextt.dat ├── azavmoyt.dat ├── az2007_ext.dat ├── ah6407.dat └── ah7476.dat ├── h ├── hm50.dat ├── hm51.dat ├── hm50t.dat ├── hn003.dat ├── hn032.dat ├── hn033.dat ├── hn034.dat ├── hn035.dat ├── hn036.dat ├── hn038.dat ├── hn1004.dat ├── hn1015.dat ├── hn1023.dat ├── hn1027.dat ├── hn1029.dat ├── hn1032.dat ├── hn1033.dat ├── hn1036.dat ├── hn1038.dat ├── hn1051.dat ├── hn1054.dat ├── hn1069.dat ├── hn1070.dat ├── hn1091.dat ├── hn153s.dat ├── hn163.dat ├── hn184.dat ├── hn184m.dat ├── hn188.dat ├── hn203.dat ├── hn211.dat ├── hn216.dat ├── hn217.dat ├── hn227.dat ├── hn239.dat ├── hn274s.dat ├── hn275s.dat ├── hn304.dat ├── hn309.dat ├── hn30s.dat ├── hn311s.dat ├── hn312s.dat ├── hn315s.dat ├── hn316s.dat ├── hn319.dat ├── hn321.dat ├── hn326.dat ├── hn327.dat ├── hn333.dat ├── hn33s.dat ├── hn350.dat ├── hn352.dat ├── hn354.dat ├── hn354a.dat ├── hn354e.dat ├── hn360.dat ├── hn374.dat ├── hn380.dat ├── hn409.dat ├── hn411.dat ├── hn417.dat ├── hn418.dat ├── hn419.dat ├── hn424.dat ├── hn436.dat ├── hn446.dat ├── hn450.dat ├── hn450s.dat ├── hn452.dat ├── hn456.dat ├── hn462.dat ├── hn464.dat ├── hn465.dat ├── hn470.dat ├── hn470s.dat ├── hn474.dat ├── hn475.dat ├── hn477s.dat ├── hn478s.dat ├── hn480.dat ├── hn483.dat ├── hn484.dat ├── hn487.dat ├── hn507.dat ├── hn707.dat ├── hn785.dat ├── hn801.dat ├── hn802.dat ├── hn803.dat ├── hn805.dat ├── hn808.dat ├── hn832.dat ├── hn838.dat ├── hn839d.dat ├── hn840s.dat ├── hn951.dat ├── hn955.dat ├── hn956.dat ├── hn959.dat ├── hn968s.dat ├── hn969.dat ├── hn971.dat ├── hn972.dat ├── hn973.dat ├── hn974.dat ├── hn975.dat ├── hn976s.dat ├── hn978.dat ├── hn979.dat ├── hn979d.dat ├── hn980.dat ├── hn981.dat ├── hn984.dat ├── hn987.dat ├── hn989.dat ├── hn990.dat ├── hn997a.dat ├── hn997b.dat ├── hn998.dat ├── hn999.dat ├── hs179.dat ├── hs2080.dat ├── hs3080.dat ├── hs3090.dat ├── hs3512.dat ├── hs510.dat ├── hs520.dat ├── hs522.dat ├── hs602.dat ├── hn1033a.dat ├── hn1069a.dat ├── hn1069b.dat ├── hn1069c.dat ├── hn1091a.dat ├── hn1091b.dat ├── hn163ta.dat ├── hn163tb.dat ├── hn216ta.dat ├── hn276sa.dat ├── hn304ta.dat ├── hn350m01.dat ├── hn350m02.dat ├── hn354es.dat ├── hn354oc.dat ├── hn354sm.dat ├── hn354sr.dat ├── hn470jt.dat ├── hn785sr.dat ├── hn832ta.dat ├── hn961sa.dat ├── hn975ta.dat ├── hs3412b.dat ├── htropfen.dat ├── handselrev.dat ├── hobie.dat └── horten.dat ├── m ├── mg05.dat ├── mg06.dat ├── mh16.dat ├── mh17.dat ├── mh28.dat ├── mh31.dat ├── mh34.dat ├── mh50.dat ├── mh51.dat ├── mh52.dat ├── mh53.dat ├── mh54.dat ├── mh18b.dat ├── mve8516f3.dat ├── mjp711f3rev.dat ├── mvr22_3-10.dat ├── mg05na09_210.dat ├── m7.dat ├── m6.dat ├── marske1.dat ├── marske5.dat ├── marske2.dat ├── marske3.dat └── marske4.dat ├── r ├── rk40.dat ├── ritz33012.dat ├── ritz33015.dat ├── rz10.00-225-235.dat ├── raf32.dat ├── raf38.dat ├── raf6.dat ├── raf69.dat ├── raf89.dat ├── r13010.dat ├── raf30md.dat ├── raf32md.dat ├── r23012.dat ├── rhodesg30.dat ├── rhodesg32.dat ├── rhodesg34.dat ├── rhodesg36.dat ├── raf15.dat ├── raf30.dat ├── raf48.dat ├── raf32mdrev.dat └── r13012.dat ├── t ├── tp42.dat ├── tt54.dat ├── tp28-0.dat ├── tp28-4.dat ├── tp28-l.dat ├── tp29-5.dat ├── tp29-6.dat ├── tp29-7.dat ├── tp29-8.dat ├── tp29-9.dat ├── tp96-1.dat ├── tp202-10.dat ├── tp202-9.dat ├── tp28-60.dat ├── tp96-05.dat ├── tp96-075.dat ├── tp96-125.dat ├── tp73-60inch.dat ├── tp36-95-tp29-85.dat └── tpr-95-96-95_sb96vs.dat ├── e ├── e193gu.dat ├── eb380.dat ├── e49.dat ├── ea61009.dat ├── ea61012.dat ├── ea81006.dat ├── eiffel10.dat ├── ebambino7.dat ├── eiffel371.dat ├── eiffel385.dat ├── eiffel428.dat ├── eiffel430.dat └── ec863914.dat ├── f ├── fad04.dat ├── fad16.dat ├── fad17.dat ├── fad21.dat ├── fad24.dat ├── fx057816.dat ├── fx082512.dat ├── fx049915.dat ├── fg1.dat ├── fg2.dat ├── fg3.dat └── fg4.dat ├── n ├── nn1817.dat ├── n64212rb.dat ├── naca6409.dat ├── nasa_gw_1.dat ├── nm02f3f.dat ├── nm41-3f3j.dat ├── nm41f3j.dat ├── naca63a612.dat ├── nm-retro-13.dat ├── nm-retro-14.dat ├── nm-retro-saumon-30.dat ├── nm-retro-saumon-50.dat ├── nm-spatz-saumon-30.dat ├── nm-spatz-saumon-50.dat ├── nm-retro-16-emplanture.dat ├── n10.dat ├── n11.dat ├── n22.dat ├── n24.dat ├── n9.dat ├── nacacyh.dat ├── nacam18.dat ├── n12.dat ├── n13.dat ├── n14.dat ├── nacam12rev.dat ├── nacam12.dat ├── nacam2.dat ├── nacam3.dat ├── naca000834.dat ├── naca001034.dat ├── naca001035.dat ├── naca001064.dat ├── naca001065.dat ├── naca001066.dat ├── naca001234.dat ├── naca001264.dat ├── naca16006.dat ├── naca16012.dat ├── naca16015.dat ├── naca16018.dat ├── naca16021.dat ├── nacam6.dat ├── naca2412.dat ├── naca2415.dat ├── naca2418.dat ├── naca2421.dat ├── naca4412.dat ├── naca4418.dat └── naca4421.dat ├── p ├── pegase.dat ├── phn1051.dat └── prisenaca.dat ├── b ├── borge-b3.dat ├── b707c.dat ├── b707d.dat ├── b707b.dat ├── bambino6.dat └── b707brev.dat ├── c ├── cristal.dat ├── clarkyhrev.dat ├── clarkk.dat ├── clarkyh.dat ├── coanda1.dat ├── coanda2.dat ├── coanda3.dat ├── cj3209.dat ├── curtisc72.dat ├── cootie.dat ├── clarkv.dat ├── clarkw.dat ├── clarkx.dat └── clarkz.dat ├── s ├── s4083rev.dat ├── salaz_moy.dat ├── sb95_95_2.dat ├── sb96_lm.dat ├── sb96_mu.dat ├── sb97_fw.dat ├── sb98vm5.dat ├── sb98vr5.dat ├── sb98vs5.dat ├── sb99a22c0.dat ├── sb99a22c4.dat ├── sb99f3j.dat ├── strom98.dat ├── sb95_105_2.dat ├── sb95_115_2.dat ├── sb96_105_3.dat ├── sb96_116_3.dat ├── sb96_127_3.dat ├── sb96d_13_3.dat ├── sb97_8_125.dat ├── schoon2_915.dat ├── schoon2_930.dat ├── saratov.dat ├── strand.dat ├── stcyr234.dat ├── stcyr24.dat ├── stcyr171.dat ├── stcyr172.dat └── stcyr171rev.dat ├── u ├── usa35arev.dat └── usa98.dat ├── d ├── dp189-7831.dat ├── dormoy.dat ├── dga1138.dat ├── daytonwright6.dat ├── daytonwrightt1.dat ├── dga1182.dat └── davis.dat ├── j └── jedelskyej85rev.dat ├── g ├── goe477.dat ├── goe480.dat ├── goe507.dat ├── goe517.dat ├── goe584.dat ├── goe358.dat ├── goe797.dat ├── goe300.dat ├── goe09k.dat ├── goe10k.dat ├── goe11k.dat ├── goe12k.dat ├── goe13k.dat ├── goe14k.dat ├── goe15k.dat ├── goe16k.dat ├── goe405.dat ├── goe439.dat ├── goe443.dat ├── goe496.dat ├── goe670.dat ├── goe682.dat ├── goe610bm.dat ├── glennmartin2.dat ├── glennmartin3.dat ├── glennmartin4.dat ├── goe05k.dat ├── goe06k.dat ├── goe07k.dat ├── goe08k.dat ├── goe101.dat ├── goe113.dat ├── goe342.dat ├── goe411.dat ├── goe484.dat ├── goe488.dat ├── goe533.dat ├── goe565.dat ├── goe611.dat ├── goe711.dat ├── goe770.dat ├── goe798.dat ├── goe610b.dat ├── goe804.dat ├── gs1.dat ├── goe229rev.dat ├── goe417a.dat ├── goe123.dat ├── goe14.dat ├── goe15.dat ├── goe177.dat ├── goe178.dat ├── goe195.dat ├── goe257.dat ├── goe264.dat ├── goe265.dat ├── goe269.dat ├── goe284.dat ├── goe286.dat ├── goe287.dat ├── goe288.dat └── goe298.dat ├── i ├── isa571.dat ├── isa960.dat ├── isa961.dat └── isa962.dat ├── z ├── zagi08.dat ├── zagi10.dat └── zagi12.dat └── 0-9 └── 2032c.dat /a/avx.dat: 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0.370590 0.132260 10 | 0.250000 0.118870 11 | 0.146450 0.094790 12 | 0.066990 0.062900 13 | 0.017040 0.029790 14 | 0.000000 0.000000 15 | 0.017040 -0.013530 16 | 0.066990 -0.021280 17 | 0.146450 -0.026730 18 | 0.250000 -0.030190 19 | 0.370590 -0.029580 20 | 0.500000 -0.029060 21 | 0.629410 -0.027280 22 | 0.750000 -0.019190 23 | 0.853560 -0.005420 24 | 0.933020 0.001210 25 | 0.982970 0.001360 26 | 1.000000 0.000000 27 | -------------------------------------------------------------------------------- /e/e49.dat: -------------------------------------------------------------------------------- 1 | EPPLER 49 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9966400 0.0016100 4 | 0.9873600 0.0066800 5 | 0.9378100 0.0375600 6 | 0.8905500 0.0593500 7 | 0.6676800 0.1042800 8 | 0.6220800 0.1086800 9 | 0.3843200 0.1143100 10 | 0.2934500 0.1088000 11 | 0.1385800 0.0863300 12 | 0.0573200 0.0616200 13 | 0.0377900 0.0525200 14 | 0.0106500 0.0350900 15 | 0.0032500 0.0275500 16 | 0.0002000 0.0216700 17 | 0.0023000 0.0183600 18 | 0.0110000 0.0167400 19 | 0.3336100 0.0399300 20 | 0.3901600 0.0422400 21 | 0.4483800 0.0437000 22 | 0.7861900 0.0330400 23 | 0.9856000 0.0039800 24 | 0.9963900 0.0010800 25 | 1.0000000 0.0000000 26 | -------------------------------------------------------------------------------- /f/fx082512.dat: -------------------------------------------------------------------------------- 1 | WORTMANN FX 082-512 AIRFOIL 2 | 1.000000 0.000000 3 | 0.982970 0.009150 4 | 0.933020 0.024840 5 | 0.853560 0.042850 6 | 0.750000 0.060120 7 | 0.629410 0.072920 8 | 0.500000 0.079190 9 | 0.370590 0.077630 10 | 0.250000 0.069340 11 | 0.146450 0.054400 12 | 0.066990 0.035590 13 | 0.017040 0.018340 14 | 0.000000 0.000000 15 | 0.017040 -0.018020 16 | 0.066990 -0.033030 17 | 0.146450 -0.046340 18 | 0.250000 -0.048660 19 | 0.370590 -0.028110 20 | 0.500000 -0.005910 21 | 0.629410 0.010200 22 | 0.750000 0.018980 23 | 0.853560 0.019690 24 | 0.933020 0.013900 25 | 0.982970 0.005170 26 | 1.000000 0.000000 27 | -------------------------------------------------------------------------------- /f/fx049915.dat: -------------------------------------------------------------------------------- 1 | WORTMANN FX 049-915 AIRFOIL 2 | 1.000000 0.000000 3 | 0.982970 0.004690 4 | 0.933020 0.014010 5 | 0.853560 0.027510 6 | 0.750000 0.048700 7 | 0.629410 0.075190 8 | 0.500000 0.105870 9 | 0.370590 0.131780 10 | 0.250000 0.127320 11 | 0.146450 0.102880 12 | 0.066990 0.068620 13 | 0.017040 0.031870 14 | 0.000000 0.000000 15 | 0.017040 -0.010550 16 | 0.066990 -0.014360 17 | 0.146450 -0.015300 18 | 0.250000 -0.015900 19 | 0.370590 -0.015400 20 | 0.500000 -0.014190 21 | 0.629410 -0.012010 22 | 0.750000 -0.009420 23 | 0.853560 -0.007010 24 | 0.933020 -0.004270 25 | 0.982970 -0.001930 26 | 1.000000 0.000000 27 | -------------------------------------------------------------------------------- /r/raf32.dat: -------------------------------------------------------------------------------- 1 | RAF 32 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0315000 4 | 0.8000000 0.0578000 5 | 0.7000000 0.0799000 6 | 0.6000000 0.0962000 7 | 0.5000000 0.1069000 8 | 0.4000000 0.1100000 9 | 0.3000000 0.1055000 10 | 0.2000000 0.0916000 11 | 0.1000000 0.0663000 12 | 0.0500000 0.0458500 13 | 0.0250000 0.0318200 14 | 0.0000000 0.0000000 15 | 0.0250000 -.0183700 16 | 0.0500000 -.0237500 17 | 0.1000000 -.0279000 18 | 0.2000000 -.0276000 19 | 0.3000000 -.0213000 20 | 0.4000000 -.0140000 21 | 0.5000000 -.0067000 22 | 0.6000000 0.0002000 23 | 0.7000000 0.0049000 24 | 0.8000000 0.0068000 25 | 0.9000000 0.0047000 26 | 1.0000000 0.0000000 27 | -------------------------------------------------------------------------------- /r/raf38.dat: -------------------------------------------------------------------------------- 1 | RAF 38 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0183000 4 | 0.8000000 0.0354000 5 | 0.7000000 0.0527000 6 | 0.6000000 0.0685000 7 | 0.5000000 0.0806000 8 | 0.4000000 0.0869000 9 | 0.3000000 0.0875000 10 | 0.2000000 0.0791000 11 | 0.1000000 0.0594000 12 | 0.0500000 0.0421000 13 | 0.0250000 0.0298000 14 | 0.0000000 0.0000000 15 | 0.0250000 -.0202000 16 | 0.0500000 -.0266000 17 | 0.1000000 -.0338000 18 | 0.2000000 -.0386000 19 | 0.3000000 -.0390000 20 | 0.4000000 -.0366000 21 | 0.5000000 -.0323000 22 | 0.6000000 -.0273000 23 | 0.7000000 -.0213000 24 | 0.8000000 -.0146000 25 | 0.9000000 -.0079000 26 | 1.0000000 0.0000000 27 | -------------------------------------------------------------------------------- /r/raf6.dat: -------------------------------------------------------------------------------- 1 | RAF 6 AIRFOIL 2 | 1.0000000 0.0015000 3 | 0.8998800 0.0331400 4 | 0.7998101 0.0537800 5 | 0.6997400 0.0714200 6 | 0.5997000 0.0840600 7 | 0.4996700 0.0917000 8 | 0.3996600 0.0953400 9 | 0.2996600 0.0957800 10 | 0.1996700 0.0906200 11 | 0.0997300 0.0742600 12 | 0.0498100 0.0540800 13 | 0.0248700 0.0359900 14 | 0.0000000 0.0000000 15 | 0.0250200 -.0050100 16 | 0.0500200 -.0049200 17 | 0.1000200 -.0047400 18 | 0.2000200 -.0043800 19 | 0.3000100 -.0040200 20 | 0.4000100 -.0036600 21 | 0.5000100 -.0033000 22 | 0.6000100 -.0029400 23 | 0.7000100 -.0025800 24 | 0.8000100 -.0022200 25 | 0.9000100 -.0018600 26 | 1.0000000 -.0015000 27 | -------------------------------------------------------------------------------- /r/raf69.dat: -------------------------------------------------------------------------------- 1 | RAF 69 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0243700 4 | 0.8000000 0.0490400 5 | 0.7000000 0.0724100 6 | 0.6000000 0.0927800 7 | 0.5000000 0.1082500 8 | 0.4000000 0.1171200 9 | 0.3000000 0.1186900 10 | 0.2000000 0.1096600 11 | 0.1000000 0.0849300 12 | 0.0500000 0.0609600 13 | 0.0250000 0.0414800 14 | 0.0000000 0.0000000 15 | 0.0250000 -.0374200 16 | 0.0500000 -.0526400 17 | 0.1000000 -.0705700 18 | 0.2000000 -.0855400 19 | 0.3000000 -.0877100 20 | 0.4000000 -.0831800 21 | 0.5000000 -.0739500 22 | 0.6000000 -.0615200 23 | 0.7000000 -.0464900 24 | 0.8000000 -.0297600 25 | 0.9000000 -.0148300 26 | 1.0000000 0.0000000 27 | -------------------------------------------------------------------------------- /r/raf89.dat: -------------------------------------------------------------------------------- 1 | RAF 89 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0285100 4 | 0.8000000 0.0565200 5 | 0.7000000 0.0840300 6 | 0.6000000 0.1091400 7 | 0.5000000 0.1275500 8 | 0.4000000 0.1375600 9 | 0.3000000 0.1393700 10 | 0.2000000 0.1294800 11 | 0.1000000 0.1003900 12 | 0.0500000 0.0730500 13 | 0.0250000 0.0523200 14 | 0.0000000 0.0000000 15 | 0.0250000 -.0484800 16 | 0.0500000 -.0663500 17 | 0.1000000 -.0878100 18 | 0.2000000 -.1074200 19 | 0.3000000 -.1106300 20 | 0.4000000 -.1054400 21 | 0.5000000 -.0947500 22 | 0.6000000 -.0767600 23 | 0.7000000 -.0582700 24 | 0.8000000 -.0382800 25 | 0.9000000 -.0192900 26 | 1.0000000 0.0000000 27 | -------------------------------------------------------------------------------- /u/usa98.dat: -------------------------------------------------------------------------------- 1 | USA 98 AIRFOIL 2 | 1.0000000 0.0090000 3 | 0.9000000 0.0450000 4 | 0.8000000 0.0690000 5 | 0.7000000 0.0910000 6 | 0.6000000 0.1100000 7 | 0.5000000 0.1230000 8 | 0.4000000 0.1290000 9 | 0.3000000 0.1260000 10 | 0.2000000 0.1120000 11 | 0.1000000 0.0830000 12 | 0.0500000 0.0580000 13 | 0.0250000 0.0410000 14 | 0.0000000 0.0000000 15 | 0.0250000 -.0340000 16 | 0.0500000 -.0375000 17 | 0.1000000 -.0360000 18 | 0.2000000 -.0295000 19 | 0.3000000 -.0170000 20 | 0.4000000 -.0030000 21 | 0.5000000 0.0090000 22 | 0.6000000 0.0160000 23 | 0.7000000 0.0190000 24 | 0.8000000 0.0170000 25 | 0.9000000 0.0090000 26 | 1.0000000 0.0000000 27 | -------------------------------------------------------------------------------- /g/goe477.dat: -------------------------------------------------------------------------------- 1 | GOE 477 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0233500 4 | 0.8000000 0.0457000 5 | 0.7000000 0.0690500 6 | 0.6000000 0.0849000 7 | 0.5000000 0.0942500 8 | 0.4000000 0.0975000 9 | 0.3000000 0.0969500 10 | 0.2000000 0.0898000 11 | 0.1000000 0.0681500 12 | 0.0500000 0.0443200 13 | 0.0250000 0.0289100 14 | 0.0000000 0.0000000 15 | 0.0250000 -.0130900 16 | 0.0500000 -.0151800 17 | 0.1000000 -.0143500 18 | 0.2000000 -.0087000 19 | 0.3000000 -.0035500 20 | 0.4000000 0.0001000 21 | 0.5000000 0.0022500 22 | 0.6000000 0.0034000 23 | 0.7000000 0.0030500 24 | 0.8000000 0.0022000 25 | 0.9000000 0.0013500 26 | 1.0000000 0.0000000 27 | -------------------------------------------------------------------------------- /g/goe480.dat: -------------------------------------------------------------------------------- 1 | GOE 480 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0259500 4 | 0.8000000 0.0494000 5 | 0.7000000 0.0708500 6 | 0.6000000 0.0898000 7 | 0.5000000 0.1032500 8 | 0.4000000 0.1107000 9 | 0.3000000 0.1106500 10 | 0.2000000 0.1006000 11 | 0.1000000 0.0750500 12 | 0.0500000 0.0522700 13 | 0.0250000 0.0366400 14 | 0.0000000 0.0000000 15 | 0.0250000 -.0218600 16 | 0.0500000 -.0237200 17 | 0.1000000 -.0219500 18 | 0.2000000 -.0134000 19 | 0.3000000 -.0068500 20 | 0.4000000 -.0008000 21 | 0.5000000 0.0027500 22 | 0.6000000 0.0048000 23 | 0.7000000 0.0048500 24 | 0.8000000 0.0034000 25 | 0.9000000 0.0014500 26 | 1.0000000 0.0000000 27 | -------------------------------------------------------------------------------- /g/goe507.dat: -------------------------------------------------------------------------------- 1 | GOE 507 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0169500 4 | 0.8000000 0.0339000 5 | 0.7000000 0.0488500 6 | 0.6000000 0.0603000 7 | 0.5000000 0.0672500 8 | 0.4000000 0.0712000 9 | 0.3000000 0.0706500 10 | 0.2000000 0.0641000 11 | 0.1000000 0.0480500 12 | 0.0500000 0.0337800 13 | 0.0250000 0.0241400 14 | 0.0000000 0.0000000 15 | 0.0250000 -.0178600 16 | 0.0500000 -.0212200 17 | 0.1000000 -.0234500 18 | 0.2000000 -.0199000 19 | 0.3000000 -.0158500 20 | 0.4000000 -.0128000 21 | 0.5000000 -.0102500 22 | 0.6000000 -.0087000 23 | 0.7000000 -.0071500 24 | 0.8000000 -.0056000 25 | 0.9000000 -.0030500 26 | 1.0000000 0.0000000 27 | -------------------------------------------------------------------------------- /g/goe517.dat: -------------------------------------------------------------------------------- 1 | GOE 517 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0197500 4 | 0.8000000 0.0370000 5 | 0.7000000 0.0532500 6 | 0.6000000 0.0660000 7 | 0.5000000 0.0747500 8 | 0.4000000 0.0810000 9 | 0.3000000 0.0807500 10 | 0.2000000 0.0745000 11 | 0.1000000 0.0552500 12 | 0.0500000 0.0373700 13 | 0.0250000 0.0246900 14 | 0.0000000 0.0000000 15 | 0.0250000 -.0068100 16 | 0.0500000 -.0071200 17 | 0.1000000 -.0027500 18 | 0.2000000 0.0060000 19 | 0.3000000 0.0107500 20 | 0.4000000 0.0120000 21 | 0.5000000 0.0112500 22 | 0.6000000 0.0090000 23 | 0.7000000 0.0052500 24 | 0.8000000 0.0030000 25 | 0.9000000 0.0007500 26 | 1.0000000 0.0000000 27 | -------------------------------------------------------------------------------- /g/goe584.dat: -------------------------------------------------------------------------------- 1 | GOE 584 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0237500 4 | 0.8000000 0.0465000 5 | 0.7000000 0.0687500 6 | 0.6000000 0.0880000 7 | 0.5000000 0.1027500 8 | 0.4000000 0.1110000 9 | 0.3000000 0.1107500 10 | 0.2000000 0.1010000 11 | 0.1000000 0.0767500 12 | 0.0500000 0.0548800 13 | 0.0250000 0.0371900 14 | 0.0000000 0.0000000 15 | 0.0250000 -.0198100 16 | 0.0500000 -.0236200 17 | 0.1000000 -.0247500 18 | 0.2000000 -.0210000 19 | 0.3000000 -.0162500 20 | 0.4000000 -.0120000 21 | 0.5000000 -.0092500 22 | 0.6000000 -.0065000 23 | 0.7000000 -.0042500 24 | 0.8000000 -.0025000 25 | 0.9000000 -.0012500 26 | 1.0000000 0.0000000 27 | -------------------------------------------------------------------------------- /b/b707c.dat: -------------------------------------------------------------------------------- 1 | BOEING 707 .40 SPAN AIRFOIL 2 | 1.0000 0.0000 3 | 0.7000 0.0413 4 | 0.6000 0.0512 5 | 0.5000 0.0611 6 | 0.4000 0.0661 7 | 0.3000 0.0661 8 | 0.2500 0.0628 9 | 0.2000 0.0578 10 | 0.1500 0.0545 11 | 0.1000 0.0446 12 | 0.0748 0.0396 13 | 0.0500 0.0330 14 | 0.0249 0.0256 15 | 0.0125 0.0206 16 | 0.0083 0.0165 17 | 0.0050 0.0149 18 | 0.0000 0.0000 19 | 0.0050 -0.0066 20 | 0.0083 -0.0074 21 | 0.0125 -0.0083 22 | 0.0249 -0.0091 23 | 0.0500 -0.0099 24 | 0.0748 -0.0124 25 | 0.1000 -0.0132 26 | 0.1500 -0.0165 27 | 0.2000 -0.0215 28 | 0.2500 -0.0248 29 | 0.3000 -0.0297 30 | 0.4000 -0.0297 31 | 0.5000 -0.0289 32 | 0.6000 -0.0264 33 | 0.7000 -0.0198 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /c/clarkk.dat: -------------------------------------------------------------------------------- 1 | CLARK K AIRFOIL 2 | 1.0000000 0.0006000 3 | 0.8990800 0.0234200 4 | 0.7982800 0.0436500 5 | 0.6976000 0.0609900 6 | 0.5970400 0.0750200 7 | 0.4966600 0.0846700 8 | 0.3964700 0.0896200 9 | 0.2965100 0.0886800 10 | 0.1968300 0.0805500 11 | 0.0976100 0.0606500 12 | 0.0729500 0.0520700 13 | 0.0483700 0.0414100 14 | 0.0239200 0.0273400 15 | 0.0000000 0.0000000 16 | 0.0259500 -.0241800 17 | 0.0510500 -.0265900 18 | 0.0761100 -.0282000 19 | 0.1012200 -.0310100 20 | 0.2012500 -.0317700 21 | 0.3011100 -.0281400 22 | 0.4009500 -.0242000 23 | 0.5008000 -.0202700 24 | 0.6006400 -.0163300 25 | 0.7004901 -.0124000 26 | 0.8003300 -.0084700 27 | 0.9001800 -.0045300 28 | 1.0000000 -.0006000 29 | -------------------------------------------------------------------------------- /g/goe358.dat: -------------------------------------------------------------------------------- 1 | GOE 358 AIRFOIL 2 | 1.0000000 0.0032000 3 | 0.9000000 0.0290500 4 | 0.8000000 0.0499000 5 | 0.7000000 0.0664500 6 | 0.6000000 0.0807000 7 | 0.5000000 0.0907500 8 | 0.4000000 0.0965000 9 | 0.3000000 0.0970500 10 | 0.2000000 0.0891000 11 | 0.1500000 0.0787800 12 | 0.1000000 0.0658500 13 | 0.0500000 0.0460200 14 | 0.0250000 0.0321600 15 | 0.0000000 0.0000000 16 | 0.0250000 -.0176400 17 | 0.0500000 -.0214800 18 | 0.1000000 -.0238500 19 | 0.1500000 -.0225300 20 | 0.2000000 -.0196000 21 | 0.3000000 -.0067500 22 | 0.4000000 0.0100000 23 | 0.5000000 0.0231500 24 | 0.6000000 0.0290000 25 | 0.7000000 0.0289500 26 | 0.8000000 0.0227000 27 | 0.9000000 0.0117500 28 | 1.0000000 0.0000000 29 | -------------------------------------------------------------------------------- /g/goe797.dat: -------------------------------------------------------------------------------- 1 | GOE 797 AIRFOIL 2 | 1.0000000 0.0080000 3 | 0.9000000 0.0392000 4 | 0.8000000 0.0674000 5 | 0.7000000 0.0906000 6 | 0.6000000 0.1104000 7 | 0.5000000 0.1240000 8 | 0.4000000 0.1292000 9 | 0.3000000 0.1264000 10 | 0.2000000 0.1146000 11 | 0.1500000 0.1022000 12 | 0.0500000 0.0604000 13 | 0.0250000 0.0412000 14 | 0.0125000 0.0276000 15 | 0.0000000 0.0000000 16 | 0.0125000 -.0214000 17 | 0.0250000 -.0288000 18 | 0.0500000 -.0360000 19 | 0.1500000 -.0400000 20 | 0.2000000 -.0384000 21 | 0.3000000 -.0336000 22 | 0.4000000 -.0288000 23 | 0.5000000 -.0240000 24 | 0.6000000 -.0192000 25 | 0.7000000 -.0144000 26 | 0.8000000 -.0096000 27 | 0.9000000 -.0048000 28 | 1.0000000 0.0000000 29 | -------------------------------------------------------------------------------- /e/ea61009.dat: -------------------------------------------------------------------------------- 1 | EPPLER EA 6(-1)-009 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0021000 4 | 0.9000000 0.0050000 5 | 0.8000000 0.0145000 6 | 0.7000000 0.0255000 7 | 0.6000000 0.0344000 8 | 0.5000000 0.0408000 9 | 0.4000000 0.0438000 10 | 0.3000000 0.0450000 11 | 0.2000000 0.0420000 12 | 0.1000000 0.0348000 13 | 0.0500000 0.0264000 14 | 0.0100000 0.0136000 15 | 0.0000000 0.0000000 16 | 0.0100000 -.0136000 17 | 0.0500000 -.0264000 18 | 0.1000000 -.0348000 19 | 0.2000000 -.0420000 20 | 0.3000000 -.0450000 21 | 0.4000000 -.0438000 22 | 0.5000000 -.0408000 23 | 0.6000000 -.0344000 24 | 0.7000000 -.0255000 25 | 0.8000000 -.0145000 26 | 0.9000000 -.0050000 27 | 0.9500000 -.0021000 28 | 1.0000000 0.0000000 29 | -------------------------------------------------------------------------------- /e/ea61012.dat: -------------------------------------------------------------------------------- 1 | EPPLER EA 6(-1)-012 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0042000 4 | 0.9000000 0.0086000 5 | 0.8000000 0.0192000 6 | 0.7000000 0.0340000 7 | 0.6000000 0.0468000 8 | 0.5000000 0.0560000 9 | 0.4000000 0.0594000 10 | 0.3000000 0.0600000 11 | 0.2000000 0.0558000 12 | 0.1000000 0.0456000 13 | 0.0500000 0.0360000 14 | 0.0100000 0.0180000 15 | 0.0000000 0.0000000 16 | 0.0100000 -.0180000 17 | 0.0500000 -.0360000 18 | 0.1000000 -.0456000 19 | 0.2000000 -.0558000 20 | 0.3000000 -.0600000 21 | 0.4000000 -.0594000 22 | 0.5000000 -.0560000 23 | 0.6000000 -.0468000 24 | 0.7000000 -.0340000 25 | 0.8000000 -.0192000 26 | 0.9000000 -.0086000 27 | 0.9500000 -.0042000 28 | 1.0000000 0.0000000 29 | -------------------------------------------------------------------------------- /e/ea81006.dat: -------------------------------------------------------------------------------- 1 | EPPLER EA 8(-1)-006 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0036000 4 | 0.9000000 0.0074000 5 | 0.8000000 0.0148000 6 | 0.7000000 0.0212000 7 | 0.6000000 0.0255000 8 | 0.5000000 0.0280000 9 | 0.4000000 0.0298000 10 | 0.3000000 0.0300000 11 | 0.2000000 0.0288000 12 | 0.1000000 0.0238000 13 | 0.0500000 0.0178000 14 | 0.0100000 0.0100000 15 | 0.0000000 0.0000000 16 | 0.0100000 -.0100000 17 | 0.0500000 -.0178000 18 | 0.1000000 -.0238000 19 | 0.2000000 -.0288000 20 | 0.3000000 -.0300000 21 | 0.4000000 -.0298000 22 | 0.5000000 -.0280000 23 | 0.6000000 -.0255000 24 | 0.7000000 -.0212000 25 | 0.8000000 -.0148000 26 | 0.9000000 -.0074000 27 | 0.9500000 -.0036000 28 | 1.0000000 0.0000000 29 | -------------------------------------------------------------------------------- /g/goe300.dat: -------------------------------------------------------------------------------- 1 | GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL 2 | 1.0000000 0.0018000 3 | 0.9000000 0.0256000 4 | 0.8000000 0.0485000 5 | 0.7000000 0.0685000 6 | 0.6000000 0.0854000 7 | 0.5000000 0.0989000 8 | 0.4000000 0.1078000 9 | 0.3000000 0.1090000 10 | 0.2000000 0.1015000 11 | 0.1500000 0.0915000 12 | 0.1000000 0.0784000 13 | 0.0500000 0.0566000 14 | 0.0250000 0.0389500 15 | 0.0000000 0.0000000 16 | 0.0250000 -.0097500 17 | 0.0500000 -.0080000 18 | 0.1000000 0.0030000 19 | 0.1500000 0.0125000 20 | 0.2000000 0.0186000 21 | 0.3000000 0.0247000 22 | 0.4000000 0.0245000 23 | 0.5000000 0.0215000 24 | 0.6000000 0.0173000 25 | 0.7000000 0.0130000 26 | 0.8000000 0.0086000 27 | 0.9000000 0.0040000 28 | 1.0000000 0.0000000 29 | -------------------------------------------------------------------------------- /r/r13010.dat: -------------------------------------------------------------------------------- 1 | RITZ 1-30-10 de profils MRA 2 | 1.00000 0.00000 3 | 0.91890 0.01060 4 | 0.82730 0.02200 5 | 0.68880 0.03680 6 | 0.61940 0.04280 7 | 0.47710 0.05300 8 | 0.40950 0.05700 9 | 0.30040 0.05960 10 | 0.20320 0.05650 11 | 0.15430 0.05220 12 | 0.11210 0.04660 13 | 0.05420 0.03290 14 | 0.02610 0.02340 15 | 0.01330 0.01730 16 | 0.00490 0.01020 17 | 0.00000 0.00000 18 | 0.00490 -0.00740 19 | 0.01330 -0.01290 20 | 0.02610 -0.01830 21 | 0.05420 -0.02420 22 | 0.11210 -0.03150 23 | 0.15430 -0.03460 24 | 0.20320 -0.03750 25 | 0.30040 -0.03970 26 | 0.40950 -0.03780 27 | 0.47710 -0.03500 28 | 0.61940 -0.02830 29 | 0.68880 -0.02360 30 | 0.82730 -0.01390 31 | 0.91890 -0.00690 32 | 1.00000 0.00000 33 | Epaisseur relative 9.93 -------------------------------------------------------------------------------- /c/clarkyh.dat: -------------------------------------------------------------------------------- 1 | CLARK YH AIRFOIL 2 | 1.000000 0.021000 3 | 0.950000 0.028500 4 | 0.900000 0.037000 5 | 0.800000 0.056000 6 | 0.700000 0.075500 7 | 0.600000 0.091000 8 | 0.500000 0.105000 9 | 0.400000 0.114500 10 | 0.300000 0.119000 11 | 0.200000 0.113000 12 | 0.150000 0.108000 13 | 0.100000 0.098000 14 | 0.075000 0.090000 15 | 0.050000 0.081000 16 | 0.025000 0.068000 17 | 0.000000 0.041000 18 | 0.025000 0.018500 19 | 0.050000 0.012000 20 | 0.075000 0.007000 21 | 0.100000 0.004500 22 | 0.150000 0.000000 23 | 0.200000 0.000000 24 | 0.300000 0.000000 25 | 0.400000 0.000000 26 | 0.500000 0.000000 27 | 0.600000 0.000000 28 | 0.700000 0.000000 29 | 0.800000 0.004000 30 | 0.900000 0.010000 31 | 0.950000 0.013700 32 | 1.000000 0.020000 33 | -------------------------------------------------------------------------------- /g/goe09k.dat: -------------------------------------------------------------------------------- 1 | GOE 9K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0053500 4 | 0.9000000 0.0090000 5 | 0.8000000 0.0148000 6 | 0.7000000 0.0187000 7 | 0.6000000 0.0209000 8 | 0.5000000 0.0212000 9 | 0.4000000 0.0205000 10 | 0.3000000 0.0193000 11 | 0.2000000 0.0167000 12 | 0.1500000 0.0147500 13 | 0.1000000 0.0122000 14 | 0.0500000 0.0088500 15 | 0.0250000 0.0063200 16 | 0.0000000 0.0000000 17 | 0.0250000 -.0042800 18 | 0.0500000 -.0050500 19 | 0.1000000 -.0053000 20 | 0.1500000 -.0050500 21 | 0.2000000 -.0048000 22 | 0.3000000 -.0043000 23 | 0.4000000 -.0038000 24 | 0.5000000 -.0033000 25 | 0.6000000 -.0028000 26 | 0.7000000 -.0023000 27 | 0.8000000 -.0018000 28 | 0.9000000 -.0013000 29 | 0.9500000 -.0010500 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe10k.dat: -------------------------------------------------------------------------------- 1 | GOE 10K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0084100 4 | 0.9000000 0.0141300 5 | 0.8000000 0.0232600 6 | 0.7000000 0.0293900 7 | 0.6000000 0.0328200 8 | 0.5000000 0.0333500 9 | 0.4000000 0.0323800 10 | 0.3000000 0.0305100 11 | 0.2000000 0.0263400 12 | 0.1500000 0.0232600 13 | 0.1000000 0.0192700 14 | 0.0500000 0.0139800 15 | 0.0250000 0.0100900 16 | 0.0000000 0.0000000 17 | 0.0250000 -.0066100 18 | 0.0500000 -.0078100 19 | 0.1000000 -.0082300 20 | 0.1500000 -.0078500 21 | 0.2000000 -.0074600 22 | 0.3000000 -.0066900 23 | 0.4000000 -.0059200 24 | 0.5000000 -.0051500 25 | 0.6000000 -.0043800 26 | 0.7000000 -.0036100 27 | 0.8000000 -.0028400 28 | 0.9000000 -.0020700 29 | 0.9500000 -.0016900 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe11k.dat: -------------------------------------------------------------------------------- 1 | GOE 11K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0161500 4 | 0.9000000 0.0272900 5 | 0.8000000 0.0449800 6 | 0.7000000 0.0568700 7 | 0.6000000 0.0633600 8 | 0.5000000 0.0644500 9 | 0.4000000 0.0625400 10 | 0.3000000 0.0588300 11 | 0.2000000 0.0507200 12 | 0.1500000 0.0447700 13 | 0.1000000 0.0372100 14 | 0.0500000 0.0269500 15 | 0.0250000 0.0192800 16 | 0.0000000 0.0000000 17 | 0.0250000 -.0129200 18 | 0.0500000 -.0152500 19 | 0.1000000 -.0160900 20 | 0.1500000 -.0153300 21 | 0.2000000 -.0145800 22 | 0.3000000 -.0130700 23 | 0.4000000 -.0115600 24 | 0.5000000 -.0100500 25 | 0.6000000 -.0085400 26 | 0.7000000 -.0070300 27 | 0.8000000 -.0055200 28 | 0.9000000 -.0040100 29 | 0.9500000 -.0032600 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe12k.dat: -------------------------------------------------------------------------------- 1 | GOE 12K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0239800 4 | 0.9000000 0.0395600 5 | 0.8000000 0.0670200 6 | 0.7000000 0.0846800 7 | 0.6000000 0.0944400 8 | 0.5000000 0.0960000 9 | 0.4000000 0.0930600 10 | 0.3000000 0.0876200 11 | 0.2000000 0.0755800 12 | 0.1500000 0.0667600 13 | 0.1000000 0.0554400 14 | 0.0500000 0.0402200 15 | 0.0250000 0.0287600 16 | 0.0000000 0.0000000 17 | 0.0250000 -.0192400 18 | 0.0500000 -.0226800 19 | 0.1000000 -.0239600 20 | 0.1500000 -.0228400 21 | 0.2000000 -.0217200 22 | 0.3000000 -.0194800 23 | 0.4000000 -.0172400 24 | 0.5000000 -.0150000 25 | 0.6000000 -.0127600 26 | 0.7000000 -.0105200 27 | 0.8000000 -.0082800 28 | 0.9000000 -.0060400 29 | 0.9500000 -.0049200 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe13k.dat: -------------------------------------------------------------------------------- 1 | GOE 13K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0321100 4 | 0.9000000 0.0542100 5 | 0.8000000 0.0893200 6 | 0.7000000 0.1130300 7 | 0.6000000 0.1260400 8 | 0.5000000 0.1280500 9 | 0.4000000 0.1241600 10 | 0.3000000 0.1168700 11 | 0.2000000 0.1008800 12 | 0.1500000 0.0889900 13 | 0.1000000 0.0738900 14 | 0.0500000 0.0535900 15 | 0.0250000 0.0383500 16 | 0.0000000 0.0000000 17 | 0.0250000 -.0255500 18 | 0.0500000 -.0301000 19 | 0.1000000 -.0319100 20 | 0.1500000 -.0304200 21 | 0.2000000 -.0289200 22 | 0.3000000 -.0259300 23 | 0.4000000 -.0229400 24 | 0.5000000 -.0199500 25 | 0.6000000 -.0169600 26 | 0.7000000 -.0139700 27 | 0.8000000 -.0109800 28 | 0.9000000 -.0079900 29 | 0.9500000 -.0065000 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe14k.dat: -------------------------------------------------------------------------------- 1 | GOE 14K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0226000 4 | 0.9000000 0.0380000 5 | 0.8000000 0.0612000 6 | 0.7000000 0.0776000 7 | 0.6000000 0.0850000 8 | 0.5000000 0.0870000 9 | 0.4000000 0.0838000 10 | 0.3000000 0.0776000 11 | 0.2000000 0.0661000 12 | 0.1500000 0.0581000 13 | 0.1000000 0.0480000 14 | 0.0500000 0.0340000 15 | 0.0250000 0.0237500 16 | 0.0000000 0.0000000 17 | 0.0250000 -.0176500 18 | 0.0500000 -.0233000 19 | 0.1000000 -.0300000 20 | 0.1500000 -.0336000 21 | 0.2000000 -.0353000 22 | 0.3000000 -.0358000 23 | 0.4000000 -.0344000 24 | 0.5000000 -.0330000 25 | 0.6000000 -.0316000 26 | 0.7000000 -.0296000 27 | 0.8000000 -.0262000 28 | 0.9000000 -.0195000 29 | 0.9500000 -.0134000 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe15k.dat: -------------------------------------------------------------------------------- 1 | GOE 15K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0282200 4 | 0.9000000 0.0474500 5 | 0.8000000 0.0765000 6 | 0.7000000 0.0969500 7 | 0.6000000 0.1063000 8 | 0.5000000 0.1087500 9 | 0.4000000 0.1047000 10 | 0.3000000 0.0969500 11 | 0.2000000 0.0826000 12 | 0.1500000 0.0726200 13 | 0.1000000 0.0600500 14 | 0.0500000 0.0424700 15 | 0.0250000 0.0296400 16 | 0.0000000 0.0000000 17 | 0.0250000 -.0221600 18 | 0.0500000 -.0291200 19 | 0.1000000 -.0374500 20 | 0.1500000 -.0419800 21 | 0.2000000 -.0441000 22 | 0.3000000 -.0447500 23 | 0.4000000 -.0430000 24 | 0.5000000 -.0412500 25 | 0.6000000 -.0395000 26 | 0.7000000 -.0370500 27 | 0.8000000 -.0327000 28 | 0.9000000 -.0243500 29 | 0.9500000 -.0167800 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe16k.dat: -------------------------------------------------------------------------------- 1 | GOE 16K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0341500 4 | 0.9000000 0.0574000 5 | 0.8000000 0.0925000 6 | 0.7000000 0.1173000 7 | 0.6000000 0.1286000 8 | 0.5000000 0.1316000 9 | 0.4000000 0.1268000 10 | 0.3000000 0.1174000 11 | 0.2000000 0.1001000 12 | 0.1500000 0.0879500 13 | 0.1000000 0.0727000 14 | 0.0500000 0.0515500 15 | 0.0250000 0.0359200 16 | 0.0000000 0.0000000 17 | 0.0250000 -.0266800 18 | 0.0500000 -.0352500 19 | 0.1000000 -.0452000 20 | 0.1500000 -.0507500 21 | 0.2000000 -.0533000 22 | 0.3000000 -.0541000 23 | 0.4000000 -.0520000 24 | 0.5000000 -.0499000 25 | 0.6000000 -.0478000 26 | 0.7000000 -.0448000 27 | 0.8000000 -.0396000 28 | 0.9000000 -.0295000 29 | 0.9500000 -.0203500 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe405.dat: -------------------------------------------------------------------------------- 1 | GOE 405 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0314000 4 | 0.8000000 0.0593000 5 | 0.7000000 0.0822000 6 | 0.6000000 0.1011000 7 | 0.5000000 0.1140000 8 | 0.4000000 0.1199000 9 | 0.3000000 0.1188000 10 | 0.2000000 0.1067000 11 | 0.1000000 0.0771000 12 | 0.0750000 0.0647000 13 | 0.0500000 0.0498000 14 | 0.0250000 0.0324000 15 | 0.0125000 0.0212000 16 | 0.0000000 0.0000000 17 | 0.0125000 -.0098000 18 | 0.0250000 -.0126000 19 | 0.0500000 -.0147000 20 | 0.0750000 -.0148000 21 | 0.1000000 -.0134000 22 | 0.2000000 -.0018000 23 | 0.3000000 0.0078000 24 | 0.4000000 0.0109000 25 | 0.5000000 0.0115000 26 | 0.6000000 0.0106000 27 | 0.7000000 0.0092000 28 | 0.8000000 0.0068000 29 | 0.9000000 0.0039000 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe439.dat: -------------------------------------------------------------------------------- 1 | GOE 439 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0217000 4 | 0.8000000 0.0404000 5 | 0.7000000 0.0571000 6 | 0.6000000 0.0718000 7 | 0.5000000 0.0825000 8 | 0.4000000 0.0892000 9 | 0.3000000 0.0904000 10 | 0.2000000 0.0831000 11 | 0.1000000 0.0608000 12 | 0.0750000 0.0516000 13 | 0.0500000 0.0409000 14 | 0.0250000 0.0257000 15 | 0.0125000 0.0171000 16 | 0.0000000 0.0000000 17 | 0.0125000 -.0059000 18 | 0.0250000 -.0073000 19 | 0.0500000 -.0071000 20 | 0.0750000 -.0059000 21 | 0.1000000 -.0032000 22 | 0.2000000 0.0056000 23 | 0.3000000 0.0114000 24 | 0.4000000 0.0152000 25 | 0.5000000 0.0170000 26 | 0.6000000 0.0163000 27 | 0.7000000 0.0136000 28 | 0.8000000 0.0094000 29 | 0.9000000 0.0052000 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe443.dat: -------------------------------------------------------------------------------- 1 | GOE 443 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0065000 4 | 0.8000000 0.0115000 5 | 0.7000000 0.0165000 6 | 0.6000000 0.0205000 7 | 0.5000000 0.0235000 8 | 0.4000000 0.0250000 9 | 0.3000000 0.0250000 10 | 0.2000000 0.0215000 11 | 0.1000000 0.0160000 12 | 0.0750000 0.0140000 13 | 0.0500000 0.0115000 14 | 0.0250000 0.0085000 15 | 0.0125000 0.0060000 16 | 0.0000000 0.0000000 17 | 0.0125000 -.0060000 18 | 0.0250000 -.0085000 19 | 0.0500000 -.0115000 20 | 0.0750000 -.0140000 21 | 0.1000000 -.0160000 22 | 0.2000000 -.0215000 23 | 0.3000000 -.0250000 24 | 0.4000000 -.0250000 25 | 0.5000000 -.0235000 26 | 0.6000000 -.0205000 27 | 0.7000000 -.0165000 28 | 0.8000000 -.0115000 29 | 0.9000000 -.0065000 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe496.dat: -------------------------------------------------------------------------------- 1 | GOE 496 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0260000 4 | 0.8000000 0.0470000 5 | 0.7000000 0.0650000 6 | 0.6000000 0.0795000 7 | 0.5000000 0.0895000 8 | 0.4000000 0.0945000 9 | 0.3000000 0.0925000 10 | 0.2000000 0.0825000 11 | 0.1000000 0.0620000 12 | 0.0750000 0.0533800 13 | 0.0500000 0.0427500 14 | 0.0250000 0.0291200 15 | 0.0125000 0.0198100 16 | 0.0000000 0.0000000 17 | 0.0125000 -.0136900 18 | 0.0250000 -.0178800 19 | 0.0500000 -.0212500 20 | 0.0750000 -.0231300 21 | 0.1000000 -.0225000 22 | 0.2000000 -.0165000 23 | 0.3000000 -.0070000 24 | 0.4000000 0.0025000 25 | 0.5000000 0.0105000 26 | 0.6000000 0.0150000 27 | 0.7000000 0.0175000 28 | 0.8000000 0.0150000 29 | 0.9000000 0.0100000 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe670.dat: -------------------------------------------------------------------------------- 1 | GOE 670 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0223500 4 | 0.8000000 0.0417000 5 | 0.7000000 0.0570500 6 | 0.6000000 0.0674000 7 | 0.5000000 0.0757500 8 | 0.4000000 0.0786000 9 | 0.3000000 0.0769500 10 | 0.2000000 0.0703000 11 | 0.1000000 0.0546500 12 | 0.0750000 0.0471100 13 | 0.0500000 0.0380700 14 | 0.0250000 0.0250400 15 | 0.0125000 0.0167700 16 | 0.0000000 0.0000000 17 | 0.0125000 -.0147300 18 | 0.0250000 -.0189600 19 | 0.0500000 -.0219300 20 | 0.0750000 -.0223900 21 | 0.1000000 -.0213500 22 | 0.2000000 -.0172000 23 | 0.3000000 -.0130500 24 | 0.4000000 -.0109000 25 | 0.5000000 -.0097500 26 | 0.6000000 -.0091000 27 | 0.7000000 -.0089500 28 | 0.8000000 -.0063000 29 | 0.9000000 -.0036500 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe682.dat: -------------------------------------------------------------------------------- 1 | GOE 682 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0230000 4 | 0.8000000 0.0435000 5 | 0.7000000 0.0615000 6 | 0.6000000 0.0765000 7 | 0.5000000 0.0880000 8 | 0.4000000 0.0940000 9 | 0.3000000 0.0945000 10 | 0.2000000 0.0865000 11 | 0.1000000 0.0665000 12 | 0.0750000 0.0573800 13 | 0.0500000 0.0462500 14 | 0.0250000 0.0311200 15 | 0.0125000 0.0208100 16 | 0.0000000 0.0000000 17 | 0.0125000 -.0141900 18 | 0.0250000 -.0183700 19 | 0.0500000 -.0212500 20 | 0.0750000 -.0221300 21 | 0.1000000 -.0225000 22 | 0.2000000 -.0180000 23 | 0.3000000 -.0120000 24 | 0.4000000 -.0075000 25 | 0.5000000 -.0045000 26 | 0.6000000 -.0015000 27 | 0.7000000 0.0000000 28 | 0.8000000 0.0010000 29 | 0.9000000 0.0010000 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /r/raf30md.dat: -------------------------------------------------------------------------------- 1 | RAF 30 MOD AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0078000 4 | 0.8000000 0.0150000 5 | 0.7000000 0.0222000 6 | 0.6000000 0.0287000 7 | 0.5000000 0.0340000 8 | 0.4000000 0.0372000 9 | 0.3000000 0.0380000 10 | 0.2000000 0.0356000 11 | 0.1500000 0.0326000 12 | 0.1000000 0.0281000 13 | 0.0500000 0.0208000 14 | 0.0250000 0.0149000 15 | 0.0125000 0.0108000 16 | 0.0000000 0.0000000 17 | 0.0125000 -.0108000 18 | 0.0250000 -.0149000 19 | 0.0500000 -.0208000 20 | 0.1000000 -.0281000 21 | 0.1500000 -.0326000 22 | 0.2000000 -.0356000 23 | 0.3000000 -.0380000 24 | 0.4000000 -.0372000 25 | 0.5000000 -.0340000 26 | 0.6000000 -.0287000 27 | 0.7000000 -.0222000 28 | 0.8000000 -.0150000 29 | 0.9000000 -.0078000 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /r/raf32md.dat: -------------------------------------------------------------------------------- 1 | RAF 32 MOD AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0251600 4 | 0.8000000 0.0462200 5 | 0.7000000 0.0638800 6 | 0.6000000 0.0769400 7 | 0.5000000 0.0853000 8 | 0.4000000 0.0881600 9 | 0.3000000 0.0845200 10 | 0.2000000 0.0733800 11 | 0.1500000 0.0645600 12 | 0.1000000 0.0530400 13 | 0.0500000 0.0366200 14 | 0.0250000 0.0254600 15 | 0.0125000 0.0174300 16 | 0.0000000 0.0000000 17 | 0.0125000 -.0113700 18 | 0.0250000 -.0147400 19 | 0.0500000 -.0190800 20 | 0.1000000 -.0223600 21 | 0.1500000 -.0228400 22 | 0.2000000 -.0221200 23 | 0.3000000 -.0170800 24 | 0.4000000 -.0112400 25 | 0.5000000 -.0062000 26 | 0.6000000 0.0001400 27 | 0.7000000 0.0038800 28 | 0.8000000 0.0054200 29 | 0.9000000 0.0037600 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /s/saratov.dat: -------------------------------------------------------------------------------- 1 | SARATOV AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0285000 4 | 0.8000000 0.0550000 5 | 0.7000000 0.0775000 6 | 0.6000000 0.0970000 7 | 0.5000000 0.1135000 8 | 0.4000000 0.1250000 9 | 0.3000000 0.1175000 10 | 0.2000000 0.0970000 11 | 0.1500000 0.0827500 12 | 0.1000000 0.0675000 13 | 0.0500000 0.0462500 14 | 0.0250000 0.0306300 15 | 0.0125000 0.0203100 16 | 0.0000000 0.0000000 17 | 0.0125000 -.0146900 18 | 0.0250000 -.0193800 19 | 0.0500000 -.0217500 20 | 0.1000000 -.0205000 21 | 0.1500000 -.0092500 22 | 0.2000000 0.0050000 23 | 0.3000000 0.0355000 24 | 0.4000000 0.0700000 25 | 0.5000000 0.0625000 26 | 0.6000000 0.0500000 27 | 0.7000000 0.0375000 28 | 0.8000000 0.0250000 29 | 0.9000000 0.0125000 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /g/goe610bm.dat: -------------------------------------------------------------------------------- 1 | GOE 610-B MOD. AIRFOIL 2 | 1.0000000 0.0080000 3 | 0.9000000 0.0273000 4 | 0.8000000 0.0466000 5 | 0.7000000 0.0629000 6 | 0.6000000 0.0772000 7 | 0.5000000 0.0865000 8 | 0.4000000 0.0928000 9 | 0.3000000 0.0931000 10 | 0.2000000 0.0834000 11 | 0.1500000 0.0740500 12 | 0.1000000 0.0617000 13 | 0.0500000 0.0433500 14 | 0.0250000 0.0281800 15 | 0.0125000 0.0170900 16 | 0.0000000 0.0000000 17 | 0.0125000 -.0069100 18 | 0.0250000 -.0068300 19 | 0.0500000 -.0046500 20 | 0.1000000 -.0003000 21 | 0.1500000 0.0040500 22 | 0.2000000 0.0094000 23 | 0.3000000 0.0161000 24 | 0.4000000 0.0208000 25 | 0.5000000 0.0225000 26 | 0.6000000 0.0232000 27 | 0.7000000 0.0209000 28 | 0.8000000 0.0146000 29 | 0.9000000 0.0073000 30 | 1.0000000 0.0000000 31 | -------------------------------------------------------------------------------- /h/hobie.dat: -------------------------------------------------------------------------------- 1 | HOBIE 2 | 1.00000 0.00000 3 | 0.9 0.01943 4 | 0.8 0.03619 5 | 0.7 0.05105 6 | 0.6 0.06400 7 | 0.5 0.07302 8 | 0.45 0.07606 9 | 0.4 0.07784 10 | 0.35 0.07911 11 | 0.30 0.07835 12 | 0.25 0.07568 13 | 0.20 0.06984 14 | 0.15 0.06349 15 | 0.10 0.05206 16 | 0.075 0.04406 17 | 0.05 0.03492 18 | 0.025 0.02413 19 | 0.0000 0.00000 20 | 0.025 -.01460 21 | 0.05 -.01651 22 | 0.075 -.01714 23 | 0.1 -.01778 24 | 0.15 -.01651 25 | 0.20 -.01359 26 | 0.25 -.00927 27 | 0.30 -.00635 28 | 0.35 -.00229 29 | 0.4 0.00063 30 | 0.45 0.00317 31 | 0.5 0.00508 32 | 0.6 0.00813 33 | 0.7 0.00952 34 | 0.8 0.00800 35 | 0.9 0.00483 36 | 1.00000 0.00000 37 | -------------------------------------------------------------------------------- /b/b707d.dat: -------------------------------------------------------------------------------- 1 | BOEING 707 .54 SPAN AIRFOIL 2 | 1.0000 0.0000 3 | 0.9000 0.0145 4 | 0.8000 0.0290 5 | 0.7000 0.0427 6 | 0.6000 0.0541 7 | 0.5000 0.0618 8 | 0.4000 0.0644 9 | 0.3000 0.0627 10 | 0.2500 0.0604 11 | 0.2000 0.0570 12 | 0.1500 0.0520 13 | 0.1000 0.0442 14 | 0.0753 0.0385 15 | 0.0500 0.0303 16 | 0.0250 0.0215 17 | 0.0126 0.0147 18 | 0.0074 0.0120 19 | 0.0050 0.0099 20 | 0.0000 0.0030 21 | 0.0050 -0.0046 22 | 0.0074 -0.0055 23 | 0.0126 -0.0065 24 | 0.0250 -0.0074 25 | 0.0500 -0.0090 26 | 0.0753 -0.0105 27 | 0.1000 -0.0118 28 | 0.1500 -0.0149 29 | 0.2000 -0.0177 30 | 0.2500 -0.0206 31 | 0.3000 -0.0227 32 | 0.4000 -0.0253 33 | 0.5000 -0.0250 34 | 0.6000 -0.0208 35 | 0.7000 -0.0156 36 | 0.8000 -0.0105 37 | 0.9000 -0.0051 38 | 1.0000 0.0000 39 | -------------------------------------------------------------------------------- /b/b707b.dat: -------------------------------------------------------------------------------- 1 | BOEING 707 .19 SPAN AIRFOIL 2 | 1.000000 0.000000 3 | 0.598899 0.046634 4 | 0.498566 0.060766 5 | 0.398560 0.061006 6 | 0.298540 0.061846 7 | 0.248554 0.061266 8 | 0.198551 0.061386 9 | 0.148638 0.057708 10 | 0.098786 0.051431 11 | 0.073920 0.045745 12 | 0.049040 0.040657 13 | 0.024309 0.029274 14 | 0.012157 0.018787 15 | 0.007052 0.014766 16 | 0.004712 0.012211 17 | 0.000000 0.000000 18 | 0.005209 -0.008877 19 | 0.007681 -0.011919 20 | 0.012940 -0.014395 21 | 0.025467 -0.019799 22 | 0.050649 -0.027505 23 | 0.075755 -0.032012 24 | 0.100876 -0.037119 25 | 0.151044 -0.044235 26 | 0.201198 -0.050752 27 | 0.251319 -0.055869 28 | 0.301411 -0.059787 29 | 0.401417 -0.060027 30 | 0.501361 -0.057668 31 | 0.601185 -0.050212 32 | 1.000000 0.000000 33 | -------------------------------------------------------------------------------- /e/eiffel10.dat: -------------------------------------------------------------------------------- 1 | Eiffel 10 (Wright) - 1903 Wright Flyer airfoil 2 | 1.0000 0.0064 3 | .9500 0.0143 4 | .9000 0.0220 5 | .8000 0.0370 6 | .7000 0.0510 7 | .6000 0.0623 8 | .5000 0.0693 9 | .4000 0.0718 10 | .3000 0.0701 11 | .2000 0.0614 12 | .1500 0.0550 13 | .1000 0.0468 14 | .0750 0.0423 15 | .0500 0.0375 16 | .0250 0.0323 17 | .0125 0.0296 18 | .0000 0.0273 19 | .0000 0.0000 20 | .0125 0.0032 21 | .0250 0.0060 22 | .0500 0.0117 23 | .0750 0.0170 24 | .1000 0.0223 25 | .1500 0.0315 26 | .2000 0.0390 27 | .3000 0.0486 28 | .4000 0.0527 29 | .5000 0.0518 30 | .6000 0.0456 31 | .7000 0.0370 32 | .8000 0.0255 33 | .9000 0.0127 34 | .9500 0.0065 35 | 1.0000 0.0000 -------------------------------------------------------------------------------- /n/n10.dat: -------------------------------------------------------------------------------- 1 | N-10 2 | 1.0000 0.0034 3 | 0.9500 0.0174 4 | 0.9000 0.0296 5 | 0.8000 0.0510 6 | 0.7000 0.0712 7 | 0.6000 0.0874 8 | 0.5000 0.1010 9 | 0.4000 0.1088 10 | 0.3000 0.1124 11 | 0.2000 0.1096 12 | 0.1500 0.1022 13 | 0.1000 0.0914 14 | 0.0750 0.0842 15 | 0.0500 0.0738 16 | 0.0250 0.0594 17 | 0.0125 0.0492 18 | 0.0000 0.0300 19 | 0.0125 0.0158 20 | 0.0250 0.0114 21 | 0.0500 0.0068 22 | 0.0750 0.0042 23 | 0.1000 0.0026 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0002 27 | 0.4000 0.0006 28 | 0.5000 0.0012 29 | 0.6000 0.0014 30 | 0.7000 0.0010 31 | 0.8000 0.0008 32 | 0.9000 0.0004 33 | 0.9500 0.0002 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /n/n11.dat: -------------------------------------------------------------------------------- 1 | N-11 2 | 1.0000 0.0020 3 | 0.9500 0.0165 4 | 0.9000 0.0300 5 | 0.8000 0.0524 6 | 0.7000 0.0732 7 | 0.6000 0.0898 8 | 0.5000 0.1026 9 | 0.4000 0.1108 10 | 0.3000 0.1128 11 | 0.2000 0.1082 12 | 0.1500 0.1008 13 | 0.1000 0.0890 14 | 0.0750 0.0800 15 | 0.0500 0.0694 16 | 0.0250 0.0540 17 | 0.0125 0.0430 18 | 0.0000 0.0230 19 | 0.0125 0.0094 20 | 0.0250 0.0060 21 | 0.0500 0.0022 22 | 0.0750 0.0006 23 | 0.1000 0.0000 24 | 0.1500 0.0002 25 | 0.2000 0.0014 26 | 0.3000 0.0034 27 | 0.4000 0.0048 28 | 0.5000 0.0056 29 | 0.6000 0.0060 30 | 0.7000 0.0050 31 | 0.8000 0.0034 32 | 0.9000 0.0016 33 | 0.9500 0.0008 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /n/n22.dat: -------------------------------------------------------------------------------- 1 | N-22 2 | 1.0000 0.0040 3 | 0.9500 0.0173 4 | 0.9000 0.0306 5 | 0.8000 0.0551 6 | 0.7000 0.0768 7 | 0.6000 0.0957 8 | 0.5000 0.1104 9 | 0.4000 0.1201 10 | 0.3000 0.1242 11 | 0.2000 0.1201 12 | 0.1500 0.1128 13 | 0.1000 0.1013 14 | 0.0750 0.0933 15 | 0.0500 0.0825 16 | 0.0250 0.0666 17 | 0.0125 0.0558 18 | 0.0000 0.0337 19 | 0.0125 0.0170 20 | 0.0250 0.0115 21 | 0.0500 0.0062 22 | 0.0750 0.0032 23 | 0.1000 0.0016 24 | 0.1500 0.0003 25 | 0.2000 0.0000 26 | 0.3000 0.0005 27 | 0.4000 0.0015 28 | 0.5000 0.0024 29 | 0.6000 0.0030 30 | 0.7000 0.0032 31 | 0.8000 0.0024 32 | 0.9000 0.0012 33 | 0.9500 0.0005 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /n/n24.dat: -------------------------------------------------------------------------------- 1 | N-24 2 | 1.0000 0.0130 3 | 0.9500 0.0230 4 | 0.9000 0.0396 5 | 0.8000 0.0732 6 | 0.7000 0.1039 7 | 0.6000 0.1302 8 | 0.5000 0.1512 9 | 0.4000 0.1660 10 | 0.3000 0.1712 11 | 0.2000 0.1660 12 | 0.1500 0.1564 13 | 0.1000 0.1404 14 | 0.0750 0.1294 15 | 0.0500 0.1142 16 | 0.0250 0.0928 17 | 0.0125 0.0764 18 | 0.0000 0.0460 19 | 0.0125 0.0240 20 | 0.0250 0.0176 21 | 0.0500 0.0090 22 | 0.0750 0.0054 23 | 0.1000 0.0026 24 | 0.1500 0.0004 25 | 0.2000 0.0000 26 | 0.3000 0.0010 27 | 0.4000 0.0026 28 | 0.5000 0.0038 29 | 0.6000 0.0044 30 | 0.7000 0.0046 31 | 0.8000 0.0030 32 | 0.9000 0.0008 33 | 0.9500 0.0006 34 | 1.0000 0.0030 35 | -------------------------------------------------------------------------------- /n/n9.dat: -------------------------------------------------------------------------------- 1 | N-9 2 | 1.0000 0.0028 3 | 0.9500 0.0135 4 | 0.9000 0.0212 5 | 0.8000 0.0386 6 | 0.7000 0.0524 7 | 0.6000 0.0652 8 | 0.5000 0.0760 9 | 0.4000 0.0822 10 | 0.3000 0.0846 11 | 0.2000 0.0826 12 | 0.1500 0.0776 13 | 0.1000 0.0692 14 | 0.0750 0.0644 15 | 0.0500 0.0580 16 | 0.0250 0.0478 17 | 0.0125 0.0398 18 | 0.0000 0.0225 19 | 0.0125 0.0124 20 | 0.0250 0.0088 21 | 0.0500 0.0048 22 | 0.0750 0.0030 23 | 0.1000 0.0022 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0000 27 | 0.4000 0.0002 28 | 0.5000 0.0008 29 | 0.6000 0.0012 30 | 0.7000 0.0012 31 | 0.8000 0.0008 32 | 0.9000 0.0002 33 | 0.9500 0.0001 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /d/dormoy.dat: -------------------------------------------------------------------------------- 1 | Dormoy 2 | 1.0000 0.0000 3 | 0.9500 0.0105 4 | 0.9000 0.0200 5 | 0.8000 0.0367 6 | 0.7000 0.0540 7 | 0.6000 0.0687 8 | 0.5000 0.0800 9 | 0.4000 0.0873 10 | 0.3000 0.0900 11 | 0.2000 0.0880 12 | 0.1500 0.0820 13 | 0.1000 0.0733 14 | 0.0750 0.0635 15 | 0.0500 0.0535 16 | 0.0250 0.0445 17 | 0.0125 0.0360 18 | 0.0000 0.0247 19 | 0.0125 0.0200 20 | 0.0250 0.0170 21 | 0.0500 0.0120 22 | 0.0750 0.0085 23 | 0.1000 0.0053 24 | 0.1500 0.0035 25 | 0.2000 0.0027 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0000 31 | 0.8000 0.0000 32 | 0.9000 0.0000 33 | 0.9500 0.0000 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /s/strand.dat: -------------------------------------------------------------------------------- 1 | STRAND AIRFOIL 2 | 1.0000 0.0000 3 | 0.9540 0.0031 4 | 0.8949 0.0082 5 | 0.7901 0.0203 6 | 0.6978 0.0341 7 | 0.5981 0.0524 8 | 0.5186 0.0690 9 | 0.4395 0.0868 10 | 0.4100 0.0943 11 | 0.3805 0.1018 12 | 0.3214 0.1160 13 | 0.2607 0.1167 14 | 0.2003 0.1093 15 | 0.1607 0.1005 16 | 0.1030 0.0815 17 | 0.0488 0.0541 18 | 0.0198 0.0320 19 | 0.0114 0.0232 20 | 0.0044 0.0133 21 | 0.0000 0.0000 22 | 0.0048 -.0152 23 | 0.0106 -.0208 24 | 0.0240 -.0237 25 | 0.0459 -.0273 26 | 0.1069 -.0366 27 | 0.1652 -.0399 28 | 0.2090 -.0397 29 | 0.2632 -.0377 30 | 0.3193 -.0344 31 | 0.3972 -.0281 32 | 0.4171 -.0263 33 | 0.4374 -.0243 34 | 0.5200 -.0164 35 | 0.6044 -.0089 36 | 0.6914 -.0027 37 | 0.7800 0.0023 38 | 0.8917 0.0042 39 | 0.9579 0.0026 40 | 1.0000 0.0000 41 | -------------------------------------------------------------------------------- /b/bambino6.dat: -------------------------------------------------------------------------------- 1 | Bambino 6 2 | 1.0000 0.0350 3 | 0.9500 0.0470 4 | 0.9000 0.0570 5 | 0.8000 0.0750 6 | 0.7000 0.0910 7 | 0.6000 0.1030 8 | 0.5000 0.1140 9 | 0.4000 0.1200 10 | 0.3000 0.1180 11 | 0.2000 0.1090 12 | 0.1500 0.1014 13 | 0.1000 0.0915 14 | 0.0750 0.0850 15 | 0.0500 0.0750 16 | 0.0250 0.0630 17 | 0.0125 0.0415 18 | 0.0000 0.0300 19 | 0.0125 0.0155 20 | 0.0250 0.0100 21 | 0.0500 0.0050 22 | 0.0750 0.0030 23 | 0.1000 0.0000 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0000 31 | 0.8000 0.0050 32 | 0.9000 0.0200 33 | 0.9500 0.0250 34 | 1.0000 0.0350 35 | -------------------------------------------------------------------------------- /c/coanda1.dat: -------------------------------------------------------------------------------- 1 | Coanda 1 2 | 1.0000 0.0100 3 | 0.9500 0.0195 4 | 0.9000 0.0270 5 | 0.8000 0.0400 6 | 0.7000 0.0500 7 | 0.6000 0.0585 8 | 0.5000 0.0650 9 | 0.4000 0.0695 10 | 0.3000 0.0700 11 | 0.2000 0.0670 12 | 0.1500 0.0632 13 | 0.1000 0.0570 14 | 0.0750 0.0515 15 | 0.0500 0.0435 16 | 0.0250 0.0325 17 | 0.0125 0.0240 18 | 0.0000 0.0140 19 | 0.0125 0.0070 20 | 0.0250 0.0030 21 | 0.0500 0.0000 22 | 0.0750 0.0030 23 | 0.1000 0.0070 24 | 0.1500 0.0100 25 | 0.2000 0.0115 26 | 0.3000 0.0135 27 | 0.4000 0.0135 28 | 0.5000 0.0125 29 | 0.6000 0.0110 30 | 0.7000 0.0085 31 | 0.8000 0.0040 32 | 0.9000 0.0000 33 | 0.9500 0.0030 34 | 1.0000 0.0100 35 | -------------------------------------------------------------------------------- /c/coanda2.dat: -------------------------------------------------------------------------------- 1 | Coanda 2 2 | 1.0000 0.0070 3 | 0.9500 0.0170 4 | 0.9000 0.0250 5 | 0.8000 0.0390 6 | 0.7000 0.0500 7 | 0.6000 0.0580 8 | 0.5000 0.0650 9 | 0.4000 0.0700 10 | 0.3000 0.0730 11 | 0.2000 0.0710 12 | 0.1500 0.0670 13 | 0.1000 0.0600 14 | 0.0750 0.0545 15 | 0.0500 0.0465 16 | 0.0250 0.0355 17 | 0.0125 0.0270 18 | 0.0000 0.0170 19 | 0.0125 0.0088 20 | 0.0250 0.0040 21 | 0.0500 0.0000 22 | 0.0750 0.0025 23 | 0.1000 0.0060 24 | 0.1500 0.0090 25 | 0.2000 0.0112 26 | 0.3000 0.0130 27 | 0.4000 0.0130 28 | 0.5000 0.0125 29 | 0.6000 0.0115 30 | 0.7000 0.0100 31 | 0.8000 0.0070 32 | 0.9000 0.0020 33 | 0.9500 0.0000 34 | 1.0000 0.0070 35 | -------------------------------------------------------------------------------- /c/coanda3.dat: -------------------------------------------------------------------------------- 1 | Coanda 3 2 | 1.0000 0.0070 3 | 0.9500 0.0185 4 | 0.9000 0.0280 5 | 0.8000 0.0450 6 | 0.7000 0.0572 7 | 0.6000 0.0670 8 | 0.5000 0.0740 9 | 0.4000 0.0770 10 | 0.3000 0.0770 11 | 0.2000 0.0740 12 | 0.1500 0.0695 13 | 0.1000 0.0620 14 | 0.0750 0.0560 15 | 0.0500 0.0480 16 | 0.0250 0.0362 17 | 0.0125 0.0285 18 | 0.0000 0.0170 19 | 0.0125 0.0105 20 | 0.0250 0.0055 21 | 0.0500 0.0005 22 | 0.0750 0.0005 23 | 0.1000 0.0020 24 | 0.1500 0.0045 25 | 0.2000 0.0055 26 | 0.3000 0.0070 27 | 0.4000 0.0070 28 | 0.5000 0.0070 29 | 0.6000 0.0050 30 | 0.7000 0.0030 31 | 0.8000 0.0000 32 | 0.9000 0.0020 33 | 0.9500 0.0030 34 | 1.0000 0.0070 35 | -------------------------------------------------------------------------------- /i/isa571.dat: -------------------------------------------------------------------------------- 1 | I.S.A. 571 2 | 1.0000 0.0030 3 | 0.9500 0.0150 4 | 0.9000 0.0250 5 | 0.8000 0.0410 6 | 0.7000 0.0532 7 | 0.6000 0.0632 8 | 0.5000 0.0717 9 | 0.4000 0.0772 10 | 0.3000 0.0802 11 | 0.2000 0.0780 12 | 0.1500 0.0725 13 | 0.1000 0.0640 14 | 0.0750 0.0570 15 | 0.0500 0.0487 16 | 0.0250 0.0355 17 | 0.0125 0.0267 18 | 0.0000 0.0100 19 | 0.0125 0.0024 20 | 0.0250 0.0000 21 | 0.0500 0.0000 22 | 0.0750 0.0000 23 | 0.1000 0.0020 24 | 0.1500 0.0040 25 | 0.2000 0.0055 26 | 0.3000 0.0065 27 | 0.4000 0.0070 28 | 0.5000 0.0070 29 | 0.6000 0.0062 30 | 0.7000 0.0055 31 | 0.8000 0.0044 32 | 0.9000 0.0025 33 | 0.9500 0.0015 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /i/isa960.dat: -------------------------------------------------------------------------------- 1 | I.S.A. 960 2 | 1.0000 0.0042 3 | 0.9500 0.0170 4 | 0.9000 0.0275 5 | 0.8000 0.0495 6 | 0.7000 0.0677 7 | 0.6000 0.0842 8 | 0.5000 0.0957 9 | 0.4000 0.1030 10 | 0.3000 0.1043 11 | 0.2000 0.0990 12 | 0.1500 0.0935 13 | 0.1000 0.0792 14 | 0.0750 0.0750 15 | 0.0500 0.0637 16 | 0.0250 0.0490 17 | 0.0125 0.0383 18 | 0.0000 0.0180 19 | 0.0125 0.0085 20 | 0.0250 0.0050 21 | 0.0500 0.0005 22 | 0.0750 0.0000 23 | 0.1000 0.0000 24 | 0.1500 0.0030 25 | 0.2000 0.0055 26 | 0.3000 0.0097 27 | 0.4000 0.0112 28 | 0.5000 0.0115 29 | 0.6000 0.0095 30 | 0.7000 0.0075 31 | 0.8000 0.0050 32 | 0.9000 0.0025 33 | 0.9500 0.0010 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /i/isa961.dat: -------------------------------------------------------------------------------- 1 | I.S.A. 961 2 | 1.0000 0.0037 3 | 0.9500 0.0168 4 | 0.9000 0.0277 5 | 0.8000 0.0490 6 | 0.7000 0.0675 7 | 0.6000 0.0825 8 | 0.5000 0.0937 9 | 0.4000 0.1005 10 | 0.3000 0.1030 11 | 0.2000 0.0987 12 | 0.1500 0.0925 13 | 0.1000 0.0807 14 | 0.0750 0.0740 15 | 0.0500 0.0620 16 | 0.0250 0.0490 17 | 0.0125 0.0372 18 | 0.0000 0.0162 19 | 0.0125 0.0080 20 | 0.0250 0.0038 21 | 0.0500 0.0000 22 | 0.0750 0.0000 23 | 0.1000 0.0000 24 | 0.1500 0.0030 25 | 0.2000 0.0060 26 | 0.3000 0.0105 27 | 0.4000 0.0122 28 | 0.5000 0.0112 29 | 0.6000 0.0097 30 | 0.7000 0.0077 31 | 0.8000 0.0047 32 | 0.9000 0.0020 33 | 0.9500 0.0001 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /i/isa962.dat: -------------------------------------------------------------------------------- 1 | I.S.A. 962 2 | 1.0000 0.0042 3 | 0.9500 0.0166 4 | 0.9000 0.0269 5 | 0.8000 0.0490 6 | 0.7000 0.0682 7 | 0.6000 0.0842 8 | 0.5000 0.0967 9 | 0.4000 0.1042 10 | 0.3000 0.1060 11 | 0.2000 0.1025 12 | 0.1500 0.0960 13 | 0.1000 0.0870 14 | 0.0750 0.0800 15 | 0.0500 0.0702 16 | 0.0250 0.0550 17 | 0.0125 0.0430 18 | 0.0000 0.0200 19 | 0.0125 0.0035 20 | 0.0250 0.0010 21 | 0.0500 0.0000 22 | 0.0750 0.0000 23 | 0.1000 0.0015 24 | 0.1500 0.0040 25 | 0.2000 0.0067 26 | 0.3000 0.0115 27 | 0.4000 0.0144 28 | 0.5000 0.0137 29 | 0.6000 0.0122 30 | 0.7000 0.0090 31 | 0.8000 0.0055 32 | 0.9000 0.0022 33 | 0.9500 0.0002 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /n/nacacyh.dat: -------------------------------------------------------------------------------- 1 | NACA CYH 2 | 1.0000 0.0205 3 | 0.9500 0.0293 4 | 0.9000 0.0384 5 | 0.8000 0.0562 6 | 0.7000 0.0741 7 | 0.6000 0.0915 8 | 0.5000 0.1052 9 | 0.4000 0.1140 10 | 0.3000 0.1170 11 | 0.2000 0.1136 12 | 0.1500 0.1068 13 | 0.1000 0.0960 14 | 0.0750 0.0885 15 | 0.0500 0.0790 16 | 0.0250 0.0650 17 | 0.0125 0.0545 18 | 0.0000 0.0350 19 | 0.0125 0.0193 20 | 0.0250 0.0147 21 | 0.0500 0.0093 22 | 0.0750 0.0063 23 | 0.1000 0.0042 24 | 0.1500 0.0015 25 | 0.2000 0.0003 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0006 31 | 0.8000 0.0038 32 | 0.9000 0.0102 33 | 0.9500 0.0140 34 | 1.0000 0.0185 35 | -------------------------------------------------------------------------------- /n/nacam18.dat: -------------------------------------------------------------------------------- 1 | NACA M18 2 | 1.0000 0.0295 3 | 0.9500 0.0366 4 | 0.9000 0.0445 5 | 0.8000 0.0623 6 | 0.7000 0.0809 7 | 0.6000 0.0982 8 | 0.5000 0.1133 9 | 0.4000 0.1226 10 | 0.3000 0.1242 11 | 0.2000 0.1148 12 | 0.1500 0.1047 13 | 0.1000 0.0894 14 | 0.0750 0.0799 15 | 0.0500 0.0678 16 | 0.0250 0.0525 17 | 0.0125 0.0425 18 | 0.0000 0.0220 19 | 0.0125 0.0056 20 | 0.0250 0.0025 21 | 0.0500 0.0003 22 | 0.0750 0.0000 23 | 0.1000 0.0003 24 | 0.1500 0.0017 25 | 0.2000 0.0031 26 | 0.3000 0.0046 27 | 0.4000 0.0041 28 | 0.5000 0.0019 29 | 0.6000 0.0003 30 | 0.7000 0.0005 31 | 0.8000 0.0040 32 | 0.9000 0.0117 33 | 0.9500 0.0175 34 | 1.0000 0.0251 35 | -------------------------------------------------------------------------------- /c/cj3209.dat: -------------------------------------------------------------------------------- 1 | CJ3209 2 | 1.00000 0.00000 3 | 0.95000 0.00360 4 | 0.90000 0.00610 5 | 0.80000 0.01120 6 | 0.70000 0.02550 7 | 0.60000 0.03980 8 | 0.50000 0.05240 9 | 0.40000 0.06150 10 | 0.30000 0.06650 11 | 0.20000 0.06360 12 | 0.15000 0.05750 13 | 0.10000 0.04720 14 | 0.07500 0.03950 15 | 0.05000 0.03040 16 | 0.02500 0.02020 17 | 0.01250 0.01000 18 | 0.00000 0.00000 19 | 0.01250 -0.01110 20 | 0.02500 -0.01390 21 | 0.05000 -0.01810 22 | 0.07500 -0.02200 23 | 0.10000 -0.02500 24 | 0.15000 -0.02750 25 | 0.20000 -0.02810 26 | 0.30000 -0.02690 27 | 0.40000 -0.02470 28 | 0.50000 -0.02280 29 | 0.60000 -0.02100 30 | 0.70000 -0.01910 31 | 0.80000 -0.01740 32 | 0.90000 -0.01200 33 | 0.95000 -0.00640 34 | 1.00000 0.00000 35 | 36 | http://perso.wanadoo.fr/scherrer/matthieu/fwairf.html -------------------------------------------------------------------------------- /c/curtisc72.dat: -------------------------------------------------------------------------------- 1 | Curtis C-72 2 | 1.0000 0.0010 3 | 0.9500 0.0152 4 | 0.9000 0.0280 5 | 0.8000 0.0523 6 | 0.7000 0.0736 7 | 0.6000 0.0915 8 | 0.5000 0.1053 9 | 0.4000 0.1141 10 | 0.3000 0.1173 11 | 0.2000 0.1136 12 | 0.1500 0.1069 13 | 0.1000 0.0960 14 | 0.0750 0.0885 15 | 0.0500 0.0789 16 | 0.0250 0.0651 17 | 0.0125 0.0555 18 | 0.0000 0.0349 19 | 0.0125 0.0192 20 | 0.0250 0.0147 21 | 0.0500 0.0093 22 | 0.0750 0.0064 23 | 0.1000 0.0043 24 | 0.1500 0.0016 25 | 0.2000 0.0003 26 | 0.3000 0.0000 27 | 0.4000 0.0021 28 | 0.5000 0.0059 29 | 0.6000 0.0085 30 | 0.7000 0.0091 31 | 0.8000 0.0072 32 | 0.9000 0.0040 33 | 0.9500 0.0021 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /d/dga1138.dat: -------------------------------------------------------------------------------- 1 | D.G.A. 1138 2 | 1.0000 0.0100 3 | 0.9500 0.0200 4 | 0.9000 0.0275 5 | 0.8000 0.0425 6 | 0.7000 0.0550 7 | 0.6000 0.0650 8 | 0.5000 0.0700 9 | 0.4000 0.0750 10 | 0.3000 0.0750 11 | 0.2000 0.0700 12 | 0.1500 0.0655 13 | 0.1000 0.0600 14 | 0.0750 0.0550 15 | 0.0500 0.0490 16 | 0.0250 0.0390 17 | 0.0125 0.0320 18 | 0.0000 0.0200 19 | 0.0125 0.0090 20 | 0.0250 0.0060 21 | 0.0500 0.0040 22 | 0.0750 0.0010 23 | 0.1000 0.0000 24 | 0.1500 0.0010 25 | 0.2000 0.0030 26 | 0.3000 0.0060 27 | 0.4000 0.0060 28 | 0.5000 0.0050 29 | 0.6000 0.0030 30 | 0.7000 0.0020 31 | 0.8000 0.0010 32 | 0.9000 0.0000 33 | 0.9500 0.0010 34 | 1.0000 0.0040 35 | -------------------------------------------------------------------------------- /e/ebambino7.dat: -------------------------------------------------------------------------------- 1 | E. Bambino 2 | 1.0000 0.0270 3 | 0.9500 0.0290 4 | 0.9000 0.0325 5 | 0.8000 0.0400 6 | 0.7000 0.0460 7 | 0.6000 0.0520 8 | 0.5000 0.0580 9 | 0.4000 0.0600 10 | 0.3000 0.0580 11 | 0.2000 0.0555 12 | 0.1500 0.0510 13 | 0.1000 0.0480 14 | 0.0750 0.0430 15 | 0.0500 0.0360 16 | 0.0250 0.0295 17 | 0.0125 0.0160 18 | 0.0000 0.0050 19 | 0.0125 0.0020 20 | 0.0250 0.0000 21 | 0.0500 0.0000 22 | 0.0750 0.0000 23 | 0.1000 0.0000 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0010 31 | 0.8000 0.0075 32 | 0.9000 0.0140 33 | 0.9500 0.0180 34 | 1.0000 0.0220 35 | -------------------------------------------------------------------------------- /f/fg1.dat: -------------------------------------------------------------------------------- 1 | Fage & Collins 1 2 | 1.0000 0.0040 3 | 0.9500 0.0185 4 | 0.9000 0.0273 5 | 0.8000 0.0451 6 | 0.7000 0.0593 7 | 0.6000 0.0694 8 | 0.5000 0.0761 9 | 0.4000 0.0806 10 | 0.3000 0.0817 11 | 0.2000 0.0775 12 | 0.1500 0.0725 13 | 0.1000 0.0651 14 | 0.0750 0.0590 15 | 0.0500 0.0510 16 | 0.0250 0.0398 17 | 0.0125 0.0315 18 | 0.0000 0.0133 19 | 0.0125 0.0002 20 | 0.0250 0.0000 21 | 0.0500 0.0000 22 | 0.0750 0.0000 23 | 0.1000 0.0000 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0000 31 | 0.8000 0.0000 32 | 0.9000 0.0000 33 | 0.9500 0.0000 34 | 1.0000 0.0040 35 | -------------------------------------------------------------------------------- /f/fg2.dat: -------------------------------------------------------------------------------- 1 | Fage & Collins 2 2 | 1.0000 0.0050 3 | 0.9500 0.0185 4 | 0.9000 0.0265 5 | 0.8000 0.0410 6 | 0.7000 0.0530 7 | 0.6000 0.0630 8 | 0.5000 0.0720 9 | 0.4000 0.0790 10 | 0.3000 0.0816 11 | 0.2000 0.0785 12 | 0.1500 0.0720 13 | 0.1000 0.0625 14 | 0.0750 0.0560 15 | 0.0500 0.0465 16 | 0.0250 0.0337 17 | 0.0125 0.0245 18 | 0.0000 0.0083 19 | 0.0125 0.0000 20 | 0.0250 0.0000 21 | 0.0500 0.0000 22 | 0.0750 0.0000 23 | 0.1000 0.0000 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0000 31 | 0.8000 0.0000 32 | 0.9000 0.0000 33 | 0.9500 0.0000 34 | 1.0000 0.0050 35 | -------------------------------------------------------------------------------- /f/fg3.dat: -------------------------------------------------------------------------------- 1 | Fage & Collins 3 2 | 1.0000 0.0065 3 | 0.9500 0.0225 4 | 0.9000 0.0325 5 | 0.8000 0.0533 6 | 0.7000 0.0705 7 | 0.6000 0.0835 8 | 0.5000 0.0925 9 | 0.4000 0.0985 10 | 0.3000 0.1014 11 | 0.2000 0.0976 12 | 0.1500 0.0900 13 | 0.1000 0.0758 14 | 0.0750 0.0660 15 | 0.0500 0.0528 16 | 0.0250 0.0370 17 | 0.0125 0.0270 18 | 0.0000 0.0083 19 | 0.0125 0.0000 20 | 0.0250 0.0000 21 | 0.0500 0.0000 22 | 0.0750 0.0000 23 | 0.1000 0.0000 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0000 31 | 0.8000 0.0000 32 | 0.9000 0.0000 33 | 0.9500 0.0000 34 | 1.0000 0.0065 35 | -------------------------------------------------------------------------------- /f/fg4.dat: -------------------------------------------------------------------------------- 1 | Fage & Collins 4 2 | 1.0000 0.0075 3 | 0.9500 0.0300 4 | 0.9000 0.0423 5 | 0.8000 0.0668 6 | 0.7000 0.0860 7 | 0.6000 0.1020 8 | 0.5000 0.1151 9 | 0.4000 0.1244 10 | 0.3000 0.1270 11 | 0.2000 0.1218 12 | 0.1500 0.1145 13 | 0.1000 0.1020 14 | 0.0750 0.0925 15 | 0.0500 0.0794 16 | 0.0250 0.0655 17 | 0.0125 0.0480 18 | 0.0000 0.0200 19 | 0.0125 0.0015 20 | 0.0250 0.0000 21 | 0.0500 0.0000 22 | 0.0750 0.0000 23 | 0.1000 0.0000 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0000 31 | 0.8000 0.0000 32 | 0.9000 0.0000 33 | 0.9500 0.0000 34 | 1.0000 0.0075 35 | -------------------------------------------------------------------------------- /n/n12.dat: -------------------------------------------------------------------------------- 1 | N-12 2 | 1.0000 0.0000 3 | 0.9500 0.0086 4 | 0.9000 0.0138 5 | 0.8000 0.0242 6 | 0.7000 0.0340 7 | 0.6000 0.0418 8 | 0.5000 0.0480 9 | 0.4000 0.0520 10 | 0.3000 0.0528 11 | 0.2000 0.0508 12 | 0.1500 0.0472 13 | 0.1000 0.0392 14 | 0.0750 0.0352 15 | 0.0500 0.0292 16 | 0.0250 0.0210 17 | 0.0125 0.0154 18 | 0.0000 0.0000 19 | 0.0125 -0.0152 20 | 0.0250 -0.0200 21 | 0.0500 -0.0280 22 | 0.0750 -0.0348 23 | 0.1000 -0.0386 24 | 0.1500 -0.0440 25 | 0.2000 -0.0480 26 | 0.3000 -0.0518 27 | 0.4000 -0.0500 28 | 0.5000 -0.0470 29 | 0.6000 -0.0418 30 | 0.7000 -0.0340 31 | 0.8000 -0.0246 32 | 0.9000 -0.0134 33 | 0.9500 -0.0080 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /n/n13.dat: -------------------------------------------------------------------------------- 1 | N-13 2 | 1.0000 0.0000 3 | 0.9500 0.0102 4 | 0.9000 0.0160 5 | 0.8000 0.0302 6 | 0.7000 0.0400 7 | 0.6000 0.0486 8 | 0.5000 0.0552 9 | 0.4000 0.0580 10 | 0.3000 0.0584 11 | 0.2000 0.0546 12 | 0.1500 0.0504 13 | 0.1000 0.0438 14 | 0.0750 0.0390 15 | 0.0500 0.0328 16 | 0.0250 0.0238 17 | 0.0125 0.0166 18 | 0.0000 0.0000 19 | 0.0125 -0.0154 20 | 0.0250 -0.0228 21 | 0.0500 -0.0318 22 | 0.0750 -0.0392 23 | 0.1000 -0.0434 24 | 0.1500 -0.0504 25 | 0.2000 -0.0548 26 | 0.3000 -0.0596 27 | 0.4000 -0.0590 28 | 0.5000 -0.0552 29 | 0.6000 -0.0482 30 | 0.7000 -0.0388 31 | 0.8000 -0.0286 32 | 0.9000 -0.0160 33 | 0.9500 -0.0080 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /n/n14.dat: -------------------------------------------------------------------------------- 1 | N-14 2 | 1.0000 0.0000 3 | 0.9500 0.0086 4 | 0.9000 0.0158 5 | 0.8000 0.0286 6 | 0.7000 0.0404 7 | 0.6000 0.0490 8 | 0.5000 0.0548 9 | 0.4000 0.0576 10 | 0.3000 0.0578 11 | 0.2000 0.0550 12 | 0.1500 0.0506 13 | 0.1000 0.0440 14 | 0.0750 0.0394 15 | 0.0500 0.0326 16 | 0.0250 0.0240 17 | 0.0125 0.0170 18 | 0.0000 0.0000 19 | 0.0125 -0.0180 20 | 0.0250 -0.0246 21 | 0.0500 -0.0334 22 | 0.0750 -0.0400 23 | 0.1000 -0.0436 24 | 0.1500 -0.0500 25 | 0.2000 -0.0540 26 | 0.3000 -0.0570 27 | 0.4000 -0.0568 28 | 0.5000 -0.0540 29 | 0.6000 -0.0484 30 | 0.7000 -0.0400 31 | 0.8000 -0.0287 32 | 0.9000 -0.0156 33 | 0.9500 -0.0084 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /c/cootie.dat: -------------------------------------------------------------------------------- 1 | WACO COOTIE AIRFOIL 2 | 1.000000 0.005000 3 | 0.950000 0.017000 4 | 0.900000 0.028000 5 | 0.800000 0.050000 6 | 0.700000 0.070000 7 | 0.600000 0.085000 8 | 0.500000 0.097000 9 | 0.400000 0.103600 10 | 0.300000 0.103600 11 | 0.200000 0.095600 12 | 0.150000 0.086400 13 | 0.100000 0.073000 14 | 0.075000 0.064000 15 | 0.050000 0.053800 16 | 0.025000 0.039400 17 | 0.012500 0.029000 18 | 0.000000 0.011000 19 | 0.012500 0.001000 20 | 0.025000 0.000000 21 | 0.050000 0.000000 22 | 0.075000 0.002600 23 | 0.100000 0.006400 24 | 0.150000 0.012000 25 | 0.200000 0.015000 26 | 0.300000 0.019000 27 | 0.400000 0.022000 28 | 0.500000 0.021200 29 | 0.600000 0.016400 30 | 0.700000 0.012400 31 | 0.800000 0.008400 32 | 0.900000 0.004000 33 | 0.950000 0.002000 34 | 1.000000 0.000000 35 | -------------------------------------------------------------------------------- /e/eiffel371.dat: -------------------------------------------------------------------------------- 1 | Eiffel 371 (Monge) 2 | 1.0000 0.0395 3 | 0.9500 0.0522 4 | 0.9000 0.0638 5 | 0.8000 0.0855 6 | 0.7000 0.1033 7 | 0.6000 0.1188 8 | 0.5000 0.1322 9 | 0.4000 0.1421 10 | 0.3000 0.1447 11 | 0.2000 0.1395 12 | 0.1500 0.1320 13 | 0.1000 0.1195 14 | 0.0750 0.1110 15 | 0.0500 0.0983 16 | 0.0250 0.0800 17 | 0.0125 0.0660 18 | 0.0000 0.0395 19 | 0.0125 0.0304 20 | 0.0250 0.0260 21 | 0.0500 0.0200 22 | 0.0750 0.0162 23 | 0.1000 0.0132 24 | 0.1500 0.0088 25 | 0.2000 0.0053 26 | 0.3000 0.0007 27 | 0.4000 0.0013 28 | 0.5000 0.0046 29 | 0.6000 0.0099 30 | 0.7000 0.0045 31 | 0.8000 0.0224 32 | 0.9000 0.0288 33 | 0.9500 0.0345 34 | 1.0000 0.0395 35 | -------------------------------------------------------------------------------- /g/glennmartin2.dat: -------------------------------------------------------------------------------- 1 | Glenn Martin 2 2 | 1.0000 0.0082 3 | 0.9500 0.0265 4 | 0.9000 0.0423 5 | 0.8000 0.0709 6 | 0.7000 0.0947 7 | 0.6000 0.1128 8 | 0.5000 0.1289 9 | 0.4000 0.1377 10 | 0.3000 0.1423 11 | 0.2000 0.1383 12 | 0.1500 0.1280 13 | 0.1000 0.1116 14 | 0.0750 0.0995 15 | 0.0500 0.0829 16 | 0.0250 0.0597 17 | 0.0125 0.0440 18 | 0.0000 0.0193 19 | 0.0125 0.0083 20 | 0.0250 0.0043 21 | 0.0500 0.0006 22 | 0.0750 0.0000 23 | 0.1000 0.0000 24 | 0.1500 0.0005 25 | 0.2000 0.0036 26 | 0.3000 0.0110 27 | 0.4000 0.0114 28 | 0.5000 0.0092 29 | 0.6000 0.0035 30 | 0.7000 0.0007 31 | 0.8000 0.0000 32 | 0.9000 0.0017 33 | 0.9500 0.0035 34 | 1.0000 0.0082 35 | -------------------------------------------------------------------------------- /g/glennmartin3.dat: -------------------------------------------------------------------------------- 1 | Glenn Martin 3 2 | 1.0000 0.0191 3 | 0.9500 0.0475 4 | 0.9000 0.0646 5 | 0.8000 0.0889 6 | 0.7000 0.1084 7 | 0.6000 0.1216 8 | 0.5000 0.1309 9 | 0.4000 0.1356 10 | 0.3000 0.1378 11 | 0.2000 0.1331 12 | 0.1500 0.1270 13 | 0.1000 0.1149 14 | 0.0750 0.1045 15 | 0.0500 0.0905 16 | 0.0250 0.0705 17 | 0.0125 0.0568 18 | 0.0000 0.0245 19 | 0.0125 0.0140 20 | 0.0250 0.0105 21 | 0.0500 0.0067 22 | 0.0750 0.0045 23 | 0.1000 0.0023 24 | 0.1500 0.0015 25 | 0.2000 0.0013 26 | 0.3000 0.0001 27 | 0.4000 0.0000 28 | 0.5000 0.0006 29 | 0.6000 0.0000 30 | 0.7000 0.0000 31 | 0.8000 0.0006 32 | 0.9000 0.0027 33 | 0.9500 0.0050 34 | 1.0000 0.0191 35 | -------------------------------------------------------------------------------- /n/nacam12rev.dat: -------------------------------------------------------------------------------- 1 | NACA M12 2 | 1.0000 0.0020 3 | 0.9500 0.0107 4 | 0.9000 0.0189 5 | 0.8000 0.0350 6 | 0.7000 0.0498 7 | 0.6000 0.0627 8 | 0.5000 0.0725 9 | 0.4000 0.0786 10 | 0.3000 0.0795 11 | 0.2000 0.0730 12 | 0.1500 0.0661 13 | 0.1000 0.0559 14 | 0.0750 0.0489 15 | 0.0500 0.0401 16 | 0.0250 0.0286 17 | 0.0125 0.0203 18 | 0.0000 0.0000 19 | 0.0125 -0.0165 20 | 0.0250 -0.0214 21 | 0.0500 -0.0272 22 | 0.0750 -0.0307 23 | 0.1000 -0.0331 24 | 0.1500 -0.0360 25 | 0.2000 -0.0380 26 | 0.3000 -0.0398 27 | 0.4000 -0.0396 28 | 0.5000 -0.0382 29 | 0.6000 -0.0350 30 | 0.7000 -0.0300 31 | 0.8000 -0.0231 32 | 0.9000 -0.0137 33 | 0.9500 -0.0081 34 | 1.0000 -0.0020 -------------------------------------------------------------------------------- /z/zagi08.dat: -------------------------------------------------------------------------------- 1 | ZAGI 08 2 | 1.00000 0.00000 3 | 0.95000 0.00490 4 | 0.90000 0.00977 5 | 0.80000 0.01960 6 | 0.70000 0.02950 7 | 0.60000 0.03880 8 | 0.50000 0.04670 9 | 0.40000 0.05180 10 | 0.30000 0.05310 11 | 0.20000 0.04860 12 | 0.15000 0.04350 13 | 0.10000 0.03590 14 | 0.07500 0.03080 15 | 0.05000 0.02470 16 | 0.02500 0.01660 17 | 0.01250 0.01110 18 | 0.00000 0.00000 19 | 0.01250 -0.00850 20 | 0.02500 -0.01190 21 | 0.05000 -0.01610 22 | 0.07500 -0.01870 23 | 0.10000 -0.02050 24 | 0.15000 -0.02310 25 | 0.20000 -0.02470 26 | 0.30000 -0.02640 27 | 0.40000 -0.02720 28 | 0.50000 -0.02680 29 | 0.60000 -0.02560 30 | 0.70000 -0.02280 31 | 0.80000 -0.01830 32 | 0.90000 -0.01120 33 | 0.95000 -0.00650 34 | 1.00000 0.00000 35 | 36 | http://perso.wanadoo.fr/scherrer/matthieu/fwairf.html -------------------------------------------------------------------------------- /d/daytonwright6.dat: -------------------------------------------------------------------------------- 1 | Dayton-Wright 6 2 | 1.0000 0.0057 3 | 0.9500 0.0230 4 | 0.9000 0.0377 5 | 0.8000 0.0637 6 | 0.7000 0.0882 7 | 0.6000 0.1075 8 | 0.5000 0.1230 9 | 0.4000 0.1350 10 | 0.3000 0.1397 11 | 0.2000 0.1340 12 | 0.1500 0.1245 13 | 0.1000 0.1088 14 | 0.0750 0.0978 15 | 0.0500 0.0838 16 | 0.0250 0.0647 17 | 0.0125 0.0522 18 | 0.0000 0.0308 19 | 0.0125 0.0127 20 | 0.0250 0.0083 21 | 0.0500 0.0033 22 | 0.0750 0.0013 23 | 0.1000 0.0005 24 | 0.1500 0.0007 25 | 0.2000 0.0017 26 | 0.3000 0.0037 27 | 0.4000 0.0045 28 | 0.5000 0.0030 29 | 0.6000 0.0015 30 | 0.7000 0.0003 31 | 0.8000 0.0003 32 | 0.9000 0.0012 33 | 0.9500 0.0020 34 | 1.0000 0.0057 35 | -------------------------------------------------------------------------------- /d/daytonwrightt1.dat: -------------------------------------------------------------------------------- 1 | Dayton-Wright T-1 2 | 1.0000 0.0070 3 | 0.9500 0.0233 4 | 0.9000 0.0388 5 | 0.8000 0.0673 6 | 0.7000 0.0916 7 | 0.6000 0.1107 8 | 0.5000 0.1252 9 | 0.4000 0.1344 10 | 0.3000 0.1373 11 | 0.2000 0.1325 12 | 0.1500 0.1251 13 | 0.1000 0.1111 14 | 0.0750 0.1017 15 | 0.0500 0.0900 16 | 0.0250 0.0734 17 | 0.0125 0.0621 18 | 0.0000 0.0404 19 | 0.0125 0.0200 20 | 0.0250 0.0141 21 | 0.0500 0.0074 22 | 0.0750 0.0038 23 | 0.1000 0.0017 24 | 0.1500 0.0000 25 | 0.2000 0.0002 26 | 0.3000 0.0036 27 | 0.4000 0.0068 28 | 0.5000 0.0065 29 | 0.6000 0.0036 30 | 0.7000 0.0003 31 | 0.8000 0.0000 32 | 0.9000 0.0016 33 | 0.9500 0.0026 34 | 1.0000 0.0049 35 | -------------------------------------------------------------------------------- /e/eiffel385.dat: -------------------------------------------------------------------------------- 1 | Eiffel 385 (S.T. Ae) 2 | 1.0000 0.0000 3 | 0.9500 0.0165 4 | 0.9000 0.0313 5 | 0.8000 0.0590 6 | 0.7000 0.0833 7 | 0.6000 0.1042 8 | 0.5000 0.1229 9 | 0.4000 0.1354 10 | 0.3000 0.1403 11 | 0.2000 0.1363 12 | 0.1500 0.1290 13 | 0.1000 0.1167 14 | 0.0750 0.1085 15 | 0.0500 0.0980 16 | 0.0250 0.0850 17 | 0.0125 0.0749 18 | 0.0000 0.0521 19 | 0.0125 0.0303 20 | 0.0250 0.0225 21 | 0.0500 0.0125 22 | 0.0750 0.0065 23 | 0.1000 0.0035 24 | 0.1500 0.0005 25 | 0.2000 0.0028 26 | 0.3000 0.0083 27 | 0.4000 0.0153 28 | 0.5000 0.0174 29 | 0.6000 0.0174 30 | 0.7000 0.0160 31 | 0.8000 0.0125 32 | 0.9000 0.0069 33 | 0.9500 0.0025 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /e/eiffel428.dat: -------------------------------------------------------------------------------- 1 | Eiffel 428 (Bleriot) 2 | 1.0000 0.0000 3 | 0.9500 0.0115 4 | 0.9000 0.0210 5 | 0.8000 0.0400 6 | 0.7000 0.0580 7 | 0.6000 0.0750 8 | 0.5000 0.0880 9 | 0.4000 0.0950 10 | 0.3000 0.0950 11 | 0.2000 0.0850 12 | 0.1500 0.0777 13 | 0.1000 0.0650 14 | 0.0750 0.0602 15 | 0.0500 0.0480 16 | 0.0250 0.0375 17 | 0.0125 0.0310 18 | 0.0000 0.0150 19 | 0.0125 0.0028 20 | 0.0250 0.0000 21 | 0.0500 0.0000 22 | 0.0750 0.0000 23 | 0.1000 0.0000 24 | 0.1500 0.0000 25 | 0.2000 0.0020 26 | 0.3000 0.0055 27 | 0.4000 0.0070 28 | 0.5000 0.0080 29 | 0.6000 0.0080 30 | 0.7000 0.0070 31 | 0.8000 0.0050 32 | 0.9000 0.0020 33 | 0.9500 0.0000 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /e/eiffel430.dat: -------------------------------------------------------------------------------- 1 | Eiffel 430 (Lachassgne) 2 | 1.0000 0.0050 3 | 0.9500 0.0169 4 | 0.9000 0.0280 5 | 0.8000 0.0510 6 | 0.7000 0.0700 7 | 0.6000 0.0860 8 | 0.5000 0.1020 9 | 0.4000 0.1100 10 | 0.3000 0.1020 11 | 0.2000 0.1060 12 | 0.1500 0.1017 13 | 0.1000 0.0910 14 | 0.0750 0.0848 15 | 0.0500 0.0757 16 | 0.0250 0.0621 17 | 0.0125 0.0509 18 | 0.0000 0.0270 19 | 0.0125 0.0090 20 | 0.0250 0.0042 21 | 0.0500 0.0014 22 | 0.0750 0.0000 23 | 0.1000 0.0010 24 | 0.1500 0.0048 25 | 0.2000 0.0120 26 | 0.3000 0.0160 27 | 0.4000 0.0160 28 | 0.5000 0.0140 29 | 0.6000 0.0110 30 | 0.7000 0.0060 31 | 0.8000 0.0030 32 | 0.9000 0.0000 33 | 0.9500 0.0014 34 | 1.0000 0.0050 35 | -------------------------------------------------------------------------------- /g/glennmartin4.dat: -------------------------------------------------------------------------------- 1 | Glenn Martin 4 2 | 1.0000 0.0140 3 | 0.9500 0.0558 4 | 0.9000 0.0752 5 | 0.8000 0.0993 6 | 0.7000 0.1180 7 | 0.6000 0.1322 8 | 0.5000 0.1439 9 | 0.4000 0.1525 10 | 0.3000 0.1542 11 | 0.2000 0.1460 12 | 0.1500 0.1340 13 | 0.1000 0.1144 14 | 0.0750 0.1000 15 | 0.0500 0.0798 16 | 0.0250 0.0581 17 | 0.0125 0.0450 18 | 0.0000 0.0185 19 | 0.0125 0.0085 20 | 0.0250 0.0051 21 | 0.0500 0.0013 22 | 0.0750 0.0010 23 | 0.1000 0.0001 24 | 0.1500 0.0000 25 | 0.2000 -0.0001 26 | 0.3000 -0.0007 27 | 0.4000 0.0001 28 | 0.5000 0.0006 29 | 0.6000 0.0013 30 | 0.7000 0.0043 31 | 0.8000 0.0061 32 | 0.9000 0.0092 33 | 0.9500 0.0098 34 | 1.0000 0.0140 35 | -------------------------------------------------------------------------------- /m/m7.dat: -------------------------------------------------------------------------------- 1 | NACA M7 AIRFOIL 2 | 1.0000000 0.0047000 3 | 0.9000000 0.0094200 4 | 0.8000000 0.0207400 5 | 0.7000000 0.0358600 6 | 0.6000000 0.0519800 7 | 0.5000000 0.0666000 8 | 0.4000000 0.0772200 9 | 0.3000000 0.0809400 10 | 0.2000000 0.0747600 11 | 0.1500000 0.0669200 12 | 0.1000000 0.0554800 13 | 0.0750000 0.0477100 14 | 0.0500000 0.0385400 15 | 0.0250000 0.0273700 16 | 0.0125000 0.0203300 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0001600 19 | 0.0250000 0.0000700 20 | 0.0500000 0.0025400 21 | 0.0750000 0.0055100 22 | 0.1000000 0.0075800 23 | 0.1500000 0.0138200 24 | 0.2000000 0.0171600 25 | 0.3000000 0.0191400 26 | 0.4000000 0.0153200 27 | 0.5000000 0.0087000 28 | 0.6000000 0.0005800 29 | 0.7000000 -.0065400 30 | 0.8000000 -.0105600 31 | 0.9000000 -.0088800 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /n/nacam12.dat: -------------------------------------------------------------------------------- 1 | NACA M12 2 | 1.0000 0.0020 3 | 0.9500 0.0107 4 | 0.9000 0.0189 5 | 0.8000 0.0350 6 | 0.7000 0.0498 7 | 0.6000 0.0627 8 | 0.5000 0.0725 9 | 0.4000 0.0786 10 | 0.3000 0.0795 11 | 0.2000 0.0730 12 | 0.1500 0.0661 13 | 0.1000 0.0559 14 | 0.0750 0.0489 15 | 0.0500 0.0401 16 | 0.0250 0.0286 17 | 0.0125 0.0203 18 | 0.0000 0.0000 19 | 0.0125 -0.0165 20 | 0.0250 -0.0214 21 | 0.0500 -0.0272 22 | 0.0750 -0.0307 23 | 0.1000 -0.0331 24 | 0.1500 -0.0300 25 | 0.2000 -0.0380 26 | 0.3000 -0.0398 27 | 0.4000 -0.0396 28 | 0.5000 -0.0382 29 | 0.6000 -0.0350 30 | 0.7000 -0.0300 31 | 0.8000 -0.0231 32 | 0.9000 -0.0137 33 | 0.9500 -0.0081 34 | 1.0000 -0.0020 35 | -------------------------------------------------------------------------------- /n/nacam2.dat: -------------------------------------------------------------------------------- 1 | NACA M2 2 | 1.0000 0.0020 3 | 0.9500 0.0069 4 | 0.9000 0.0115 5 | 0.8000 0.0199 6 | 0.7000 0.0271 7 | 0.6000 0.0330 8 | 0.5000 0.0374 9 | 0.4000 0.0400 10 | 0.3000 0.0403 11 | 0.2000 0.0378 12 | 0.1500 0.0349 13 | 0.1000 0.0305 14 | 0.0750 0.0274 15 | 0.0500 0.0233 16 | 0.0250 0.0174 17 | 0.0125 0.0130 18 | 0.0000 0.0000 19 | 0.0125 -0.0130 20 | 0.0250 -0.0174 21 | 0.0500 -0.0233 22 | 0.0750 -0.0274 23 | 0.1000 -0.0305 24 | 0.1500 -0.0349 25 | 0.2000 -0.0378 26 | 0.3000 -0.0403 27 | 0.4000 -0.0400 28 | 0.5000 -0.0374 29 | 0.6000 -0.0330 30 | 0.7000 -0.0271 31 | 0.8000 -0.0199 32 | 0.9000 -0.0115 33 | 0.9500 -0.0069 34 | 1.0000 -0.0020 35 | -------------------------------------------------------------------------------- /n/nacam3.dat: -------------------------------------------------------------------------------- 1 | NACA M3 2 | 1.0000 0.0020 3 | 0.9500 0.0093 4 | 0.9000 0.0162 5 | 0.8000 0.0288 6 | 0.7000 0.0396 7 | 0.6000 0.0485 8 | 0.5000 0.0550 9 | 0.4000 0.0589 10 | 0.3000 0.0595 11 | 0.2000 0.0557 12 | 0.1500 0.0514 13 | 0.1000 0.0447 14 | 0.0750 0.0400 15 | 0.0500 0.0339 16 | 0.0250 0.0251 17 | 0.0125 0.0186 18 | 0.0000 0.0000 19 | 0.0125 -0.0186 20 | 0.0250 -0.0251 21 | 0.0500 -0.0339 22 | 0.0750 -0.0400 23 | 0.1000 -0.0447 24 | 0.1500 -0.0514 25 | 0.2000 -0.0557 26 | 0.3000 -0.0595 27 | 0.4000 -0.0589 28 | 0.5000 -0.0550 29 | 0.6000 -0.0485 30 | 0.7000 -0.0396 31 | 0.8000 -0.0288 32 | 0.9000 -0.0162 33 | 0.9500 -0.0093 34 | 1.0000 -0.0020 35 | -------------------------------------------------------------------------------- /r/r23012.dat: -------------------------------------------------------------------------------- 1 | Ritz 2-30-12 de profils MRA 2 | 1.000000 0.000000 3 | 0.950200 0.008500 4 | 0.873100 0.021000 5 | 0.759700 0.039400 6 | 0.627400 0.056800 7 | 0.506200 0.069500 8 | 0.397300 0.076700 9 | 0.308500 0.079700 10 | 0.233600 0.076900 11 | 0.169300 0.070000 12 | 0.113800 0.059000 13 | 0.068100 0.045600 14 | 0.035500 0.031300 15 | 0.009900 0.015500 16 | 0.002900 0.008300 17 | 0.001100 0.005500 18 | 0.000000 0.000000 19 | 0.003400 -0.006100 20 | 0.010700 -0.011900 21 | 0.023000 -0.018200 22 | 0.047000 -0.025300 23 | 0.086400 -0.031700 24 | 0.165900 -0.038100 25 | 0.266100 -0.039700 26 | 0.386200 -0.037600 27 | 0.529400 -0.031600 28 | 0.676300 -0.023000 29 | 0.818600 -0.013100 30 | 0.915100 -0.006900 31 | 0.976800 -0.001900 32 | 1.000000 0.000000 33 | Epaisseur relative 11.73 34 | -------------------------------------------------------------------------------- /r/rhodesg30.dat: -------------------------------------------------------------------------------- 1 | Rhode St. Genese 30 2 | 1.0000 0.0000 3 | 0.9500 0.0105 4 | 0.9000 0.0203 5 | 0.8000 0.0405 6 | 0.7000 0.0585 7 | 0.6000 0.0735 8 | 0.5000 0.0855 9 | 0.4000 0.0930 10 | 0.3000 0.0974 11 | 0.2000 0.0960 12 | 0.1500 0.0890 13 | 0.1000 0.0787 14 | 0.0750 0.0720 15 | 0.0500 0.0623 16 | 0.0250 0.0510 17 | 0.0125 0.0435 18 | 0.0000 0.0241 19 | 0.0125 0.0145 20 | 0.0250 0.0059 21 | 0.0500 0.0030 22 | 0.0750 0.0015 23 | 0.1000 0.0000 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0000 31 | 0.8000 0.0000 32 | 0.9000 0.0000 33 | 0.9500 0.0000 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /r/rhodesg32.dat: -------------------------------------------------------------------------------- 1 | Rhode St. Genese 32 2 | 1.0000 0.0000 3 | 0.9500 0.0128 4 | 0.9000 0.0248 5 | 0.8000 0.0495 6 | 0.7000 0.0715 7 | 0.6000 0.0898 8 | 0.5000 0.1045 9 | 0.4000 0.1137 10 | 0.3000 0.1190 11 | 0.2000 0.1178 12 | 0.1500 0.1085 13 | 0.1000 0.0962 14 | 0.0750 0.0880 15 | 0.0500 0.0762 16 | 0.0250 0.0623 17 | 0.0125 0.0525 18 | 0.0000 0.0293 19 | 0.0125 0.0130 20 | 0.0250 0.0072 21 | 0.0500 0.0037 22 | 0.0750 0.0019 23 | 0.1000 0.0000 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0000 31 | 0.8000 0.0000 32 | 0.9000 0.0000 33 | 0.9500 0.0000 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /r/rhodesg34.dat: -------------------------------------------------------------------------------- 1 | Rhode St. Genese 34 2 | 1.0000 0.0000 3 | 0.9500 0.0152 4 | 0.9000 0.0293 5 | 0.8000 0.0565 6 | 0.7000 0.0845 7 | 0.6000 0.1061 8 | 0.5000 0.1235 9 | 0.4000 0.1343 10 | 0.3000 0.1407 11 | 0.2000 0.1386 12 | 0.1500 0.1285 13 | 0.1000 0.1137 14 | 0.0750 0.1040 15 | 0.0500 0.0896 16 | 0.0250 0.0737 17 | 0.0125 0.0620 18 | 0.0000 0.0347 19 | 0.0125 0.0140 20 | 0.0250 0.0086 21 | 0.0500 0.0044 22 | 0.0750 0.0022 23 | 0.1000 0.0000 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0000 31 | 0.8000 0.0000 32 | 0.9000 0.0000 33 | 0.9500 0.0000 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /r/rhodesg36.dat: -------------------------------------------------------------------------------- 1 | Rhode St. Genese 36 2 | 1.0000 0.0000 3 | 0.9500 0.0126 4 | 0.9000 0.0338 5 | 0.8000 0.0675 6 | 0.7000 0.0975 7 | 0.6000 0.1224 8 | 0.5000 0.1429 9 | 0.4000 0.1550 10 | 0.3000 0.1623 11 | 0.2000 0.1599 12 | 0.1500 0.1495 13 | 0.1000 0.1313 14 | 0.0750 0.1195 15 | 0.0500 0.1037 16 | 0.0250 0.0850 17 | 0.0125 0.0710 18 | 0.0000 0.0400 19 | 0.0125 0.0165 20 | 0.0250 0.0099 21 | 0.0500 0.0050 22 | 0.0750 0.0026 23 | 0.1000 0.0000 24 | 0.1500 0.0000 25 | 0.2000 0.0000 26 | 0.3000 0.0000 27 | 0.4000 0.0000 28 | 0.5000 0.0000 29 | 0.6000 0.0000 30 | 0.7000 0.0000 31 | 0.8000 0.0000 32 | 0.9000 0.0000 33 | 0.9500 0.0000 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /z/zagi10.dat: -------------------------------------------------------------------------------- 1 | ZAGI 10 2 | 1.00000 0.00000 3 | 0.95000 0.00590 4 | 0.90000 0.01201 5 | 0.80000 0.02471 6 | 0.70000 0.03782 7 | 0.60000 0.05014 8 | 0.50000 0.06072 9 | 0.40000 0.06729 10 | 0.30000 0.06957 11 | 0.20000 0.06373 12 | 0.15000 0.05695 13 | 0.10000 0.04681 14 | 0.07500 0.04010 15 | 0.05000 0.03208 16 | 0.02500 0.02129 17 | 0.01250 0.01417 18 | 0.00000 0.00000 19 | 0.01250 -0.01029 20 | 0.02500 -0.01428 21 | 0.05000 -0.01868 22 | 0.07500 -0.02160 23 | 0.10000 -0.02382 24 | 0.15000 -0.02645 25 | 0.20000 -0.02794 26 | 0.30000 -0.02978 27 | 0.40000 -0.03099 28 | 0.50000 -0.03112 29 | 0.60000 -0.03044 30 | 0.70000 -0.02772 31 | 0.80000 -0.02271 32 | 0.90000 -0.01421 33 | 0.95000 -0.00830 34 | 1.00000 0.00000 35 | 36 | http://perso.wanadoo.fr/scherrer/matthieu/fwairf.html 37 | -------------------------------------------------------------------------------- /z/zagi12.dat: -------------------------------------------------------------------------------- 1 | ZAGI 12 2 | 1.00000 0.00000 3 | 0.95000 0.00730 4 | 0.90000 0.01460 5 | 0.80000 0.02940 6 | 0.70000 0.04430 7 | 0.60000 0.05810 8 | 0.50000 0.06980 9 | 0.40000 0.07700 10 | 0.30000 0.07940 11 | 0.20000 0.07280 12 | 0.15000 0.06520 13 | 0.10000 0.05380 14 | 0.07500 0.04620 15 | 0.05000 0.03710 16 | 0.02500 0.02480 17 | 0.01250 0.01660 18 | 0.00000 0.00000 19 | 0.01250 -0.01270 20 | 0.02500 -0.01780 21 | 0.05000 -0.02370 22 | 0.07500 -0.02770 23 | 0.10000 -0.03080 24 | 0.15000 -0.03470 25 | 0.20000 -0.03700 26 | 0.30000 -0.03960 27 | 0.40000 -0.04070 28 | 0.50000 -0.04020 29 | 0.60000 -0.03840 30 | 0.70000 -0.03420 31 | 0.80000 -0.02740 32 | 0.90000 -0.01680 33 | 0.95000 -0.00970 34 | 1.00000 0.00000 35 | 36 | http://perso.wanadoo.fr/scherrer/matthieu/fwairf.html 37 | -------------------------------------------------------------------------------- /a/ah6407.dat: -------------------------------------------------------------------------------- 1 | AH-6-40-7 AIRFOIL 2 | 1.0000000 0.0035000 3 | 0.8998800 0.0270500 4 | 0.7997900 0.0466000 5 | 0.6997200 0.0621500 6 | 0.5996700 0.0737000 7 | 0.4996300 0.0812500 8 | 0.3996200 0.0848000 9 | 0.2996200 0.0843500 10 | 0.1996500 0.0779000 11 | 0.1496800 0.0706700 12 | 0.0997400 0.0584500 13 | 0.0747700 0.0503400 14 | 0.0498200 0.0402200 15 | 0.0248800 0.0271100 16 | 0.0124200 0.0180600 17 | 0.0000000 0.0000000 18 | 0.0125300 -.0069400 19 | 0.0250400 -.0078900 20 | 0.0500300 -.0067700 21 | 0.0750200 -.0051600 22 | 0.1000100 -.0025500 23 | 0.1499900 0.0031700 24 | 0.1999600 0.0094000 25 | 0.2999100 0.0193500 26 | 0.3998800 0.0258000 27 | 0.4998700 0.0282500 28 | 0.5998700 0.0287000 29 | 0.6998900 0.0251500 30 | 0.7999200 0.0186000 31 | 0.8999600 0.0090500 32 | 1.0000000 -.0035000 33 | -------------------------------------------------------------------------------- /a/ah7476.dat: -------------------------------------------------------------------------------- 1 | AH-7-47-6 AIRFOIL 2 | 1.0000000 0.0035000 3 | 0.8998500 0.0340500 4 | 0.7997500 0.0546000 5 | 0.6996800 0.0706500 6 | 0.5996400 0.0807000 7 | 0.4996100 0.0862500 8 | 0.3996000 0.0878000 9 | 0.2996100 0.0858500 10 | 0.1996600 0.0759000 11 | 0.1497000 0.0676700 12 | 0.0997500 0.0564500 13 | 0.0747800 0.0488400 14 | 0.0498200 0.0392200 15 | 0.0248800 0.0271100 16 | 0.0124200 0.0180600 17 | 0.0000000 0.0000000 18 | 0.0125400 -.0079400 19 | 0.0250300 -.0058900 20 | 0.0500100 -.0032700 21 | 0.0750000 0.0003400 22 | 0.0999800 0.0034500 23 | 0.1499500 0.0106700 24 | 0.1999200 0.0169000 25 | 0.2998800 0.0273500 26 | 0.3998500 0.0343000 27 | 0.4998300 0.0377500 28 | 0.5998300 0.0387000 29 | 0.6998400 0.0361500 30 | 0.7998700 0.0291000 31 | 0.8999299 0.0160500 32 | 1.0000000 -.0035000 33 | -------------------------------------------------------------------------------- /d/dga1182.dat: -------------------------------------------------------------------------------- 1 | D.G.A. 1182 2 | 1.0000 0.0030 3 | 0.9500 0.0075 4 | 0.9000 0.0125 5 | 0.8000 0.0210 6 | 0.7000 0.0290 7 | 0.6000 0.0350 8 | 0.5000 0.0400 9 | 0.4000 0.0430 10 | 0.3000 0.0430 11 | 0.2000 0.0400 12 | 0.1500 0.0265 13 | 0.1000 0.0310 14 | 0.0750 0.0280 15 | 0.0500 0.0250 16 | 0.0250 0.0190 17 | 0.0125 0.0140 18 | 0.0000 0.0000 19 | 0.0125 -0.0055 20 | 0.0250 -0.0080 21 | 0.0500 -0.0120 22 | 0.0750 -0.0150 23 | 0.1000 -0.0170 24 | 0.1500 -0.0195 25 | 0.2000 -0.0210 26 | 0.3000 -0.0330 27 | 0.4000 -0.0240 28 | 0.5000 -0.0230 29 | 0.6000 -0.0200 30 | 0.7000 -0.0175 31 | 0.8000 -0.0125 32 | 0.9000 -0.0050 33 | 0.9500 -0.0030 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /g/goe05k.dat: -------------------------------------------------------------------------------- 1 | GOE 5K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0080800 4 | 0.9000000 0.0138700 5 | 0.8000000 0.0231400 6 | 0.7000000 0.0294100 7 | 0.6000000 0.0329800 8 | 0.5000000 0.0338500 9 | 0.4000000 0.0329200 10 | 0.3000000 0.0299900 11 | 0.2000000 0.0249600 12 | 0.1500000 0.0216400 13 | 0.1000000 0.0173300 14 | 0.0750000 0.0146200 15 | 0.0500000 0.0116100 16 | 0.0250000 0.0078100 17 | 0.0000000 0.0000000 18 | 0.0250000 -.0034900 19 | 0.0500000 -.0038900 20 | 0.0750000 -.0041800 21 | 0.1000000 -.0042700 22 | 0.1500000 -.0045600 23 | 0.2000000 -.0044400 24 | 0.3000000 -.0040100 25 | 0.4000000 -.0035800 26 | 0.5000000 -.0031500 27 | 0.6000000 -.0027200 28 | 0.7000000 -.0022900 29 | 0.8000000 -.0018600 30 | 0.9000000 -.0014300 31 | 0.9500000 -.0012200 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe06k.dat: -------------------------------------------------------------------------------- 1 | GOE 6K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0162700 4 | 0.9000000 0.0279400 5 | 0.8000000 0.0467800 6 | 0.7000000 0.0594200 7 | 0.6000000 0.0668600 8 | 0.5000000 0.0685000 9 | 0.4000000 0.0665400 10 | 0.3000000 0.0607800 11 | 0.2000000 0.0506200 12 | 0.1500000 0.0436900 13 | 0.1000000 0.0349600 14 | 0.0750000 0.0295400 15 | 0.0500000 0.0234300 16 | 0.0250000 0.0157100 17 | 0.0000000 0.0000000 18 | 0.0250000 -.0070900 19 | 0.0500000 -.0079700 20 | 0.0750000 -.0085500 21 | 0.1000000 -.0088400 22 | 0.1500000 -.0093100 23 | 0.2000000 -.0090800 24 | 0.3000000 -.0082200 25 | 0.4000000 -.0073600 26 | 0.5000000 -.0065000 27 | 0.6000000 -.0056400 28 | 0.7000000 -.0047800 29 | 0.8000000 -.0039200 30 | 0.9000000 -.0030600 31 | 0.9500000 -.0026300 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe07k.dat: -------------------------------------------------------------------------------- 1 | GOE 7K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0237800 4 | 0.9000000 0.0409500 5 | 0.8000000 0.0686000 6 | 0.7000000 0.0871500 7 | 0.6000000 0.0980000 8 | 0.5000000 0.1004500 9 | 0.4000000 0.0975000 10 | 0.3000000 0.0891500 11 | 0.2000000 0.0741000 12 | 0.1500000 0.0641800 13 | 0.1000000 0.0513500 14 | 0.0750000 0.0433400 15 | 0.0500000 0.0344300 16 | 0.0250000 0.0231100 17 | 0.0000000 0.0000000 18 | 0.0250000 -.0102900 19 | 0.0500000 -.0116800 20 | 0.0750000 -.0124600 21 | 0.1000000 -.0129500 22 | 0.1500000 -.0136200 23 | 0.2000000 -.0133000 24 | 0.3000000 -.0120500 25 | 0.4000000 -.0108000 26 | 0.5000000 -.0095500 27 | 0.6000000 -.0083000 28 | 0.7000000 -.0070500 29 | 0.8000000 -.0058000 30 | 0.9000000 -.0045500 31 | 0.9500000 -.0039300 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe08k.dat: -------------------------------------------------------------------------------- 1 | GOE 8K AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0320500 4 | 0.9000000 0.0553100 5 | 0.8000000 0.0925200 6 | 0.7000000 0.1175300 7 | 0.6000000 0.1321400 8 | 0.5000000 0.1355500 9 | 0.4000000 0.1316600 10 | 0.3000000 0.1202700 11 | 0.2000000 0.1000800 12 | 0.1500000 0.0865300 13 | 0.1000000 0.0691900 14 | 0.0750000 0.0583700 15 | 0.0500000 0.0463500 16 | 0.0250000 0.0311200 17 | 0.0000000 0.0000000 18 | 0.0250000 -.0140800 19 | 0.0500000 -.0158600 20 | 0.0750000 -.0164300 21 | 0.1000000 -.0175100 22 | 0.1500000 -.0184700 23 | 0.2000000 -.0180200 24 | 0.3000000 -.0163300 25 | 0.4000000 -.0146400 26 | 0.5000000 -.0129500 27 | 0.6000000 -.0112600 28 | 0.7000000 -.0095700 29 | 0.8000000 -.0078800 30 | 0.9000000 -.0061900 31 | 0.9500000 -.0053500 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe101.dat: -------------------------------------------------------------------------------- 1 | GOE 101 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0153000 4 | 0.8000000 0.0296000 5 | 0.7000000 0.0424000 6 | 0.6000000 0.0542000 7 | 0.5000000 0.0640000 8 | 0.4000000 0.0713000 9 | 0.3000000 0.0741000 10 | 0.2000000 0.0674000 11 | 0.1500000 0.0605500 12 | 0.1000000 0.0507000 13 | 0.0750000 0.0435200 14 | 0.0500000 0.0353500 15 | 0.0250000 0.0231800 16 | 0.0125000 0.0150900 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0069100 19 | 0.0250000 -.0067300 20 | 0.0500000 -.0054500 21 | 0.0750000 -.0037700 22 | 0.1000000 -.0023000 23 | 0.1500000 0.0000500 24 | 0.2000000 0.0019000 25 | 0.3000000 0.0051000 26 | 0.4000000 0.0075000 27 | 0.5000000 0.0085000 28 | 0.6000000 0.0082000 29 | 0.7000000 0.0069000 30 | 0.8000000 0.0051000 31 | 0.9000000 0.0028000 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe113.dat: -------------------------------------------------------------------------------- 1 | GOE 113 AIRFOIL 2 | 1.0000000 0.0030000 3 | 0.9000000 0.0184000 4 | 0.8000000 0.0303000 5 | 0.7000000 0.0407000 6 | 0.6000000 0.0501000 7 | 0.5000000 0.0580000 8 | 0.4000000 0.0634000 9 | 0.3000000 0.0638000 10 | 0.2000000 0.0584000 11 | 0.1500000 0.0539000 12 | 0.1000000 0.0461000 13 | 0.0750000 0.0404500 14 | 0.0500000 0.0313000 15 | 0.0250000 0.0201500 16 | 0.0125000 0.0120700 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0059200 19 | 0.0250000 -.0058500 20 | 0.0500000 -.0057000 21 | 0.0750000 -.0053500 22 | 0.1000000 -.0050000 23 | 0.1500000 -.0043000 24 | 0.2000000 -.0038000 25 | 0.3000000 -.0027000 26 | 0.4000000 -.0016000 27 | 0.5000000 -.0010000 28 | 0.6000000 -.0004000 29 | 0.7000000 -.0003000 30 | 0.8000000 -.0002000 31 | 0.9000000 0.0001000 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe342.dat: -------------------------------------------------------------------------------- 1 | GOE 342 AIRFOIL 2 | 1.0000000 0.0030000 3 | 0.9000000 0.0262000 4 | 0.8000000 0.0464000 5 | 0.7000000 0.0636000 6 | 0.6000000 0.0778000 7 | 0.5000000 0.0850000 8 | 0.4000000 0.0872000 9 | 0.3000000 0.0854000 10 | 0.2000000 0.0786000 11 | 0.1500000 0.0702000 12 | 0.1000000 0.0578000 13 | 0.0750000 0.0506000 14 | 0.0500000 0.0414000 15 | 0.0250000 0.0292000 16 | 0.0125000 0.0201000 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0079000 19 | 0.0250000 -.0058000 20 | 0.0500000 0.0004000 21 | 0.0750000 0.0046000 22 | 0.1000000 0.0098000 23 | 0.1500000 0.0177000 24 | 0.2000000 0.0246000 25 | 0.3000000 0.0334000 26 | 0.4000000 0.0372000 27 | 0.5000000 0.0375000 28 | 0.6000000 0.0358000 29 | 0.7000000 0.0306000 30 | 0.8000000 0.0224000 31 | 0.9000000 0.0122000 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe411.dat: -------------------------------------------------------------------------------- 1 | GOE 411 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0180000 4 | 0.8000000 0.0320000 5 | 0.7000000 0.0440000 6 | 0.6000000 0.0530000 7 | 0.5000000 0.0605000 8 | 0.4000000 0.0655000 9 | 0.3000000 0.0660000 10 | 0.2000000 0.0605000 11 | 0.1500000 0.0550000 12 | 0.1000000 0.0460000 13 | 0.0750000 0.0388000 14 | 0.0500000 0.0305000 15 | 0.0250000 0.0184000 16 | 0.0125000 0.0115000 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0115000 19 | 0.0250000 -.0184000 20 | 0.0500000 -.0305000 21 | 0.0750000 -.0388000 22 | 0.1000000 -.0460000 23 | 0.1500000 -.0550000 24 | 0.2000000 -.0605000 25 | 0.3000000 -.0660000 26 | 0.4000000 -.0655000 27 | 0.5000000 -.0605000 28 | 0.6000000 -.0530000 29 | 0.7000000 -.0440000 30 | 0.8000000 -.0320000 31 | 0.9000000 -.0180000 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe484.dat: -------------------------------------------------------------------------------- 1 | GOE 484 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0248000 4 | 0.8000000 0.0441000 5 | 0.7000000 0.0598000 6 | 0.6000000 0.0697000 7 | 0.5000000 0.0765000 8 | 0.4000000 0.0793000 9 | 0.3000000 0.0751000 10 | 0.2000000 0.0654000 11 | 0.1500000 0.0578000 12 | 0.1000000 0.0467000 13 | 0.0750000 0.0399000 14 | 0.0500000 0.0321000 15 | 0.0250000 0.0233000 16 | 0.0125000 0.0171500 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0115500 19 | 0.0250000 -.0122000 20 | 0.0500000 -.0115000 21 | 0.0750000 -.0096000 22 | 0.1000000 -.0068000 23 | 0.1500000 -.0002000 24 | 0.2000000 0.0054000 25 | 0.3000000 0.0126000 26 | 0.4000000 0.0188000 27 | 0.5000000 0.0225000 28 | 0.6000000 0.0242000 29 | 0.7000000 0.0219000 30 | 0.8000000 0.0171000 31 | 0.9000000 0.0088000 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe488.dat: -------------------------------------------------------------------------------- 1 | GOE 488 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.8997200 0.0179500 4 | 0.7994800 0.0333900 5 | 0.6992800 0.0463400 6 | 0.5991500 0.0547900 7 | 0.4990600 0.0607400 8 | 0.3990200 0.0631800 9 | 0.2990200 0.0631300 10 | 0.1990700 0.0600900 11 | 0.1491500 0.0548100 12 | 0.0992800 0.0465400 13 | 0.0743700 0.0406500 14 | 0.0495000 0.0322700 15 | 0.0246600 0.0218800 16 | 0.0122900 0.0136900 17 | 0.0000000 0.0000000 18 | 0.0126900 -.0123000 19 | 0.0252300 -.0146100 20 | 0.0502400 -.0152200 21 | 0.0752300 -.0148300 22 | 0.1002200 -.0139500 23 | 0.1501700 -.0111700 24 | 0.2001200 -.0079000 25 | 0.3000400 -.0028500 26 | 0.4000400 -.0023000 27 | 0.5000400 -.0027500 28 | 0.6000500 -.0032000 29 | 0.7000600 -.0036500 30 | 0.8000600 -.0041000 31 | 0.9000300 -.0020500 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe533.dat: -------------------------------------------------------------------------------- 1 | GOE 533 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0238000 4 | 0.8000000 0.0456000 5 | 0.7000000 0.0654000 6 | 0.6000000 0.0837000 7 | 0.5000000 0.1005000 8 | 0.4000000 0.1113000 9 | 0.3000000 0.1146000 10 | 0.2000000 0.1069000 11 | 0.1500000 0.0968000 12 | 0.1000000 0.0822000 13 | 0.0750000 0.0709000 14 | 0.0500000 0.0576000 15 | 0.0250000 0.0410000 16 | 0.0125000 0.0289000 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0141000 19 | 0.0250000 -.0177000 20 | 0.0500000 -.0209000 21 | 0.0750000 -.0231000 22 | 0.1000000 -.0238000 23 | 0.1500000 -.0247000 24 | 0.2000000 -.0246000 25 | 0.3000000 -.0224000 26 | 0.4000000 -.0177000 27 | 0.5000000 -.0100000 28 | 0.6000000 -.0028000 29 | 0.7000000 0.0044000 30 | 0.8000000 0.0071000 31 | 0.9000000 0.0053000 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe565.dat: -------------------------------------------------------------------------------- 1 | GOE 565 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0183800 4 | 0.8000000 0.0347600 5 | 0.7000000 0.0476400 6 | 0.6000000 0.0580200 7 | 0.5000000 0.0644000 8 | 0.4000000 0.0677800 9 | 0.3000000 0.0671600 10 | 0.2000000 0.0615400 11 | 0.1500000 0.0557300 12 | 0.1000000 0.0479200 13 | 0.0750000 0.0417600 14 | 0.0500000 0.0341100 15 | 0.0250000 0.0234500 16 | 0.0125000 0.0166300 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0113700 19 | 0.0250000 -.0155400 20 | 0.0500000 -.0183900 21 | 0.0750000 -.0202300 22 | 0.1000000 -.0205800 23 | 0.1500000 -.0212700 24 | 0.2000000 -.0209600 25 | 0.3000000 -.0168400 26 | 0.4000000 -.0127200 27 | 0.5000000 -.0086000 28 | 0.6000000 -.0044800 29 | 0.7000000 -.0013600 30 | 0.8000000 -.0007400 31 | 0.9000000 -.0001200 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe611.dat: -------------------------------------------------------------------------------- 1 | GOE 611 AIRFOIL 2 | 1.0000000 0.0032500 3 | 0.8998400 0.0332700 4 | 0.7997200 0.0583000 5 | 0.6996100 0.0818200 6 | 0.5995200 0.1008500 7 | 0.4994600 0.1143700 8 | 0.3994200 0.1224000 9 | 0.2994200 0.1224200 10 | 0.1994700 0.1114500 11 | 0.1495200 0.1002100 12 | 0.0996000 0.0839700 13 | 0.0746500 0.0743500 14 | 0.0497200 0.0597400 15 | 0.0248100 0.0396200 16 | 0.0123800 0.0250600 17 | 0.0000000 0.0000000 18 | 0.0125400 -.0074400 19 | 0.0250400 -.0078800 20 | 0.0500400 -.0077600 21 | 0.0750400 -.0076400 22 | 0.1000400 -.0075200 23 | 0.1500300 -.0072900 24 | 0.2000300 -.0070500 25 | 0.3000300 -.0065700 26 | 0.4000300 -.0061000 27 | 0.5000300 -.0056200 28 | 0.6000200 -.0051500 29 | 0.7000200 -.0046700 30 | 0.8000200 -.0042000 31 | 0.9000200 -.0037200 32 | 1.0000000 -.0032500 33 | -------------------------------------------------------------------------------- /g/goe711.dat: -------------------------------------------------------------------------------- 1 | GOE 711 AIRFOIL 2 | 1.0000000 0.0140000 3 | 0.9500000 0.0317500 4 | 0.9000000 0.0492000 5 | 0.8000000 0.0779000 6 | 0.7000000 0.1001000 7 | 0.5000000 0.1305000 8 | 0.4000000 0.1382000 9 | 0.3000000 0.1394000 10 | 0.2000000 0.1301000 11 | 0.1500000 0.1179500 12 | 0.1000000 0.0978000 13 | 0.0750000 0.0834700 14 | 0.0500000 0.0626500 15 | 0.0250000 0.0418200 16 | 0.0125000 0.0271600 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0108400 19 | 0.0250000 -.0126800 20 | 0.0500000 -.0123500 21 | 0.0750000 -.0120200 22 | 0.1000000 -.0117000 23 | 0.1500000 -.0110500 24 | 0.2000000 -.0104000 25 | 0.3000000 -.0091000 26 | 0.4000000 -.0078000 27 | 0.5000000 -.0065000 28 | 0.7000000 -.0039000 29 | 0.8000000 -.0026000 30 | 0.9000000 -.0013000 31 | 0.9500000 -.0006500 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe770.dat: -------------------------------------------------------------------------------- 1 | GOE 770 AIRFOIL 2 | 1.0000000 0.0026000 3 | 0.9500000 0.0146400 4 | 0.9000000 0.0266800 5 | 0.8000000 0.0505600 6 | 0.7000000 0.0750400 7 | 0.6000000 0.0991200 8 | 0.5000000 0.1223000 9 | 0.4000000 0.1394800 10 | 0.3000000 0.1453600 11 | 0.2000000 0.1369400 12 | 0.1500000 0.1242800 13 | 0.1000000 0.1056200 14 | 0.0500000 0.0769600 15 | 0.0250000 0.0562300 16 | 0.0125000 0.0427200 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0174800 19 | 0.0250000 -.0255700 20 | 0.0500000 -.0356400 21 | 0.1000000 -.0473800 22 | 0.1500000 -.0558200 23 | 0.2000000 -.0613600 24 | 0.3000000 -.0645400 25 | 0.4000000 -.0640200 26 | 0.5000000 -.0563000 27 | 0.6000000 -.0454800 28 | 0.7000000 -.0341600 29 | 0.8000000 -.0227400 30 | 0.9000000 -.0114200 31 | 0.9500000 -.0059600 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe798.dat: -------------------------------------------------------------------------------- 1 | GOE 798 AIRFOIL 2 | 1.0000000 0.0075000 3 | 0.9000000 0.0467500 4 | 0.8000000 0.0822000 5 | 0.7000000 0.1114500 6 | 0.6000000 0.1365000 7 | 0.5000000 0.1537500 8 | 0.4000000 0.1605000 9 | 0.3000000 0.1572500 10 | 0.2000000 0.1427000 11 | 0.1500000 0.1274300 12 | 0.1000000 0.1069500 13 | 0.0750000 0.0931100 14 | 0.0500000 0.0753700 15 | 0.0250000 0.0514400 16 | 0.0125000 0.0345200 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0267800 19 | 0.0250000 -.0360600 20 | 0.0500000 -.0451200 21 | 0.0750000 -.0496900 22 | 0.1000000 -.0504500 23 | 0.1500000 -.0503700 24 | 0.2000000 -.0485000 25 | 0.3000000 -.0427500 26 | 0.4000000 -.0370000 27 | 0.5000000 -.0312500 28 | 0.6000000 -.0255000 29 | 0.7000000 -.0197500 30 | 0.8000000 -.0140000 31 | 0.9000000 -.0082500 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /m/m6.dat: -------------------------------------------------------------------------------- 1 | NACA M6 AIRFOIL 2 | 1.000000 0.002600 3 | 0.950000 0.008800 4 | 0.900000 0.015500 5 | 0.800000 0.030600 6 | 0.700000 0.045800 7 | 0.600000 0.060300 8 | 0.500000 0.072600 9 | 0.400000 0.080500 10 | 0.300000 0.082200 11 | 0.200000 0.075500 12 | 0.150000 0.068200 13 | 0.100000 0.057100 14 | 0.075000 0.049400 15 | 0.050000 0.040300 16 | 0.025000 0.028100 17 | 0.012500 0.019700 18 | 0.000000 0.000000 19 | 0.012500 -0.017600 20 | 0.025000 -0.022000 21 | 0.050000 -0.027300 22 | 0.075000 -0.030300 23 | 0.100000 -0.032400 24 | 0.150000 -0.034700 25 | 0.200000 -0.036200 26 | 0.300000 -0.037900 27 | 0.400000 -0.039000 28 | 0.500000 -0.039400 29 | 0.600000 -0.038200 30 | 0.700000 -0.034800 31 | 0.800000 -0.028300 32 | 0.900000 -0.017700 33 | 0.950000 -0.010800 34 | 1.000000 -0.002600 35 | -------------------------------------------------------------------------------- /r/raf15.dat: -------------------------------------------------------------------------------- 1 | RAF 15 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0119900 4 | 0.9000000 0.0180800 5 | 0.8000000 0.0284600 6 | 0.7000000 0.0366400 7 | 0.6000000 0.0433200 8 | 0.5000000 0.0488000 9 | 0.4000000 0.0531800 10 | 0.3000000 0.0556600 11 | 0.2000000 0.0552400 12 | 0.1500000 0.0520300 13 | 0.1000000 0.0459200 14 | 0.0500000 0.0347100 15 | 0.0250000 0.0255600 16 | 0.0125000 0.0185800 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0079200 19 | 0.0250000 -.0104400 20 | 0.0500000 -.0134900 21 | 0.1000000 -.0147800 22 | 0.1500000 -.0128700 23 | 0.2000000 -.0090600 24 | 0.3000000 -.0035400 25 | 0.4000000 -.0029200 26 | 0.5000000 -.0054000 27 | 0.6000000 -.0085800 28 | 0.7000000 -.0106600 29 | 0.8000000 -.0097400 30 | 0.9000000 -.0079200 31 | 0.9500000 -.0065100 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /r/raf30.dat: -------------------------------------------------------------------------------- 1 | RAF 30 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0070000 4 | 0.9000000 0.0130000 5 | 0.8000000 0.0250000 6 | 0.7000000 0.0370000 7 | 0.6000000 0.0478000 8 | 0.5000000 0.0566000 9 | 0.4000000 0.0620000 10 | 0.3000000 0.0632000 11 | 0.2000000 0.0594000 12 | 0.1500000 0.0544000 13 | 0.1000000 0.0468000 14 | 0.0500000 0.0346000 15 | 0.0250000 0.0248000 16 | 0.0125000 0.0180000 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0180000 19 | 0.0250000 -.0248000 20 | 0.0500000 -.0346000 21 | 0.1000000 -.0468000 22 | 0.1500000 -.0544000 23 | 0.2000000 -.0594000 24 | 0.3000000 -.0632000 25 | 0.4000000 -.0620000 26 | 0.5000000 -.0566000 27 | 0.6000000 -.0478000 28 | 0.7000000 -.0370000 29 | 0.8000000 -.0250000 30 | 0.9000000 -.0130000 31 | 0.9500000 -.0070000 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /r/raf48.dat: -------------------------------------------------------------------------------- 1 | RAF-48 AIRFOIL 2 | 1.000000 0.000000 3 | 0.950000 0.010050 4 | 0.900000 0.019500 5 | 0.800000 0.040200 6 | 0.700000 0.060500 7 | 0.600000 0.079400 8 | 0.500000 0.093800 9 | 0.400000 0.102000 10 | 0.300000 0.104000 11 | 0.200000 0.095300 12 | 0.150000 0.086300 13 | 0.100000 0.073000 14 | 0.075000 0.063900 15 | 0.050000 0.052000 16 | 0.025000 0.036500 17 | 0.012500 0.026000 18 | 0.000000 0.000000 19 | 0.012500 -0.016500 20 | 0.025000 -0.023400 21 | 0.050000 -0.031600 22 | 0.075000 -0.036900 23 | 0.100000 -0.040300 24 | 0.150000 -0.044100 25 | 0.200000 -0.045800 26 | 0.300000 -0.045600 27 | 0.400000 -0.043300 28 | 0.500000 -0.039000 29 | 0.600000 -0.033600 30 | 0.700000 -0.026500 31 | 0.800000 -0.018300 32 | 0.900000 -0.010000 33 | 0.950000 -0.006400 34 | 1.000000 0.000000 35 | -------------------------------------------------------------------------------- /s/stcyr234.dat: -------------------------------------------------------------------------------- 1 | St. CYR 234 (Bartel 17-IC) 2 | 1.0000 0.0000 3 | 0.9500 0.0200 4 | 0.9000 0.0400 5 | 0.8000 0.0775 6 | 0.7000 0.1080 7 | 0.6000 0.1330 8 | 0.5000 0.1520 9 | 0.4000 0.1610 10 | 0.3000 0.1655 11 | 0.2000 0.1620 12 | 0.1500 0.1570 13 | 0.1000 0.1460 14 | 0.0750 0.1380 15 | 0.0500 0.1270 16 | 0.0250 0.1100 17 | 0.0125 0.0955 18 | 0.0000 0.0642 19 | 0.0125 0.0375 20 | 0.0250 0.0270 21 | 0.0500 0.0140 22 | 0.0750 0.0085 23 | 0.1000 0.0050 24 | 0.1500 0.0025 25 | 0.2000 0.0020 26 | 0.3000 0.0065 27 | 0.4000 0.0110 28 | 0.5000 0.0135 29 | 0.6000 0.0190 30 | 0.7000 0.0135 31 | 0.8000 0.0105 32 | 0.9000 0.0050 33 | 0.9500 0.0025 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /s/stcyr24.dat: -------------------------------------------------------------------------------- 1 | St. CYR 24 (Bartel 35-IIIC) 2 | 1.0000 0.0000 3 | 0.9500 0.0170 4 | 0.9000 0.0330 5 | 0.8000 0.0635 6 | 0.7000 0.0915 7 | 0.6000 0.1125 8 | 0.5000 0.1260 9 | 0.4000 0.1340 10 | 0.3000 0.1355 11 | 0.2000 0.1285 12 | 0.1500 0.1210 13 | 0.1000 0.1090 14 | 0.0750 0.0990 15 | 0.0500 0.0865 16 | 0.0250 0.0690 17 | 0.0125 0.0570 18 | 0.0000 0.0256 19 | 0.0125 0.0080 20 | 0.0250 0.0035 21 | 0.0500 0.0010 22 | 0.0750 0.0010 23 | 0.1000 0.0020 24 | 0.1500 0.0035 25 | 0.2000 0.0070 26 | 0.3000 0.0120 27 | 0.4000 0.0140 28 | 0.5000 0.0145 29 | 0.6000 0.0140 30 | 0.7000 0.0130 31 | 0.8000 0.0100 32 | 0.9000 0.0050 33 | 0.9500 0.0030 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /g/goe610b.dat: -------------------------------------------------------------------------------- 1 | GOE 610 B AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9498900 0.0115000 4 | 0.8997800 0.0220000 5 | 0.7995900 0.0410000 6 | 0.6994000 0.0599900 7 | 0.5992800 0.0744900 8 | 0.4991500 0.0854900 9 | 0.3990800 0.0919900 10 | 0.2991100 0.0887900 11 | 0.1991800 0.0800900 12 | 0.1492900 0.0714900 13 | 0.0994200 0.0579900 14 | 0.0744900 0.0507400 15 | 0.0495900 0.0405000 16 | 0.0148000 0.0201500 17 | 0.0000000 0.0000000 18 | 0.0151000 -.0098500 19 | 0.0500800 -.0085000 20 | 0.0750600 -.0062500 21 | 0.1000300 -.0028000 22 | 0.1499600 0.0031000 23 | 0.1999300 0.0070000 24 | 0.2998800 0.0122000 25 | 0.3998600 0.0140000 26 | 0.4998600 0.0140000 27 | 0.5998900 0.0120000 28 | 0.6999100 0.0090000 29 | 0.7999600 0.0045000 30 | 0.9000000 0.0000000 31 | 0.9500100 -.0005000 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe804.dat: -------------------------------------------------------------------------------- 1 | GOE 804 (EA 8) AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0206500 4 | 0.9000000 0.0363000 5 | 0.8000000 0.0616000 6 | 0.7000000 0.0779000 7 | 0.6000000 0.0872000 8 | 0.5000000 0.0915000 9 | 0.4000000 0.0898000 10 | 0.3000000 0.0841000 11 | 0.2000000 0.0714000 12 | 0.1500000 0.0630500 13 | 0.1000000 0.0507000 14 | 0.0750000 0.0435200 15 | 0.0500000 0.0343500 16 | 0.0250000 0.0231800 17 | 0.0000000 0.0000000 18 | 0.0250000 -.0058200 19 | 0.0500000 -.0036500 20 | 0.0750000 -.0004700 21 | 0.1000000 0.0037000 22 | 0.1500000 0.0100500 23 | 0.2000000 0.0164000 24 | 0.3000000 0.0241000 25 | 0.4000000 0.0298000 26 | 0.5000000 0.0335000 27 | 0.6000000 0.0342000 28 | 0.7000000 0.0319000 29 | 0.8000000 0.0286000 30 | 0.9000000 0.0223000 31 | 0.9500000 0.0146500 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/gs1.dat: -------------------------------------------------------------------------------- 1 | SIKORSKY GS-1 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9500000 0.0124000 4 | 0.9000000 0.0248000 5 | 0.8000000 0.0476000 6 | 0.7000000 0.0679000 7 | 0.6000000 0.0847000 8 | 0.5000000 0.0980000 9 | 0.4000000 0.1059000 10 | 0.3000000 0.1065000 11 | 0.2000000 0.0968000 12 | 0.1500000 0.0867000 13 | 0.0750000 0.0618500 14 | 0.0500000 0.0504000 15 | 0.0250000 0.0357500 16 | 0.0125000 0.0252300 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0210800 19 | 0.0250000 -.0281500 20 | 0.0500000 -.0355000 21 | 0.0750000 -.0393500 22 | 0.1500000 -.0417000 23 | 0.2000000 -.0400000 24 | 0.3000000 -.0325000 25 | 0.4000000 -.0234000 26 | 0.5000000 -.0153000 27 | 0.6000000 -.0089000 28 | 0.7000000 -.0045000 29 | 0.8000000 -.0017000 30 | 0.9000000 0.0009000 31 | 0.9500000 0.0011000 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /s/stcyr171.dat: -------------------------------------------------------------------------------- 1 | St. CYR 171 (Royer) 2 | 1.0000 0.0000 3 | 0.9500 0.0071 4 | 0.9000 0.0127 5 | 0.8000 0.0226 6 | 0.7000 0.0316 7 | 0.6000 0.0410 8 | 0.5000 0.0480 9 | 0.4000 0.0538 10 | 0.3000 0.0554 11 | 0.2000 0.0542 12 | 0.1500 0.0523 13 | 0.1000 0.0480 14 | 0.0750 0.0438 15 | 0.0500 0.0370 16 | 0.0250 0.0265 17 | 0.0125 0.0195 18 | 0.0000 0.0000 19 | 0.0125 -0.0195 20 | 0.0250 -0.0263 21 | 0.0500 -0.0370 22 | 0.0750 -0.0438 23 | 0.1000 -0.0480 24 | 0.1500 -0.0523 25 | 0.2000 -0.0542 26 | 0.3000 -0.0554 27 | 0.4000 -0.0538 28 | 0.5000 -0.0180 29 | 0.6000 -0.0410 30 | 0.7000 -0.0316 31 | 0.8000 -0.0226 32 | 0.9000 -0.0127 33 | 0.9500 -0.0071 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /s/stcyr172.dat: -------------------------------------------------------------------------------- 1 | St. CYR 172 (Royer) 2 | 1.0000 0.0000 3 | 0.9500 0.0082 4 | 0.9000 0.0141 5 | 0.8000 0.0274 6 | 0.7000 0.0381 7 | 0.6000 0.0480 8 | 0.5000 0.0562 9 | 0.4000 0.0627 10 | 0.3000 0.0678 11 | 0.2000 0.0672 12 | 0.1500 0.0635 13 | 0.1000 0.0565 14 | 0.0750 0.0503 15 | 0.0500 0.0418 16 | 0.0250 0.0311 17 | 0.0125 0.0226 18 | 0.0000 0.0000 19 | 0.0125 -0.0226 20 | 0.0250 -0.0311 21 | 0.0500 -0.0418 22 | 0.0750 -0.0503 23 | 0.1000 -0.0565 24 | 0.1500 -0.0635 25 | 0.2000 -0.0672 26 | 0.3000 -0.0678 27 | 0.4000 -0.0627 28 | 0.5000 -0.0562 29 | 0.6000 -0.0480 30 | 0.7000 -0.0381 31 | 0.8000 -0.0274 32 | 0.9000 -0.0141 33 | 0.9500 -0.0082 34 | 1.0000 0.0000 35 | -------------------------------------------------------------------------------- /r/raf32mdrev.dat: -------------------------------------------------------------------------------- 1 | RAF-32 MOD airfoil /tracfoil 2 | 1.00000 0.00000 3 | 0.90000 0.02516 4 | 0.80000 0.04622 5 | 0.70000 0.06388 6 | 0.60000 0.07694 7 | 0.50000 0.08530 8 | 0.40000 0.08816 9 | 0.30000 0.08452 10 | 0.20000 0.07338 11 | 0.15000 0.06456 12 | 0.10000 0.05304 13 | 0.05000 0.03662 14 | 0.02500 0.02546 15 | 0.01250 0.01743 16 | 0.000000 0.000000 17 | 0.012500 -0.011370 18 | 0.015054 -0.012353 19 | 0.017566 -0.013128 20 | 0.020050 -0.013748 21 | 0.022523 -0.014268 22 | 0.025000 -0.014740 23 | 0.05000 -0.01908 24 | 0.10000 -0.02236 25 | 0.15000 -0.02284 26 | 0.20000 -0.02212 27 | 0.30000 -0.01708 28 | 0.40000 -0.01124 29 | 0.50000 -0.00620 30 | 0.60000 0.00014 31 | 0.70000 0.00388 32 | 0.80000 0.00542 33 | 0.90000 0.00376 34 | 1.00000 0.00000 35 | -------------------------------------------------------------------------------- /e/ec863914.dat: -------------------------------------------------------------------------------- 1 | EPPLER EC 86(-3)-914 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9803000 0.0079000 4 | 0.9303000 0.0289000 5 | 0.8134000 0.0673000 6 | 0.7123001 0.0863000 7 | 0.5977000 0.0994000 8 | 0.4757000 0.1061000 9 | 0.3547000 0.1059000 10 | 0.2972000 0.1032000 11 | 0.1929000 0.0928000 12 | 0.1478000 0.0851000 13 | 0.1089000 0.0757000 14 | 0.0484000 0.0505000 15 | 0.0109000 0.0230000 16 | 0.0017000 0.0106000 17 | 0.0000000 0.0000000 18 | 0.0009000 -.0006000 19 | 0.0102000 -.0078000 20 | 0.0282000 -.0168000 21 | 0.0530000 -.0254000 22 | 0.0845000 -.0329000 23 | 0.1216000 -.0383000 24 | 0.2155000 -.0409000 25 | 0.3314000 -.0379000 26 | 0.4594000 -.0309000 27 | 0.5885000 -.0192000 28 | 0.7166001 0.0023000 29 | 0.8421000 0.0186000 30 | 0.9451000 0.0152000 31 | 0.9772000 0.0075000 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /g/goe229rev.dat: -------------------------------------------------------------------------------- 1 | GOE 229 (MVA H.39) AIRFOIL /tracfoil 2 | 1.00000 0.00100 3 | 0.94870 0.01959 4 | 0.89753 0.03719 5 | 0.79532 0.07039 6 | 0.69340 0.09921 7 | 0.59185 0.12266 8 | 0.49075 0.13913 9 | 0.39013 0.14844 10 | 0.29031 0.14580 11 | 0.19130 0.13092 12 | 0.14216 0.11795 13 | 0.09361 0.09622 14 | 0.06954 0.08212 15 | 0.05575 0.07004 16 | 0.02241 0.03899 17 | 0.01096 0.02323 18 | 0.00000 0.00000 19 | 0.01344 -0.01411 20 | 0.02629 -0.01925 21 | 0.05180 -0.02706 22 | 0.07726 -0.03386 23 | 0.10254 -0.03818 24 | 0.15302 -0.04532 25 | 0.20326 -0.04898 26 | 0.30315 -0.04734 27 | 0.40235 -0.03524 28 | 0.50128 -0.01917 29 | 0.60031 -0.00458 30 | 0.69953 0.00702 31 | 0.79929 0.01065 32 | 0.89945 0.00831 33 | 0.94976 0.00366 34 | 1.00000 -0.00100 35 | 36 | 37 | 0.05575 0.06404 38 | -------------------------------------------------------------------------------- /g/goe417a.dat: -------------------------------------------------------------------------------- 1 | GOE 417A (GEW. PLATTE) AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0240000 4 | 0.8000000 0.0425000 5 | 0.7000000 0.0545000 6 | 0.6000000 0.0640000 7 | 0.5000000 0.0700000 8 | 0.4000000 0.0735000 9 | 0.3000000 0.0715000 10 | 0.2000000 0.0630000 11 | 0.1500000 0.0570000 12 | 0.1000000 0.0485000 13 | 0.0750000 0.0415000 14 | 0.0500000 0.0325000 15 | 0.0250000 0.0220000 16 | 0.0125000 0.0155000 17 | 0.0000000 0.0000000 18 | 0.0125000 -.0140000 19 | 0.0250000 -.0100000 20 | 0.0500000 0.0010000 21 | 0.0750000 0.0105000 22 | 0.1000000 0.0185000 23 | 0.1500000 0.0275000 24 | 0.2000000 0.0340000 25 | 0.3000000 0.0425000 26 | 0.4000000 0.0445000 27 | 0.5000000 0.0410000 28 | 0.6000000 0.0350000 29 | 0.7000000 0.0255000 30 | 0.8000000 0.0135000 31 | 0.9000000 -.0015000 32 | 1.0000000 0.0000000 33 | -------------------------------------------------------------------------------- /m/marske1.dat: -------------------------------------------------------------------------------- 1 | MARSKE XM-1D AIRFOIL (F14-3.0) 2 | 1.000000 0.000000 3 | 0.900097 0.007409 4 | 0.800216 0.016517 5 | 0.700385 0.029425 6 | 0.600603 0.046032 7 | 0.500887 0.067738 8 | 0.401119 0.085445 9 | 0.301279 0.097653 10 | 0.251314 0.100308 11 | 0.201299 0.099163 12 | 0.151221 0.093219 13 | 0.101062 0.081076 14 | 0.075950 0.072505 15 | 0.050800 0.061035 16 | 0.025588 0.044865 17 | 0.012934 0.033131 18 | 0.000000 0.000000 19 | 0.012274 -0.017261 20 | 0.024717 -0.021624 21 | 0.049677 -0.024651 22 | 0.074602 -0.030377 23 | 0.099569 -0.032904 24 | 0.149516 -0.036959 25 | 0.199489 -0.039013 26 | 0.249480 -0.039668 27 | 0.299472 -0.040323 28 | 0.399455 -0.041633 29 | 0.499437 -0.042943 30 | 0.599473 -0.040253 31 | 0.699552 -0.034164 32 | 0.799669 -0.025276 33 | 0.899821 -0.013688 34 | 1.000000 0.000000 35 | -------------------------------------------------------------------------------- /r/r13012.dat: -------------------------------------------------------------------------------- 1 | Ritz 1-30-12 de profils MRA 2 | 1.000000 0.000000 3 | 0.977000 0.003500 4 | 0.916200 0.012700 5 | 0.820000 0.025700 6 | 0.756700 0.033600 7 | 0.620000 0.048500 8 | 0.477500 0.060900 9 | 0.368300 0.068300 10 | 0.285000 0.069500 11 | 0.206600 0.065300 12 | 0.141200 0.058000 13 | 0.089200 0.047300 14 | 0.048000 0.034200 15 | 0.020100 0.022100 16 | 0.009600 0.015300 17 | 0.001400 0.005900 18 | 0.000000 0.000000 19 | 0.000400 -0.001900 20 | 0.003400 -0.007000 21 | 0.010100 -0.012900 22 | 0.021300 -0.019000 23 | 0.044800 -0.026200 24 | 0.096500 -0.036800 25 | 0.167000 -0.045000 26 | 0.247500 -0.049700 27 | 0.341200 -0.048900 28 | 0.469400 -0.044000 29 | 0.610100 -0.036200 30 | 0.755000 -0.025000 31 | 0.873300 -0.013800 32 | 0.949900 -0.006100 33 | 1.000000 0.000000 34 | Epaisseur relative 11.84 -------------------------------------------------------------------------------- /h/horten.dat: -------------------------------------------------------------------------------- 1 | Horten Standard 13% 2 | 1.00000 0.00000 3 | 0.95000 0.00488 4 | 0.90000 0.01014 5 | 0.80000 0.02236 6 | 0.70000 0.03660 7 | 0.60000 0.05294 8 | 0.50000 0.06910 9 | 0.40000 0.08099 10 | 0.30000 0.08639 11 | 0.25000 0.08522 12 | 0.20000 0.08223 13 | 0.15000 0.07527 14 | 0.10000 0.06331 15 | 0.07500 0.05533 16 | 0.05000 0.04544 17 | 0.02500 0.03198 18 | 0.01250 0.02145 19 | 0.00000 0.00000 20 | 0.01250 -0.01417 21 | 0.02500 -0.01924 22 | 0.05000 -0.02685 23 | 0.07500 -0.03229 24 | 0.10000 -0.03601 25 | 0.15000 -0.04011 26 | 0.20000 -0.04232 27 | 0.25000 -0.04323 28 | 0.30000 -0.04362 29 | 0.40000 -0.04251 30 | 0.50000 -0.03907 31 | 0.60000 -0.03390 32 | 0.70000 -0.02704 33 | 0.80000 -0.01898 34 | 0.90000 -0.00962 35 | 0.95000 -0.00475 36 | 1.00000 0.00000 37 | 38 | -------------------------------------------------------------------------------- /m/marske5.dat: -------------------------------------------------------------------------------- 1 | MARSKE MONARCH AIRFOIL (NACA 43012A) 2 | 1.000000 0.000000 3 | 0.900000 0.012500 4 | 0.800000 0.024400 5 | 0.700000 0.037000 6 | 0.600000 0.052000 7 | 0.500000 0.065600 8 | 0.400000 0.077000 9 | 0.300000 0.085700 10 | 0.250000 0.089500 11 | 0.200000 0.092700 12 | 0.150000 0.093300 13 | 0.100000 0.087700 14 | 0.075000 0.080300 15 | 0.050000 0.069200 16 | 0.025000 0.051400 17 | 0.012500 0.038900 18 | 0.000000 0.000000 19 | 0.012500 -0.008300 20 | 0.025000 -0.011400 21 | 0.050000 -0.015400 22 | 0.075000 -0.018500 23 | 0.100000 -0.021100 24 | 0.150000 -0.025700 25 | 0.200000 -0.029500 26 | 0.250000 -0.032700 27 | 0.300000 -0.035000 28 | 0.400000 -0.039200 29 | 0.500000 -0.040300 30 | 0.600000 -0.039200 31 | 0.700000 -0.036000 32 | 0.800000 -0.027400 33 | 0.900000 -0.015000 34 | 1.000000 0.000000 35 | -------------------------------------------------------------------------------- /n/naca000834.dat: -------------------------------------------------------------------------------- 1 | NACA 0008-34 2 | 1.0000 0.00080 3 | 0.9500 0.00684 4 | 0.9000 0.01244 5 | 0.8000 0.02213 6 | 0.7000 0.02987 7 | 0.6000 0.03547 8 | 0.5000 0.03884 9 | 0.4000 0.04000 10 | 0.3000 0.03867 11 | 0.2000 0.03396 12 | 0.1500 0.02996 13 | 0.1000 0.02436 14 | 0.0750 0.02089 15 | 0.0500 0.01662 16 | 0.0250 0.01120 17 | 0.0125 0.00756 18 | 0.0000 0.00000 19 | 0.0125 -0.00756 20 | 0.0250 -0.01120 21 | 0.0500 -0.01662 22 | 0.0750 -0.02089 23 | 0.1000 -0.02436 24 | 0.1500 -0.02996 25 | 0.2000 -0.03396 26 | 0.3000 -0.03867 27 | 0.4000 -0.04000 28 | 0.5000 -0.03884 29 | 0.6000 -0.03547 30 | 0.7000 -0.02987 31 | 0.8000 -0.02213 32 | 0.9000 -0.01244 33 | 0.9500 -0.00684 34 | 1.0000 -0.00080 35 | -------------------------------------------------------------------------------- /n/naca001034.dat: -------------------------------------------------------------------------------- 1 | NACA 0010-34 2 | 1.0000 0.00100 3 | 0.9500 0.00856 4 | 0.9000 0.01556 5 | 0.8000 0.02767 6 | 0.7000 0.03733 7 | 0.6000 0.04433 8 | 0.5000 0.04856 9 | 0.4000 0.05000 10 | 0.3000 0.04833 11 | 0.2000 0.04244 12 | 0.1500 0.03744 13 | 0.1000 0.03044 14 | 0.0750 0.02611 15 | 0.0500 0.02078 16 | 0.0250 0.01400 17 | 0.0125 0.00944 18 | 0.0000 0.00000 19 | 0.0125 -0.00944 20 | 0.0250 -0.01400 21 | 0.0500 -0.02078 22 | 0.0750 -0.02611 23 | 0.1000 -0.03044 24 | 0.1500 -0.03744 25 | 0.2000 -0.04244 26 | 0.3000 -0.04833 27 | 0.4000 -0.05000 28 | 0.5000 -0.04856 29 | 0.6000 -0.04433 30 | 0.7000 -0.03733 31 | 0.8000 -0.02767 32 | 0.9000 -0.01556 33 | 0.9500 -0.00856 34 | 1.0000 -0.00100 35 | -------------------------------------------------------------------------------- /n/naca001035.dat: -------------------------------------------------------------------------------- 1 | NACA 0010-35 2 | 1.0000 0.00100 3 | 0.9500 0.01178 4 | 0.9000 0.02100 5 | 0.8000 0.03500 6 | 0.7000 0.04389 7 | 0.6000 0.04867 8 | 0.5000 0.05000 9 | 0.4000 0.04878 10 | 0.3000 0.04478 11 | 0.2000 0.03789 12 | 0.1500 0.03289 13 | 0.1000 0.02667 14 | 0.0750 0.02289 15 | 0.0500 0.01844 16 | 0.0250 0.01267 17 | 0.0125 0.00878 18 | 0.0000 0.00000 19 | 0.0125 -0.00878 20 | 0.0250 -0.01267 21 | 0.0500 -0.01844 22 | 0.0750 -0.02289 23 | 0.1000 -0.02667 24 | 0.1500 -0.03289 25 | 0.2000 -0.03789 26 | 0.3000 -0.04478 27 | 0.4000 -0.04878 28 | 0.5000 -0.05000 29 | 0.6000 -0.04867 30 | 0.7000 -0.04389 31 | 0.8000 -0.03500 32 | 0.9000 -0.02100 33 | 0.9500 -0.01178 34 | 1.0000 -0.00100 35 | -------------------------------------------------------------------------------- /n/naca001064.dat: -------------------------------------------------------------------------------- 1 | NACA 0010-64 2 | 1.0000 0.00100 3 | 0.9500 0.00856 4 | 0.9000 0.01556 5 | 0.8000 0.02767 6 | 0.7000 0.03733 7 | 0.6000 0.04433 8 | 0.5000 0.04856 9 | 0.4000 0.05000 10 | 0.3000 0.04856 11 | 0.2000 0.04411 12 | 0.1500 0.04056 13 | 0.1000 0.03533 14 | 0.0750 0.03178 15 | 0.0500 0.02722 16 | 0.0250 0.02044 17 | 0.0125 0.01511 18 | 0.0000 0.00000 19 | 0.0125 -0.01511 20 | 0.0250 -0.02044 21 | 0.0500 -0.02722 22 | 0.0750 -0.03178 23 | 0.1000 -0.03533 24 | 0.1500 -0.04056 25 | 0.2000 -0.04411 26 | 0.3000 -0.04856 27 | 0.4000 -0.05000 28 | 0.5000 -0.04856 29 | 0.6000 -0.04433 30 | 0.7000 -0.03733 31 | 0.8000 -0.02767 32 | 0.9000 -0.01556 33 | 0.9500 -0.00856 34 | 1.0000 -0.00100 35 | -------------------------------------------------------------------------------- /n/naca001065.dat: -------------------------------------------------------------------------------- 1 | NACA 0010-65 2 | 1.0000 0.00100 3 | 0.9500 0.01178 4 | 0.9000 0.02100 5 | 0.8000 0.03500 6 | 0.7000 0.04389 7 | 0.6000 0.04867 8 | 0.5000 0.05000 9 | 0.4000 0.04889 10 | 0.3000 0.04578 11 | 0.2000 0.04089 12 | 0.1500 0.03756 13 | 0.1000 0.03300 14 | 0.0750 0.02989 15 | 0.0500 0.02589 16 | 0.0250 0.01967 17 | 0.0125 0.01467 18 | 0.0000 0.00000 19 | 0.0125 -0.01467 20 | 0.0250 -0.01967 21 | 0.0500 -0.02589 22 | 0.0750 -0.02989 23 | 0.1000 -0.03300 24 | 0.1500 -0.03756 25 | 0.2000 -0.04089 26 | 0.3000 -0.04578 27 | 0.4000 -0.04889 28 | 0.5000 -0.05000 29 | 0.6000 -0.04867 30 | 0.7000 -0.04389 31 | 0.8000 -0.03500 32 | 0.9000 -0.02100 33 | 0.9500 -0.01178 34 | 1.0000 -0.00100 35 | -------------------------------------------------------------------------------- /n/naca001066.dat: -------------------------------------------------------------------------------- 1 | NACA 0010-66 2 | 1.0000 0.00100 3 | 0.9500 0.01656 4 | 0.9000 0.02833 5 | 0.8000 0.04300 6 | 0.7000 0.04889 7 | 0.6000 0.05000 8 | 0.5000 0.04956 9 | 0.4000 0.04822 10 | 0.3000 0.04578 11 | 0.2000 0.04178 12 | 0.1500 0.03856 13 | 0.1000 0.03400 14 | 0.0750 0.03089 15 | 0.0500 0.02656 16 | 0.0250 0.02011 17 | 0.0125 0.01489 18 | 0.0000 0.00000 19 | 0.0125 -0.01489 20 | 0.0250 -0.02011 21 | 0.0500 -0.02656 22 | 0.0750 -0.03089 23 | 0.1000 -0.03400 24 | 0.1500 -0.03856 25 | 0.2000 -0.04178 26 | 0.3000 -0.04578 27 | 0.4000 -0.04822 28 | 0.5000 -0.04956 29 | 0.6000 -0.05000 30 | 0.7000 -0.04889 31 | 0.8000 -0.04300 32 | 0.9000 -0.02833 33 | 0.9500 -0.01656 34 | 1.0000 -0.00100 35 | -------------------------------------------------------------------------------- /n/naca001234.dat: -------------------------------------------------------------------------------- 1 | NACA 0012-34 2 | 1.0000 0.00120 3 | 0.9500 0.01027 4 | 0.9000 0.01867 5 | 0.8000 0.03320 6 | 0.7000 0.04480 7 | 0.6000 0.05320 8 | 0.5000 0.05827 9 | 0.4000 0.06000 10 | 0.3000 0.05800 11 | 0.2000 0.05093 12 | 0.1500 0.04493 13 | 0.1000 0.03653 14 | 0.0750 0.03133 15 | 0.0500 0.02493 16 | 0.0250 0.01680 17 | 0.0125 0.01133 18 | 0.0000 0.00000 19 | 0.0125 -0.01133 20 | 0.0250 -0.01680 21 | 0.0500 -0.02493 22 | 0.0750 -0.03133 23 | 0.1000 -0.03653 24 | 0.1500 -0.04493 25 | 0.2000 -0.05093 26 | 0.3000 -0.05800 27 | 0.4000 -0.06000 28 | 0.5000 -0.05827 29 | 0.6000 -0.05320 30 | 0.7000 -0.04480 31 | 0.8000 -0.03320 32 | 0.9000 -0.01867 33 | 0.9500 -0.01027 34 | 1.0000 -0.00120 35 | -------------------------------------------------------------------------------- /n/naca001264.dat: -------------------------------------------------------------------------------- 1 | NACA 0012-64 2 | 1.0000 0.00120 3 | 0.9500 0.01027 4 | 0.9000 0.01867 5 | 0.8000 0.03320 6 | 0.7000 0.04480 7 | 0.6000 0.05320 8 | 0.5000 0.05827 9 | 0.4000 0.06000 10 | 0.3000 0.05827 11 | 0.2000 0.05293 12 | 0.1500 0.04867 13 | 0.1000 0.04240 14 | 0.0750 0.03813 15 | 0.0500 0.03267 16 | 0.0250 0.02453 17 | 0.0125 0.01813 18 | 0.0000 0.00000 19 | 0.0125 -0.01813 20 | 0.0250 -0.02453 21 | 0.0500 -0.03267 22 | 0.0750 -0.03813 23 | 0.1000 -0.04240 24 | 0.1500 -0.04867 25 | 0.2000 -0.05293 26 | 0.3000 -0.05827 27 | 0.4000 -0.06000 28 | 0.5000 -0.05827 29 | 0.6000 -0.05320 30 | 0.7000 -0.04480 31 | 0.8000 -0.03320 32 | 0.9000 -0.01867 33 | 0.9500 -0.01027 34 | 1.0000 -0.00120 35 | -------------------------------------------------------------------------------- /n/naca16006.dat: -------------------------------------------------------------------------------- 1 | NACA 16-006 2 | 1.0000 0.00060 3 | 0.9500 0.00707 4 | 0.9000 0.01259 5 | 0.8000 0.02099 6 | 0.7000 0.02635 7 | 0.6000 0.02917 8 | 0.5000 0.03000 9 | 0.4000 0.02927 10 | 0.3000 0.02709 11 | 0.2000 0.02332 12 | 0.1500 0.02067 13 | 0.1000 0.01729 14 | 0.0750 0.01516 15 | 0.0500 0.01255 16 | 0.0250 0.00903 17 | 0.0125 0.00646 18 | 0.0000 0.00000 19 | 0.0125 -0.00646 20 | 0.0250 -0.00903 21 | 0.0500 -0.01255 22 | 0.0750 -0.01516 23 | 0.1000 -0.01729 24 | 0.1500 -0.02067 25 | 0.2000 -0.02332 26 | 0.3000 -0.02709 27 | 0.4000 -0.02927 28 | 0.5000 -0.03000 29 | 0.6000 -0.02917 30 | 0.7000 -0.02635 31 | 0.8000 -0.02099 32 | 0.9000 -0.01259 33 | 0.9500 -0.00707 34 | 1.0000 -0.00060 35 | -------------------------------------------------------------------------------- /n/naca16012.dat: -------------------------------------------------------------------------------- 1 | NACA 16-012 2 | 1.0000 0.00120 3 | 0.9500 0.01415 4 | 0.9000 0.02517 5 | 0.8000 0.04199 6 | 0.7000 0.05269 7 | 0.6000 0.05835 8 | 0.5000 0.06000 9 | 0.4000 0.05855 10 | 0.3000 0.05417 11 | 0.2000 0.04664 12 | 0.1500 0.04135 13 | 0.1000 0.03457 14 | 0.0750 0.03032 15 | 0.0500 0.02509 16 | 0.0250 0.01805 17 | 0.0125 0.01292 18 | 0.0000 0.00000 19 | 0.0125 -0.01292 20 | 0.0250 -0.01805 21 | 0.0500 -0.02509 22 | 0.0750 -0.03032 23 | 0.1000 -0.03457 24 | 0.1500 -0.04135 25 | 0.2000 -0.04664 26 | 0.3000 -0.05417 27 | 0.4000 -0.05855 28 | 0.5000 -0.06000 29 | 0.6000 -0.05835 30 | 0.7000 -0.05269 31 | 0.8000 -0.04199 32 | 0.9000 -0.02517 33 | 0.9500 -0.01415 34 | 1.0000 -0.00120 35 | -------------------------------------------------------------------------------- /n/naca16015.dat: -------------------------------------------------------------------------------- 1 | NACA 16-015 2 | 1.0000 0.00150 3 | 0.9500 0.01768 4 | 0.9000 0.03147 5 | 0.8000 0.05248 6 | 0.7000 0.06587 7 | 0.6000 0.07293 8 | 0.5000 0.07500 9 | 0.4000 0.07318 10 | 0.3000 0.06772 11 | 0.2000 0.05830 12 | 0.1500 0.05168 13 | 0.1000 0.04322 14 | 0.0750 0.03790 15 | 0.0500 0.03137 16 | 0.0250 0.02257 17 | 0.0125 0.01615 18 | 0.0000 0.00000 19 | 0.0125 -0.01615 20 | 0.0250 -0.02257 21 | 0.0500 -0.03137 22 | 0.0750 -0.03790 23 | 0.1000 -0.04322 24 | 0.1500 -0.05168 25 | 0.2000 -0.05830 26 | 0.3000 -0.06772 27 | 0.4000 -0.07318 28 | 0.5000 -0.07500 29 | 0.6000 -0.07293 30 | 0.7000 -0.06587 31 | 0.8000 -0.05248 32 | 0.9000 -0.03147 33 | 0.9500 -0.01768 34 | 1.0000 -0.00150 35 | -------------------------------------------------------------------------------- /n/naca16018.dat: -------------------------------------------------------------------------------- 1 | NACA 16-018 2 | 1.0000 0.00180 3 | 0.9500 0.02122 4 | 0.9000 0.03776 5 | 0.8000 0.06298 6 | 0.7000 0.07904 7 | 0.6000 0.08752 8 | 0.5000 0.09000 9 | 0.4000 0.08782 10 | 0.3000 0.08126 11 | 0.2000 0.06996 12 | 0.1500 0.06202 13 | 0.1000 0.05186 14 | 0.0750 0.04548 15 | 0.0500 0.03764 16 | 0.0250 0.02708 17 | 0.0125 0.01938 18 | 0.0000 0.00000 19 | 0.0125 -0.01938 20 | 0.0250 -0.02708 21 | 0.0500 -0.03764 22 | 0.0750 -0.04548 23 | 0.1000 -0.05186 24 | 0.1500 -0.06202 25 | 0.2000 -0.06996 26 | 0.3000 -0.08126 27 | 0.4000 -0.08782 28 | 0.5000 -0.09000 29 | 0.6000 -0.08752 30 | 0.7000 -0.07904 31 | 0.8000 -0.06298 32 | 0.9000 -0.03776 33 | 0.9500 -0.02122 34 | 1.0000 -0.00180 35 | -------------------------------------------------------------------------------- /n/naca16021.dat: -------------------------------------------------------------------------------- 1 | NACA 16-021 2 | 1.0000 0.00210 3 | 0.9500 0.02476 4 | 0.9000 0.04405 5 | 0.8000 0.07348 6 | 0.7000 0.09221 7 | 0.6000 0.10211 8 | 0.5000 0.10500 9 | 0.4000 0.10246 10 | 0.3000 0.09480 11 | 0.2000 0.08162 12 | 0.1500 0.07236 13 | 0.1000 0.06050 14 | 0.0750 0.05306 15 | 0.0500 0.04391 16 | 0.0250 0.03159 17 | 0.0125 0.02261 18 | 0.0000 0.00000 19 | 0.0125 -0.02261 20 | 0.0250 -0.03159 21 | 0.0500 -0.04391 22 | 0.0750 -0.05306 23 | 0.1000 -0.06050 24 | 0.1500 -0.07236 25 | 0.2000 -0.08162 26 | 0.3000 -0.09480 27 | 0.4000 -0.10246 28 | 0.5000 -0.10500 29 | 0.6000 -0.10211 30 | 0.7000 -0.09221 31 | 0.8000 -0.07348 32 | 0.9000 -0.04405 33 | 0.9500 -0.02476 34 | 1.0000 -0.00210 35 | -------------------------------------------------------------------------------- /0-9/2032c.dat: -------------------------------------------------------------------------------- 1 | 20-32C AIRFOIL 2 | 1.000000 0.001600 3 | 0.950000 0.012400 4 | 0.900000 0.022900 5 | 0.800000 0.042800 6 | 0.700000 0.061000 7 | 0.600000 0.077100 8 | 0.500000 0.090500 9 | 0.400000 0.100200 10 | 0.300000 0.104800 11 | 0.250000 0.104400 12 | 0.200000 0.101300 13 | 0.150000 0.093400 14 | 0.100000 0.078000 15 | 0.075000 0.066400 16 | 0.050000 0.051300 17 | 0.025000 0.031700 18 | 0.012500 0.019300 19 | 0.000000 0.000000 20 | 0.012500 -0.005000 21 | 0.025000 -0.004200 22 | 0.050000 -0.001000 23 | 0.075000 0.002800 24 | 0.100000 0.006800 25 | 0.150000 0.014500 26 | 0.200000 0.021700 27 | 0.250000 0.028200 28 | 0.300000 0.033300 29 | 0.400000 0.038500 30 | 0.500000 0.038600 31 | 0.600000 0.035000 32 | 0.700000 0.028600 33 | 0.800000 0.020200 34 | 0.900000 0.010000 35 | 0.950000 0.004400 36 | 1.000000 -0.001600 37 | -------------------------------------------------------------------------------- /b/b707brev.dat: -------------------------------------------------------------------------------- 1 | BOEING 707 .19 SPAN AIRFOIL /tracfoil 2 | 1.00000 0.00000 3 | 0.866011 0.012882 4 | 0.732243 0.027492 5 | 0.59890 0.04663 6 | 0.49857 0.06077 7 | 0.39856 0.06101 8 | 0.29854 0.06185 9 | 0.24855 0.06127 10 | 0.19855 0.06139 11 | 0.14864 0.05771 12 | 0.09879 0.05143 13 | 0.07392 0.04575 14 | 0.04904 0.04066 15 | 0.02431 0.02927 16 | 0.01216 0.01879 17 | 0.00705 0.01477 18 | 0.00471 0.01221 19 | 0.00000 0.00000 20 | 0.00521 -0.00888 21 | 0.00768 -0.01192 22 | 0.01294 -0.01439 23 | 0.02547 -0.01980 24 | 0.05065 -0.02751 25 | 0.07576 -0.03201 26 | 0.10088 -0.03712 27 | 0.15104 -0.04423 28 | 0.20120 -0.05075 29 | 0.25132 -0.05587 30 | 0.30141 -0.05979 31 | 0.40142 -0.06003 32 | 0.50136 -0.05767 33 | 0.60118 -0.05021 34 | 0.701183 -0.040287 35 | 0.800990 -0.028794 36 | 1.00000 0.00000 37 | -------------------------------------------------------------------------------- /m/marske2.dat: -------------------------------------------------------------------------------- 1 | MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID) 2 | 1.000000 0.000000 3 | 0.900000 0.012300 4 | 0.800000 0.024400 5 | 0.700000 0.036600 6 | 0.600000 0.050600 7 | 0.500000 0.062800 8 | 0.400000 0.072900 9 | 0.300000 0.080300 10 | 0.250000 0.082800 11 | 0.200000 0.084400 12 | 0.150000 0.083400 13 | 0.100000 0.076900 14 | 0.075000 0.070000 15 | 0.050000 0.059800 16 | 0.025000 0.044300 17 | 0.012500 0.033200 18 | 0.000000 0.000000 19 | 0.012500 -0.010200 20 | 0.025000 -0.014100 21 | 0.050000 -0.018400 22 | 0.075000 -0.021700 23 | 0.100000 -0.024500 24 | 0.150000 -0.029600 25 | 0.200000 -0.034200 26 | 0.250000 -0.037700 27 | 0.300000 -0.040200 28 | 0.400000 -0.043300 29 | 0.500000 -0.043200 30 | 0.600000 -0.040800 31 | 0.700000 -0.035500 32 | 0.800000 -0.026300 33 | 0.900000 -0.014000 34 | 1.000000 0.000000 35 | -------------------------------------------------------------------------------- /n/nacam6.dat: -------------------------------------------------------------------------------- 1 | NACA M6 2 | 1.0000 0.0026 3 | 0.9500 0.0088 4 | 0.9000 0.0155 5 | 0.8000 0.0306 6 | 0.7000 0.0458 7 | 0.6000 0.0603 8 | 0.5000 0.0726 9 | 0.4000 0.0805 10 | 0.3000 0.0822 11 | 0.2500 0.0801 12 | 0.2000 0.0755 13 | 0.1500 0.0682 14 | 0.1000 0.0571 15 | 0.0750 0.0494 16 | 0.0500 0.0403 17 | 0.0250 0.0281 18 | 0.0125 0.0197 19 | 0.0000 0.0000 20 | 0.0125 -0.0176 21 | 0.0250 -0.0220 22 | 0.0500 -0.0273 23 | 0.0750 -0.0303 24 | 0.1000 -0.0324 25 | 0.1500 -0.0347 26 | 0.2000 -0.0362 27 | 0.2500 -0.0371 28 | 0.3000 -0.0379 29 | 0.4000 -0.0390 30 | 0.5000 -0.0394 31 | 0.6000 -0.0382 32 | 0.7000 -0.0348 33 | 0.8000 -0.0283 34 | 0.9000 -0.0177 35 | 0.9500 -0.0108 36 | 1.0000 0.0026 37 | -------------------------------------------------------------------------------- /s/stcyr171rev.dat: -------------------------------------------------------------------------------- 1 | St. CYR 171 (Royer) 2 | 1.0000 0.0000 3 | 0.9500 0.0071 4 | 0.9000 0.0127 5 | 0.8000 0.0226 6 | 0.7000 0.0316 7 | 0.6000 0.0410 8 | 0.5000 0.0480 9 | 0.4000 0.0538 10 | 0.3000 0.0554 11 | 0.2000 0.0542 12 | 0.1500 0.0523 13 | 0.1000 0.0480 14 | 0.0750 0.0438 15 | 0.0500 0.0370 16 | 0.0250 0.0265 17 | 0.0125 0.0195 18 | 0.0000 0.0000 19 | 0.0125 -0.0195 20 | 0.0250 -0.0263 21 | 0.0500 -0.0370 22 | 0.0750 -0.0438 23 | 0.1000 -0.0480 24 | 0.1500 -0.0523 25 | 0.2000 -0.0542 26 | 0.3000 -0.0554 27 | 0.4000 -0.0538 28 | 0.5000 -0.0480 29 | 0.6000 -0.0410 30 | 0.7000 -0.0316 31 | 0.8000 -0.0226 32 | 0.9000 -0.0127 33 | 0.9500 -0.0071 34 | 1.0000 0.0000 35 | 36 | 0.5000 -0.0180 37 | -------------------------------------------------------------------------------- /m/marske3.dat: -------------------------------------------------------------------------------- 1 | MARSKE PIONEER IID ROOT AIRFOIL (NACA 431012A/24112 HYBRID) 2 | 1.000000 0.000000 3 | 0.900000 0.012800 4 | 0.800000 0.024800 5 | 0.700000 0.036600 6 | 0.600000 0.050800 7 | 0.500000 0.063700 8 | 0.400000 0.074400 9 | 0.300000 0.082500 10 | 0.250000 0.085100 11 | 0.200000 0.086300 12 | 0.150000 0.084500 13 | 0.100000 0.077000 14 | 0.075000 0.069700 15 | 0.050000 0.059400 16 | 0.025000 0.043700 17 | 0.012500 0.032200 18 | 0.000000 0.000000 19 | 0.012500 -0.009000 20 | 0.025000 -0.012300 21 | 0.050000 -0.017300 22 | 0.075000 -0.021300 23 | 0.100000 -0.024500 24 | 0.150000 -0.029300 25 | 0.200000 -0.033100 26 | 0.250000 -0.035500 27 | 0.300000 -0.038100 28 | 0.400000 -0.041800 29 | 0.500000 -0.042300 30 | 0.600000 -0.041500 31 | 0.700000 -0.036400 32 | 0.800000 -0.026500 33 | 0.900000 -0.014100 34 | 1.000000 0.000000 35 | -------------------------------------------------------------------------------- /m/marske4.dat: -------------------------------------------------------------------------------- 1 | MARSKE PIONEER IID TIP AIRFOIL (NACA 431012A*.833 HYBRID) 2 | 1.000000 0.000000 3 | 0.900000 0.010400 4 | 0.800000 0.020300 5 | 0.700000 0.030800 6 | 0.600000 0.043300 7 | 0.500000 0.054700 8 | 0.400000 0.064200 9 | 0.300000 0.071400 10 | 0.250000 0.074600 11 | 0.200000 0.077300 12 | 0.150000 0.077700 13 | 0.100000 0.073100 14 | 0.075000 0.066900 15 | 0.050000 0.057700 16 | 0.025000 0.042800 17 | 0.012500 0.032400 18 | 0.000000 0.000000 19 | 0.012500 -0.006900 20 | 0.025000 -0.009500 21 | 0.050000 -0.012800 22 | 0.075000 -0.015400 23 | 0.100000 -0.017600 24 | 0.150000 -0.021400 25 | 0.200000 -0.024600 26 | 0.250000 -0.027200 27 | 0.300000 -0.029200 28 | 0.400000 -0.032700 29 | 0.500000 -0.033600 30 | 0.600000 -0.032700 31 | 0.700000 -0.030000 32 | 0.800000 -0.022800 33 | 0.900000 -0.012500 34 | 1.000000 0.000000 35 | -------------------------------------------------------------------------------- /n/naca2412.dat: -------------------------------------------------------------------------------- 1 | NACA 2412 2 | 1.0000 0.0013 3 | 0.9500 0.0114 4 | 0.9000 0.0208 5 | 0.8000 0.0375 6 | 0.7000 0.0518 7 | 0.6000 0.0636 8 | 0.5000 0.0724 9 | 0.4000 0.0780 10 | 0.3000 0.0788 11 | 0.2500 0.0767 12 | 0.2000 0.0726 13 | 0.1500 0.0661 14 | 0.1000 0.0563 15 | 0.0750 0.0496 16 | 0.0500 0.0413 17 | 0.0250 0.0299 18 | 0.0125 0.0215 19 | 0.0000 0.0000 20 | 0.0125 -0.0165 21 | 0.0250 -0.0227 22 | 0.0500 -0.0301 23 | 0.0750 -0.0346 24 | 0.1000 -0.0375 25 | 0.1500 -0.0410 26 | 0.2000 -0.0423 27 | 0.2500 -0.0422 28 | 0.3000 -0.0412 29 | 0.4000 -0.0380 30 | 0.5000 -0.0334 31 | 0.6000 -0.0276 32 | 0.7000 -0.0214 33 | 0.8000 -0.0150 34 | 0.9000 -0.0082 35 | 0.9500 -0.0048 36 | 1.0000 -0.0013 37 | -------------------------------------------------------------------------------- /n/naca2415.dat: -------------------------------------------------------------------------------- 1 | NACA 2415 2 | 1.0000 0.0016 3 | 0.9500 0.0134 4 | 0.9000 0.0245 5 | 0.8000 0.0441 6 | 0.7000 0.0610 7 | 0.6000 0.0750 8 | 0.5000 0.0857 9 | 0.4000 0.0925 10 | 0.3000 0.0938 11 | 0.2500 0.0917 12 | 0.2000 0.0870 13 | 0.1500 0.0797 14 | 0.1000 0.0683 15 | 0.0750 0.0606 16 | 0.0500 0.0507 17 | 0.0250 0.0371 18 | 0.0125 0.0271 19 | 0.0000 0.0000 20 | 0.0125 -0.0206 21 | 0.0250 -0.0286 22 | 0.0500 -0.0384 23 | 0.0750 -0.0447 24 | 0.1000 -0.0490 25 | 0.1500 -0.0542 26 | 0.2000 -0.0566 27 | 0.2500 -0.0570 28 | 0.3000 -0.0562 29 | 0.4000 -0.0525 30 | 0.5000 -0.0467 31 | 0.6000 -0.0390 32 | 0.7000 -0.0305 33 | 0.8000 -0.0215 34 | 0.9000 -0.0117 35 | 0.9500 -0.0068 36 | 1.0000 -0.0016 37 | -------------------------------------------------------------------------------- /n/naca2418.dat: -------------------------------------------------------------------------------- 1 | NACA 2418 2 | 1.0000 0.0019 3 | 0.9500 0.0155 4 | 0.9000 0.0281 5 | 0.8000 0.0508 6 | 0.7000 0.0702 7 | 0.6000 0.0865 8 | 0.5000 0.0989 9 | 0.4000 0.1071 10 | 0.3000 0.1088 11 | 0.2500 0.1065 12 | 0.2000 0.1015 13 | 0.1500 0.0934 14 | 0.1000 0.0805 15 | 0.0750 0.0717 16 | 0.0500 0.0603 17 | 0.0250 0.0445 18 | 0.0125 0.0328 19 | 0.0000 0.0000 20 | 0.0125 -0.0245 21 | 0.0250 -0.0344 22 | 0.0500 -0.0468 23 | 0.0750 -0.0548 24 | 0.1000 -0.0603 25 | 0.1500 -0.0674 26 | 0.2000 -0.0709 27 | 0.2500 -0.0718 28 | 0.3000 -0.0712 29 | 0.4000 -0.0671 30 | 0.5000 -0.0599 31 | 0.6000 -0.0504 32 | 0.7000 -0.0397 33 | 0.8000 -0.0280 34 | 0.9000 -0.0153 35 | 0.9500 -0.0087 36 | 1.0000 -0.0019 37 | -------------------------------------------------------------------------------- /n/naca2421.dat: -------------------------------------------------------------------------------- 1 | NACA 2421 2 | 1.0000 0.0022 3 | 0.9500 0.0176 4 | 0.9000 0.0318 5 | 0.8000 0.0574 6 | 0.7000 0.0794 7 | 0.6000 0.0979 8 | 0.5000 0.1122 9 | 0.4000 0.1216 10 | 0.3000 0.1238 11 | 0.2500 0.1215 12 | 0.2000 0.1159 13 | 0.1500 0.1070 14 | 0.1000 0.0928 15 | 0.0750 0.0829 16 | 0.0500 0.0700 17 | 0.0250 0.0521 18 | 0.0125 0.0387 19 | 0.0000 0.0000 20 | 0.0125 -0.0282 21 | 0.0250 -0.0402 22 | 0.0500 -0.0551 23 | 0.0750 -0.0648 24 | 0.1000 -0.0718 25 | 0.1500 -0.0805 26 | 0.2000 -0.0852 27 | 0.2500 -0.0867 28 | 0.3000 -0.0862 29 | 0.4000 -0.0816 30 | 0.5000 -0.0731 31 | 0.6000 -0.0617 32 | 0.7000 -0.0487 33 | 0.8000 -0.0344 34 | 0.9000 -0.0188 35 | 0.9500 -0.0106 36 | 1.0000 -0.0022 37 | -------------------------------------------------------------------------------- /n/naca4412.dat: -------------------------------------------------------------------------------- 1 | NACA 4412 2 | 1.0000 0.0013 3 | 0.9500 0.0147 4 | 0.9000 0.0271 5 | 0.8000 0.0489 6 | 0.7000 0.0669 7 | 0.6000 0.0814 8 | 0.5000 0.0919 9 | 0.4000 0.0980 10 | 0.3000 0.0976 11 | 0.2500 0.0941 12 | 0.2000 0.0880 13 | 0.1500 0.0789 14 | 0.1000 0.0659 15 | 0.0750 0.0576 16 | 0.0500 0.0473 17 | 0.0250 0.0339 18 | 0.0125 0.0244 19 | 0.0000 0.0000 20 | 0.0125 -0.0143 21 | 0.0250 -0.0195 22 | 0.0500 -0.0249 23 | 0.0750 -0.0274 24 | 0.1000 -0.0286 25 | 0.1500 -0.0288 26 | 0.2000 -0.0274 27 | 0.2500 -0.0250 28 | 0.3000 -0.0226 29 | 0.4000 -0.0180 30 | 0.5000 -0.0140 31 | 0.6000 -0.0100 32 | 0.7000 -0.0065 33 | 0.8000 -0.0039 34 | 0.9000 -0.0022 35 | 0.9500 -0.0016 36 | 1.0000 -0.0013 37 | -------------------------------------------------------------------------------- /n/naca4418.dat: -------------------------------------------------------------------------------- 1 | NACA 4418 2 | 1.0000 0.0019 3 | 0.9500 0.0189 4 | 0.9000 0.0346 5 | 0.8000 0.0622 6 | 0.7000 0.0855 7 | 0.6000 0.1044 8 | 0.5000 0.1185 9 | 0.4000 0.1270 10 | 0.3000 0.1276 11 | 0.2500 0.1240 12 | 0.2000 0.1172 13 | 0.1500 0.1066 14 | 0.1000 0.0911 15 | 0.0750 0.0806 16 | 0.0500 0.0675 17 | 0.0250 0.0500 18 | 0.0125 0.0376 19 | 0.0000 0.0000 20 | 0.0125 -0.0211 21 | 0.0250 -0.0299 22 | 0.0500 -0.0406 23 | 0.0750 -0.0467 24 | 0.1000 -0.0506 25 | 0.1500 -0.0549 26 | 0.2000 -0.0556 27 | 0.2500 -0.0549 28 | 0.3000 -0.0526 29 | 0.4000 -0.0470 30 | 0.5000 -0.0402 31 | 0.6000 -0.0324 32 | 0.7000 -0.0245 33 | 0.8000 -0.0167 34 | 0.9000 -0.0093 35 | 0.9500 -0.0055 36 | 1.0000 -0.0019 37 | -------------------------------------------------------------------------------- /n/naca4421.dat: -------------------------------------------------------------------------------- 1 | NACA 4421 2 | 1.0000 0.0022 3 | 0.9500 0.0211 4 | 0.9000 0.0385 5 | 0.8000 0.0691 6 | 0.7000 0.0950 7 | 0.6000 0.1160 8 | 0.5000 0.1318 9 | 0.4000 0.1416 10 | 0.3000 0.1427 11 | 0.2500 0.1388 12 | 0.2000 0.1317 13 | 0.1500 0.1204 14 | 0.1000 0.1035 15 | 0.0750 0.0924 16 | 0.0500 0.0782 17 | 0.0250 0.0584 18 | 0.0125 0.0445 19 | 0.0000 0.0000 20 | 0.0125 -0.0242 21 | 0.0250 -0.0348 22 | 0.0500 -0.0478 23 | 0.0750 -0.0562 24 | 0.1000 -0.0615 25 | 0.1500 -0.0675 26 | 0.2000 -0.0698 27 | 0.2500 -0.0692 28 | 0.3000 -0.0676 29 | 0.4000 -0.0616 30 | 0.5000 -0.0534 31 | 0.6000 -0.0440 32 | 0.7000 -0.0335 33 | 0.8000 -0.0231 34 | 0.9000 -0.0127 35 | 0.9500 -0.0074 36 | 1.0000 -0.0022 37 | -------------------------------------------------------------------------------- /c/clarkv.dat: -------------------------------------------------------------------------------- 1 | CLARK V AIRFOIL 2 | 1.0000000 0.0014000 3 | 0.9500000 0.0163800 4 | 0.9000000 0.0299700 5 | 0.8000000 0.0519400 6 | 0.7000000 0.0688100 7 | 0.6000000 0.0809800 8 | 0.5000000 0.0886500 9 | 0.4000000 0.0914200 10 | 0.3000000 0.0885900 11 | 0.2000000 0.0795600 12 | 0.1500000 0.0715500 13 | 0.1000000 0.0601300 14 | 0.0750000 0.0522200 15 | 0.0500000 0.0424100 16 | 0.0250000 0.0289100 17 | 0.0125000 0.0195000 18 | 0.0000000 0.0000000 19 | 0.0125000 -.0138000 20 | 0.0250000 -.0182900 21 | 0.0500000 -.0230900 22 | 0.0750000 -.0255800 23 | 0.1000000 -.0273700 24 | 0.1500000 -.0289500 25 | 0.2000000 -.0294400 26 | 0.3000000 -.0278100 27 | 0.4000000 -.0241800 28 | 0.5000000 -.0201500 29 | 0.6000000 -.0161200 30 | 0.7000000 -.0120900 31 | 0.8000000 -.0080600 32 | 0.9000000 -.0040300 33 | 0.9500000 -.0020100 34 | 1.0000000 0.0000000 35 | -------------------------------------------------------------------------------- /c/clarkw.dat: -------------------------------------------------------------------------------- 1 | CLARK W AIRFOIL 2 | 1.0000000 0.0010000 3 | 0.9500000 0.0135500 4 | 0.9000000 0.0252100 5 | 0.8000000 0.0458200 6 | 0.7000000 0.0632300 7 | 0.6000000 0.0767400 8 | 0.5000000 0.0859500 9 | 0.4000000 0.0905600 10 | 0.3000000 0.0904700 11 | 0.2000000 0.0830800 12 | 0.1500000 0.0749400 13 | 0.1000000 0.0624900 14 | 0.0750000 0.0545200 15 | 0.0500000 0.0444400 16 | 0.0250000 0.0311700 17 | 0.0125000 0.0219900 18 | 0.0000000 0.0000000 19 | 0.0125000 -.0161100 20 | 0.0250000 -.0205300 21 | 0.0500000 -.0257600 22 | 0.0750000 -.0282800 23 | 0.1000000 -.0293100 24 | 0.1500000 -.0294700 25 | 0.2000000 -.0279200 26 | 0.3000000 -.0217300 27 | 0.4000000 -.0154400 28 | 0.5000000 -.0128500 29 | 0.6000000 -.0123600 30 | 0.7000000 -.0120700 31 | 0.8000000 -.0094800 32 | 0.9000000 -.0054900 33 | 0.9500000 -.0028500 34 | 1.0000000 0.0000000 35 | -------------------------------------------------------------------------------- /c/clarkx.dat: -------------------------------------------------------------------------------- 1 | CLARK X AIRFOIL 2 | 1.0000000 0.0012000 3 | 0.9500000 0.0129000 4 | 0.9000000 0.0240000 5 | 0.8000000 0.0442000 6 | 0.7000000 0.0615000 7 | 0.6000000 0.0755000 8 | 0.5000000 0.0852000 9 | 0.4000000 0.0900000 10 | 0.3000000 0.0890000 11 | 0.2000000 0.0808000 12 | 0.1500000 0.0728000 13 | 0.1000000 0.0608000 14 | 0.0750000 0.0522000 15 | 0.0500000 0.0416000 16 | 0.0250000 0.0276000 17 | 0.0125000 0.0186000 18 | 0.0000000 0.0000000 19 | 0.0125000 -.0163000 20 | 0.0250000 -.0220000 21 | 0.0500000 -.0272000 22 | 0.0750000 -.0296000 23 | 0.1000000 -.0310000 24 | 0.1500000 -.0318000 25 | 0.2000000 -.0317000 26 | 0.3000000 -.0280000 27 | 0.4000000 -.0240000 28 | 0.5000000 -.0200000 29 | 0.6000000 -.0160000 30 | 0.7000000 -.0120000 31 | 0.8000000 -.0080000 32 | 0.9000000 -.0040000 33 | 0.9500000 -.0020000 34 | 1.0000000 0.0000000 35 | -------------------------------------------------------------------------------- /c/clarkz.dat: -------------------------------------------------------------------------------- 1 | CLARK Z AIRFOIL 2 | 1.0000000 0.0012000 3 | 0.9500000 0.0135200 4 | 0.9000000 0.0252400 5 | 0.8000000 0.0466800 6 | 0.7000000 0.0652200 7 | 0.6000000 0.0804600 8 | 0.5000000 0.0916000 9 | 0.4000000 0.0977400 10 | 0.3000000 0.0981800 11 | 0.2000000 0.0905200 12 | 0.1500000 0.0820400 13 | 0.1000000 0.0693600 14 | 0.0750000 0.0609700 15 | 0.0500000 0.0506800 16 | 0.0250000 0.0355900 17 | 0.0125000 0.0239500 18 | 0.0000000 0.0000000 19 | 0.0125000 -.0169600 20 | 0.0250000 -.0207100 21 | 0.0500000 -.0235200 22 | 0.0750000 -.0245300 23 | 0.1000000 -.0245400 24 | 0.1500000 -.0234600 25 | 0.2000000 -.0220800 26 | 0.3000000 -.0193200 27 | 0.4000000 -.0165600 28 | 0.5000000 -.0138000 29 | 0.6000000 -.0110400 30 | 0.7000000 -.0082800 31 | 0.8000000 -.0055200 32 | 0.9000000 -.0027600 33 | 0.9500000 -.0013800 34 | 1.0000000 0.0000000 35 | -------------------------------------------------------------------------------- /d/davis.dat: -------------------------------------------------------------------------------- 1 | Davis AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9000000 0.0250000 4 | 0.8000000 0.0460000 5 | 0.7000000 0.0625000 6 | 0.6000000 0.0770000 7 | 0.5000000 0.0860000 8 | 0.4000000 0.0915000 9 | 0.3000000 0.0900000 10 | 0.2500000 0.0875000 11 | 0.2000000 0.0825000 12 | 0.1500000 0.0740000 13 | 0.1000000 0.0600000 14 | 0.0750000 0.0510000 15 | 0.0500000 0.0405000 16 | 0.0250000 0.0268000 17 | 0.0125000 0.0175000 18 | 0.0000000 0.0000000 19 | 0.0125000 -.0105000 20 | 0.0250000 -.0147000 21 | 0.0500000 -.0205000 22 | 0.0750000 -.0240000 23 | 0.1000000 -.0260000 24 | 0.1500000 -.0270000 25 | 0.2000000 -.0265000 26 | 0.2500000 -.0245000 27 | 0.3000000 -.0225000 28 | 0.4000000 -.0176500 29 | 0.5000000 -.0130000 30 | 0.6000000 -.0100000 31 | 0.7000000 -.0075000 32 | 0.8000000 -.0045000 33 | 0.9000000 -.0020000 34 | 1.0000000 0.0000000 35 | -------------------------------------------------------------------------------- /g/goe123.dat: -------------------------------------------------------------------------------- 1 | GOE 123 AIRFOIL 2 | 1.0000000 0.0020000 3 | 0.9000000 0.0220000 4 | 0.8000000 0.0420000 5 | 0.7000000 0.0590000 6 | 0.6000000 0.0720000 7 | 0.5000000 0.0800000 8 | 0.4000000 0.0840000 9 | 0.3000000 0.0830000 10 | 0.2500000 0.0805000 11 | 0.2000000 0.0760000 12 | 0.1500000 0.0685000 13 | 0.1000000 0.0570000 14 | 0.0750000 0.0487500 15 | 0.0500000 0.0395000 16 | 0.0250000 0.0262500 17 | 0.0125000 0.0181300 18 | 0.0000000 0.0000000 19 | 0.0125000 -.0088700 20 | 0.0250000 -.0077500 21 | 0.0500000 -.0035000 22 | 0.0750000 0.0017500 23 | 0.1000000 0.0070000 24 | 0.1500000 0.0175000 25 | 0.2000000 0.0230000 26 | 0.2500000 0.0265000 27 | 0.3000000 0.0290000 28 | 0.4000000 0.0300000 29 | 0.5000000 0.0270000 30 | 0.6000000 0.0220000 31 | 0.7000000 0.0170000 32 | 0.8000000 0.0110000 33 | 0.9000000 0.0060000 34 | 1.0000000 0.0000000 35 | -------------------------------------------------------------------------------- /g/goe14.dat: -------------------------------------------------------------------------------- 1 | GOE 14 AIRFOIL 2 | 1.0000000 0.0006500 3 | 0.9497899 0.0119500 4 | 0.8995800 0.0235600 5 | 0.7991700 0.0465700 6 | 0.6987800 0.0685700 7 | 0.5984300 0.0878800 8 | 0.4981700 0.1025900 9 | 0.3979700 0.1136000 10 | 0.2978800 0.1188200 11 | 0.1979700 0.1137300 12 | 0.1481200 0.1051400 13 | 0.0984000 0.0897600 14 | 0.0735800 0.0793100 15 | 0.0488400 0.0648700 16 | 0.0242000 0.0446300 17 | 0.0119700 0.0297100 18 | 0.0000000 0.0000000 19 | 0.0128100 -.0172700 20 | 0.0253200 -.0180500 21 | 0.0502300 -.0131000 22 | 0.0750600 -.0031600 23 | 0.0999100 0.0050800 24 | 0.1497600 0.0131700 25 | 0.1997400 0.0163100 26 | 0.2996500 0.0198500 27 | 0.3996900 0.0183800 28 | 0.4997200 0.0159200 29 | 0.5997600 0.0137100 30 | 0.6998100 0.0104900 31 | 0.7998800 0.0067800 32 | 0.8999299 0.0029500 33 | 0.9499800 0.0010600 34 | 1.0000000 -.0006500 35 | -------------------------------------------------------------------------------- /g/goe15.dat: -------------------------------------------------------------------------------- 1 | GOE 15 AIRFOIL 2 | 1.0000000 0.0000000 3 | 0.9497800 0.0142300 4 | 0.8995900 0.0269600 5 | 0.7992100 0.0519300 6 | 0.6988800 0.0733900 7 | 0.5985600 0.0938600 8 | 0.4983300 0.1090200 9 | 0.3982000 0.1182900 10 | 0.2981200 0.1225600 11 | 0.1982500 0.1144300 12 | 0.1484100 0.1039700 13 | 0.0986500 0.0882100 14 | 0.0738200 0.0768300 15 | 0.0490500 0.0621500 16 | 0.0243600 0.0417700 17 | 0.0120800 0.0273800 18 | 0.0000000 0.0000000 19 | 0.0127100 -.0136100 20 | 0.0252300 -.0149100 21 | 0.0500800 -.0050300 22 | 0.0749300 0.0048500 23 | 0.0998100 0.0127300 24 | 0.1496500 0.0229900 25 | 0.1995800 0.0277500 26 | 0.2995000 0.0325800 27 | 0.3995300 0.0308100 28 | 0.4995800 0.0273400 29 | 0.5996900 0.0205800 30 | 0.6998100 0.0121100 31 | 0.7999000 0.0062400 32 | 0.8999800 0.0014700 33 | 0.9499900 0.0005300 34 | 1.0000000 0.0000000 35 | -------------------------------------------------------------------------------- /g/goe177.dat: -------------------------------------------------------------------------------- 1 | GOE 177 AIRFOIL 2 | 1.0000000 0.0020000 3 | 0.9500000 0.0115500 4 | 0.9000000 0.0211000 5 | 0.8000000 0.0372000 6 | 0.7000000 0.0513000 7 | 0.6000000 0.0644000 8 | 0.5000000 0.0755000 9 | 0.4000000 0.0836000 10 | 0.3000000 0.0867000 11 | 0.2000000 0.0818000 12 | 0.1500000 0.0733500 13 | 0.1000000 0.0599000 14 | 0.0750000 0.0516800 15 | 0.0500000 0.0394500 16 | 0.0250000 0.0267200 17 | 0.0125000 0.0151100 18 | 0.0000000 0.0000000 19 | 0.0125000 -.0058900 20 | 0.0250000 -.0077700 21 | 0.0500000 -.0085500 22 | 0.0750000 -.0063200 23 | 0.1000000 -.0041000 24 | 0.1500000 0.0003500 25 | 0.2000000 0.0048000 26 | 0.3000000 0.0127000 27 | 0.4000000 0.0176000 28 | 0.5000000 0.0175000 29 | 0.6000000 0.0154000 30 | 0.7000000 0.0123000 31 | 0.8000000 0.0082000 32 | 0.9000000 0.0041000 33 | 0.9500000 0.0025500 34 | 1.0000000 0.0000000 35 | -------------------------------------------------------------------------------- /g/goe178.dat: -------------------------------------------------------------------------------- 1 | GOE 178 AIRFOIL 2 | 1.0000000 0.0030000 3 | 0.9500000 0.0112500 4 | 0.9000000 0.0205000 5 | 0.8000000 0.0360000 6 | 0.7000000 0.0505000 7 | 0.6000000 0.0630000 8 | 0.5000000 0.0735000 9 | 0.4000000 0.0820000 10 | 0.3000000 0.0865000 11 | 0.2000000 0.0800000 12 | 0.1500000 0.0722500 13 | 0.1000000 0.0585000 14 | 0.0750000 0.0491200 15 | 0.0500000 0.0377500 16 | 0.0250000 0.0253700 17 | 0.0125000 0.0161900 18 | 0.0000000 0.0000000 19 | 0.0125000 -.0108100 20 | 0.0250000 -.0126300 21 | 0.0500000 -.0142500 22 | 0.0750000 -.0128800 23 | 0.1000000 -.0110000 24 | 0.1500000 -.0077500 25 | 0.2000000 -.0040000 26 | 0.3000000 0.0015000 27 | 0.4000000 0.0060000 28 | 0.5000000 0.0085000 29 | 0.6000000 0.0090000 30 | 0.7000000 0.0085000 31 | 0.8000000 0.0070000 32 | 0.9000000 0.0045000 33 | 0.9500000 0.0022500 34 | 1.0000000 0.0000000 35 | -------------------------------------------------------------------------------- /g/goe195.dat: -------------------------------------------------------------------------------- 1 | GOE 195 AIRFOIL 2 | 1.0000000 0.0020000 3 | 0.9500000 0.0141500 4 | 0.9000000 0.0253000 5 | 0.8000000 0.0446000 6 | 0.7000000 0.0599000 7 | 0.6000000 0.0732000 8 | 0.5000000 0.0815000 9 | 0.4000000 0.0878000 10 | 0.3000000 0.0871000 11 | 0.2000000 0.0784000 12 | 0.1500000 0.0705500 13 | 0.1000000 0.0587000 14 | 0.0750000 0.0512800 15 | 0.0500000 0.0418500 16 | 0.0250000 0.0284200 17 | 0.0125000 0.0202100 18 | 0.0000000 0.0000000 19 | 0.0125000 -.0117900 20 | 0.0250000 -.0135700 21 | 0.0500000 -.0151500 22 | 0.0750000 -.0157200 23 | 0.1000000 -.0153000 24 | 0.1500000 -.0124500 25 | 0.2000000 -.0076000 26 | 0.3000000 0.0051000 27 | 0.4000000 0.0138000 28 | 0.5000000 0.0205000 29 | 0.6000000 0.0242000 30 | 0.7000000 0.0229000 31 | 0.8000000 0.0166000 32 | 0.9000000 0.0083000 33 | 0.9500000 0.0041500 34 | 1.0000000 0.0000000 35 | -------------------------------------------------------------------------------- /g/goe257.dat: -------------------------------------------------------------------------------- 1 | GOE 257 AIRFOIL 2 | 1.0000000 0.0064000 3 | 0.9499500 0.0148400 4 | 0.8999299 0.0232800 5 | 0.7998700 0.0394600 6 | 0.6998300 0.0526400 7 | 0.5997900 0.0661200 8 | 0.4997500 0.0776000 9 | 0.3997300 0.0836800 10 | 0.2997300 0.0849600 11 | 0.1997500 0.0766400 12 | 0.1497800 0.0694800 13 | 0.0998200 0.0575200 14 | 0.0748400 0.0484400 15 | 0.0498800 0.0376600 16 | 0.0249200 0.0252800 17 | 0.0124500 0.0161400 18 | 0.0000000 0.0000000 19 | 0.0125300 -.0095600 20 | 0.0250300 -.0095200 21 | 0.0500300 -.0089400 22 | 0.0750300 -.0082600 23 | 0.1000200 -.0071800 24 | 0.1500200 -.0059200 25 | 0.2000200 -.0046600 26 | 0.3000100 -.0033400 27 | 0.4000100 -.0025200 28 | 0.5000100 -.0027000 29 | 0.6000100 -.0023800 30 | 0.7000100 -.0030600 31 | 0.8000100 -.0038400 32 | 0.9000200 -.0051200 33 | 0.9500200 -.0065600 34 | 1.0000000 -.0064000 35 | -------------------------------------------------------------------------------- /g/goe264.dat: -------------------------------------------------------------------------------- 1 | GOE 264 AIRFOIL 2 | 1.0000000 0.0032000 3 | 0.9499199 0.0126800 4 | 0.8998500 0.0228600 5 | 0.7997400 0.0409200 6 | 0.6996400 0.0567800 7 | 0.5995600 0.0689400 8 | 0.4994900 0.0795000 9 | 0.3994500 0.0863600 10 | 0.2892600 0.0880200 11 | 0.2017300 0.0818400 12 | 0.1495400 0.0723600 13 | 0.0996300 0.0577400 14 | 0.0746800 0.0492800 15 | 0.0497600 0.0382200 16 | 0.0276500 0.0267600 17 | 0.0122100 0.0165200 18 | 0.0000000 0.0000000 19 | 0.0125600 -.0092200 20 | 0.0261500 -.0109600 21 | 0.0500500 -.0079800 22 | 0.0750300 -.0040200 23 | 0.1000000 0.0006400 24 | 0.1499400 0.0100600 25 | 0.1998900 0.0172800 26 | 0.2998300 0.0259200 27 | 0.3998300 0.0265600 28 | 0.4998500 0.0235000 29 | 0.5998700 0.0198400 30 | 0.6999100 0.0145800 31 | 0.7999400 0.0094200 32 | 0.8999700 0.0046600 33 | 0.9499900 0.0012800 34 | 1.0000000 -.0032000 35 | -------------------------------------------------------------------------------- /g/goe265.dat: -------------------------------------------------------------------------------- 1 | GOE 265 AIRFOIL 2 | 1.0000000 0.0010500 3 | 0.9498900 0.0118000 4 | 0.8998100 0.0215500 5 | 0.7996300 0.0416600 6 | 0.6994600 0.0602600 7 | 0.5993000 0.0780600 8 | 0.4991700 0.0929700 9 | 0.3990700 0.1035700 10 | 0.2990400 0.1069800 11 | 0.1990900 0.1012800 12 | 0.1491700 0.0923400 13 | 0.0993000 0.0778900 14 | 0.0743800 0.0689700 15 | 0.0494900 0.0564400 16 | 0.0246500 0.0390200 17 | 0.0122600 0.0266100 18 | 0.0000000 0.0000000 19 | 0.0125700 -.0082900 20 | 0.0250900 -.0097800 21 | 0.0500700 -.0075500 22 | 0.0750200 -.0023300 23 | 0.0999600 0.0039900 24 | 0.1498600 0.0159400 25 | 0.1997700 0.0252900 26 | 0.2996600 0.0376800 27 | 0.3996300 0.0415800 28 | 0.4996400 0.0399700 29 | 0.5996900 0.0346700 30 | 0.6997600 0.0266600 31 | 0.7998500 0.0171600 32 | 0.8999299 0.0073500 33 | 0.9499800 0.0027000 34 | 1.0000000 -.0010500 35 | -------------------------------------------------------------------------------- /g/goe269.dat: -------------------------------------------------------------------------------- 1 | GOE 269 AIRFOIL 2 | 1.0000000 0.0029000 3 | 0.9498600 0.0118000 4 | 0.8997700 0.0197100 5 | 0.7995700 0.0365100 6 | 0.6993901 0.0512200 7 | 0.5992300 0.0643300 8 | 0.4991000 0.0752400 9 | 0.3990400 0.0809500 10 | 0.2990200 0.0824600 11 | 0.1990900 0.0764700 12 | 0.1491800 0.0691000 13 | 0.0993100 0.0585000 14 | 0.0744100 0.0515000 15 | 0.0495100 0.0420000 16 | 0.0246600 0.0287900 17 | 0.0122700 0.0192500 18 | 0.0000000 0.0000000 19 | 0.0126700 -.0116000 20 | 0.0251700 -.0135000 21 | 0.0501300 -.0113000 22 | 0.0750700 -.0060100 23 | 0.1000200 -.0017000 24 | 0.1499300 0.0057500 25 | 0.1998600 0.0113800 26 | 0.2998000 0.0165700 27 | 0.3997700 0.0195600 28 | 0.4997600 0.0203500 29 | 0.5997800 0.0182400 30 | 0.6998300 0.0143300 31 | 0.7999000 0.0085200 32 | 0.8999700 0.0022100 33 | 0.9500000 -.0002900 34 | 1.0000000 -.0029000 35 | -------------------------------------------------------------------------------- /g/goe284.dat: -------------------------------------------------------------------------------- 1 | GOE 284 AIRFOIL 2 | 1.0000000 0.0029500 3 | 0.9492300 0.0150500 4 | 0.8985200 0.0288600 5 | 0.7971300 0.0560700 6 | 0.6958600 0.0808900 7 | 0.5947200 0.1033200 8 | 0.4937100 0.1229500 9 | 0.3930100 0.1366000 10 | 0.2929700 0.1373900 11 | 0.1935400 0.1264000 12 | 0.1441800 0.1138700 13 | 0.0952400 0.0931700 14 | 0.0708600 0.0810200 15 | 0.0466400 0.0657900 16 | 0.0227000 0.0450600 17 | 0.0108800 0.0317600 18 | 0.0000000 0.0000000 19 | 0.0137300 -.0240000 20 | 0.0266100 -.0315400 21 | 0.0520900 -.0408400 22 | 0.0772900 -.0446500 23 | 0.1023200 -.0453700 24 | 0.1523100 -.0451100 25 | 0.2022400 -.0437600 26 | 0.3019800 -.0386500 27 | 0.4017200 -.0335500 28 | 0.5014600 -.0284500 29 | 0.6012000 -.0233500 30 | 0.7009300 -.0182500 31 | 0.8006700 -.0131500 32 | 0.9004100 -.0080400 33 | 0.9502800 -.0054900 34 | 1.0000000 -.0029500 35 | -------------------------------------------------------------------------------- /g/goe286.dat: -------------------------------------------------------------------------------- 1 | GOE 286 AIRFOIL 2 | 1.0000000 0.0025000 3 | 0.9498800 0.0101900 4 | 0.8997600 0.0197800 5 | 0.7995600 0.0362500 6 | 0.6993700 0.0520300 7 | 0.5992100 0.0644100 8 | 0.4990600 0.0766900 9 | 0.3989700 0.0842700 10 | 0.2989300 0.0877500 11 | 0.1989800 0.0836300 12 | 0.1490700 0.0759200 13 | 0.0992200 0.0636100 14 | 0.0743100 0.0568100 15 | 0.0494500 0.0447000 16 | 0.0246200 0.0315000 17 | 0.0122500 0.0207500 18 | 0.0000000 0.0000000 19 | 0.0126400 -.0116500 20 | 0.0251600 -.0131900 21 | 0.0501700 -.0140900 22 | 0.0751600 -.0132800 23 | 0.1001500 -.0122800 24 | 0.1501200 -.0099700 25 | 0.2001000 -.0081600 26 | 0.3000700 -.0057400 27 | 0.4000400 -.0033200 28 | 0.5000300 -.0027000 29 | 0.6000300 -.0020800 30 | 0.7000300 -.0020600 31 | 0.8000400 -.0031400 32 | 0.9000400 -.0031200 33 | 0.9500400 -.0031100 34 | 1.0000000 -.0025000 35 | -------------------------------------------------------------------------------- /g/goe287.dat: -------------------------------------------------------------------------------- 1 | GOE 287 AIRFOIL 2 | 1.0000000 0.0025000 3 | 0.9499300 0.0088900 4 | 0.8998600 0.0178900 5 | 0.7997200 0.0346800 6 | 0.6995700 0.0526700 7 | 0.5994400 0.0689600 8 | 0.4993300 0.0828400 9 | 0.3992500 0.0926300 10 | 0.2992500 0.0923200 11 | 0.1993100 0.0851100 12 | 0.1493700 0.0777100 13 | 0.0994800 0.0637100 14 | 0.0745600 0.0547000 15 | 0.0496600 0.0423000 16 | 0.0247900 0.0261000 17 | 0.0123600 0.0171000 18 | 0.0000000 0.0000000 19 | 0.0125800 -.0098000 20 | 0.0250800 -.0104000 21 | 0.0500700 -.0089900 22 | 0.0750600 -.0070900 23 | 0.1000400 -.0050900 24 | 0.1500200 -.0022800 25 | 0.2000100 -.0001000 26 | 0.2999700 0.0036300 27 | 0.3999600 0.0050400 28 | 0.4999600 0.0052500 29 | 0.5999700 0.0036600 30 | 0.6999800 0.0018700 31 | 0.8000000 0.0005800 32 | 0.9000100 -.0009100 33 | 0.9500100 -.0017000 34 | 1.0000000 -.0025000 35 | -------------------------------------------------------------------------------- /g/goe288.dat: -------------------------------------------------------------------------------- 1 | GOE 288 AIRFOIL 2 | 1.0000000 0.0029500 3 | 0.9490300 0.0184800 4 | 0.8982800 0.0329200 5 | 0.7968600 0.0599200 6 | 0.6956000 0.0840100 7 | 0.5944900 0.1052200 8 | 0.4935400 0.1234400 9 | 0.3929200 0.1352700 10 | 0.2928500 0.1365300 11 | 0.1933700 0.1266200 12 | 0.1440600 0.1134400 13 | 0.0951800 0.0921800 14 | 0.0709000 0.0784100 15 | 0.0467300 0.0624500 16 | 0.0228300 0.0414000 17 | 0.0110700 0.0272800 18 | 0.0000000 0.0000000 19 | 0.0137300 -.0233800 20 | 0.0265600 -.0298100 21 | 0.0519500 -.0372800 22 | 0.0771900 -.0417600 23 | 0.1023100 -.0440400 24 | 0.1523800 -.0455200 25 | 0.2023400 -.0447100 26 | 0.3019200 -.0365900 27 | 0.4012400 -.0237000 28 | 0.5006600 -.0125900 29 | 0.6002400 -.0044800 30 | 0.6999900 0.0001400 31 | 0.7999300 0.0012800 32 | 0.8999700 0.0006100 33 | 0.9500500 -.0009600 34 | 1.0000000 -.0029500 35 | -------------------------------------------------------------------------------- /g/goe298.dat: -------------------------------------------------------------------------------- 1 | GOE 298 AIRFOIL 2 | 1.0000000 0.0029500 3 | 0.9494700 0.0127600 4 | 0.8990900 0.0218700 5 | 0.7982100 0.0430900 6 | 0.6973300 0.0626500 7 | 0.5966500 0.0809300 8 | 0.4960800 0.0944600 9 | 0.3956900 0.1040000 10 | 0.2956900 0.1039600 11 | 0.1959500 0.0988200 12 | 0.1462200 0.0912600 13 | 0.0967700 0.0789100 14 | 0.0720800 0.0703900 15 | 0.0475900 0.0581700 16 | 0.0233400 0.0399700 17 | 0.0113300 0.0282700 18 | 0.0000000 0.0000000 19 | 0.0135800 -.0260400 20 | 0.0264000 -.0338100 21 | 0.0516700 -.0402600 22 | 0.0767100 -.0412200 23 | 0.1016200 -.0389900 24 | 0.1514100 -.0340200 25 | 0.2012000 -.0289600 26 | 0.3008300 -.0201300 27 | 0.4005400 -.0130000 28 | 0.5004100 -.0094700 29 | 0.6002900 -.0070200 30 | 0.7002400 -.0055300 31 | 0.8001700 -.0041300 32 | 0.9001000 -.0023900 33 | 0.9500800 -.0020200 34 | 1.0000000 -.0029500 35 | --------------------------------------------------------------------------------