├── .gitignore
├── Bell_Christopher
├── VLM.ipynb
└── VLM_resources
│ ├── General_VLM.png
│ ├── General_VLM.xcf
│ ├── Single_horseshoe_vortex.png
│ ├── Single_horseshoe_vortex.xcf
│ ├── VLM_Coords.xlsx
│ ├── VLM_Example_Airfoil.txt
│ ├── Vortex_Notation.png
│ ├── Vortex_Notation.xcf
│ ├── control_point.png
│ ├── control_point.xcf
│ ├── numericalmoocstyle.css
│ ├── validation_image.png
│ ├── validation_image.xcf
│ ├── vector_elements.png
│ └── vector_elements.xcf
├── Bornemeier
├── .ipynb_checkpoints
│ ├── Final Project-checkpoint.ipynb
│ └── dataexportforxflr5-checkpoint.ipynb
├── Book1.csv
├── Final Project.ipynb
├── Styles
│ ├── custom.css
│ └── numericalmoocstyle.css
├── airfoila.dat
├── b707a.txt
├── b707b.txt
├── b707c.txt
├── b707d.txt
├── b707e.txt
├── dataexportforxflr5.ipynb
├── figures
│ ├── a.png
│ ├── b.png
│ ├── cclalpha1.png
│ ├── cropped ppt 707c.png
│ ├── d.png
│ ├── dash80.jpg
│ ├── dash80.png
│ ├── dash80rollout.jpg
│ ├── dash80rollout.png
│ ├── dclalpha.png
│ └── e.png
└── resources
│ ├── JetSet.ttf
│ ├── JetSetItalic.ttf
│ ├── b707a.txt
│ ├── b707b.txt
│ ├── b707c.txt
│ ├── b707d.txt
│ ├── b707e.txt
│ └── others
│ ├── b707a.dat
│ ├── b707b.dat
│ ├── b707c.dat
│ ├── b707d.dat
│ └── b707e.dat
├── GeorgeTeel
├── .ipynb_checkpoints
│ └── Orlyonok Ekranoplan-checkpoint.ipynb
├── 10ms
│ ├── 00.csv
│ ├── 02.csv
│ ├── 03.csv
│ ├── 04.csv
│ ├── 05.csv
│ ├── 06.csv
│ ├── 07.csv
│ ├── 09.csv
│ ├── 12.csv
│ ├── 17.csv
│ ├── CLvsAlpha.csv
│ └── Data.csv
├── 2_5ms
│ ├── 00.csv
│ ├── 02.csv
│ ├── 03.csv
│ ├── 04.csv
│ ├── 05.csv
│ ├── 06.csv
│ ├── 06.xlsx
│ ├── 07.csv
│ ├── 09.csv
│ ├── 09.xlsx
│ ├── 12.csv
│ └── 17.csv
├── 3ms
│ ├── 00.csv
│ ├── 02.csv
│ ├── 03.csv
│ ├── 04.csv
│ ├── 05.csv
│ ├── 06.csv
│ ├── 07.csv
│ ├── 09.csv
│ ├── 10.csv
│ └── 16.csv
├── 5ms
│ ├── 00.csv
│ ├── 02.csv
│ ├── 03.csv
│ ├── 04.csv
│ ├── 05.csv
│ ├── 06.csv
│ ├── 08.csv
│ ├── 10.csv
│ ├── 15.csv
│ └── 21.csv
├── BannerLow.png
├── BannerThin.png
├── Ekranoplan.jpg
├── FittedCurve.png
├── Full10ms
│ ├── 00.csv
│ ├── 04.csv
│ ├── 05.csv
│ ├── 06.csv
│ ├── 07.csv
│ ├── 08.csv
│ ├── 09.csv
│ └── 10.csv
├── Full20ms
│ ├── 0.4.csv
│ ├── 00.csv
│ ├── 04.csv
│ ├── 05.csv
│ ├── 06.csv
│ ├── 07.csv
│ ├── 08.csv
│ ├── 09.csv
│ └── 10.csv
├── Full5ms
│ ├── 00.csv
│ ├── 05.csv
│ ├── 06.csv
│ ├── 07.csv
│ ├── 08.csv
│ ├── 09.csv
│ └── 10.csv
├── Orlyonok Ekranoplan.ipynb
├── Plane.gif
├── SectionalBuildup.png
├── SectionalBuildup2.png
├── SectionalBuildup3.png
├── SectionalBuildup4.png
├── Thumbs.db
├── TitleThin.png
├── Wing.gif
├── XFLR5.png
├── XFLR5Wing.png
├── blender.png
├── body1.png
├── body2.png
├── body3.png
└── project.css
├── Ground-Effect-in-Vortex-Panel-Method
├── Ground-Effect-in-Vortex-Panel-Method.ipynb
└── resources
│ ├── NACA0012_N=100
│ ├── NACA4412_N=100
│ ├── NACA4412_cl.png
│ ├── NACA4412_inv_N=100
│ ├── custom.css
│ ├── data
│ ├── lotus79.jpg
│ └── panel.png
├── Project - Michael J Carter
├── .ipynb_checkpoints
│ └── Project - Michael J Carter-checkpoint.ipynb
├── Project - Michael J Carter.ipynb
├── resources
│ └── naca0012.dat
└── styles
│ └── custom.css
├── README.md
└── cparvini
├── .ipynb_checkpoints
└── FlapNotebook-checkpoint.ipynb
├── FlapNotebook.ipynb
├── FowlerFlapPresentation.pdf
├── NACA23012_FlapFoil.csv
├── NACA23012_MainFoil.csv
├── NASAFowler.jpg
├── junkersFlap.gif
├── styles
└── custom.css
└── theta_20_plots.jpg
/.gitignore:
--------------------------------------------------------------------------------
1 | #################
2 | ## Eclipse
3 | #################
4 |
5 | *.pydevproject
6 | .project
7 | .metadata
8 | bin/
9 | tmp/
10 | *.tmp
11 | *.bak
12 | *.swp
13 | *~.nib
14 | local.properties
15 | .classpath
16 | .settings/
17 | .loadpath
18 |
19 | # External tool builders
20 | .externalToolBuilders/
21 |
22 | # Locally stored "Eclipse launch configurations"
23 | *.launch
24 |
25 | # CDT-specific
26 | .cproject
27 |
28 | # PDT-specific
29 | .buildpath
30 |
31 |
32 | #################
33 | ## Visual Studio
34 | #################
35 |
36 | ## Ignore Visual Studio temporary files, build results, and
37 | ## files generated by popular Visual Studio add-ons.
38 |
39 | # User-specific files
40 | *.suo
41 | *.user
42 | *.sln.docstates
43 |
44 | # Build results
45 |
46 | [Dd]ebug/
47 | [Rr]elease/
48 | x64/
49 | build/
50 | [Bb]in/
51 | [Oo]bj/
52 |
53 | # MSTest test Results
54 | [Tt]est[Rr]esult*/
55 | [Bb]uild[Ll]og.*
56 |
57 | *_i.c
58 | *_p.c
59 | *.ilk
60 | *.meta
61 | *.obj
62 | *.pch
63 | *.pdb
64 | *.pgc
65 | *.pgd
66 | *.rsp
67 | *.sbr
68 | *.tlb
69 | *.tli
70 | *.tlh
71 | *.tmp
72 | *.tmp_proj
73 | *.log
74 | *.vspscc
75 | *.vssscc
76 | .builds
77 | *.pidb
78 | *.log
79 | *.scc
80 |
81 | # Visual C++ cache files
82 | ipch/
83 | *.aps
84 | *.ncb
85 | *.opensdf
86 | *.sdf
87 | *.cachefile
88 |
89 | # Visual Studio profiler
90 | *.psess
91 | *.vsp
92 | *.vspx
93 |
94 | # Guidance Automation Toolkit
95 | *.gpState
96 |
97 | # ReSharper is a .NET coding add-in
98 | _ReSharper*/
99 | *.[Rr]e[Ss]harper
100 |
101 | # TeamCity is a build add-in
102 | _TeamCity*
103 |
104 | # DotCover is a Code Coverage Tool
105 | *.dotCover
106 |
107 | # NCrunch
108 | *.ncrunch*
109 | .*crunch*.local.xml
110 |
111 | # Installshield output folder
112 | [Ee]xpress/
113 |
114 | # DocProject is a documentation generator add-in
115 | DocProject/buildhelp/
116 | DocProject/Help/*.HxT
117 | DocProject/Help/*.HxC
118 | DocProject/Help/*.hhc
119 | DocProject/Help/*.hhk
120 | DocProject/Help/*.hhp
121 | DocProject/Help/Html2
122 | DocProject/Help/html
123 |
124 | # Click-Once directory
125 | publish/
126 |
127 | # Publish Web Output
128 | *.Publish.xml
129 | *.pubxml
130 | *.publishproj
131 |
132 | # NuGet Packages Directory
133 | ## TODO: If you have NuGet Package Restore enabled, uncomment the next line
134 | #packages/
135 |
136 | # Windows Azure Build Output
137 | csx
138 | *.build.csdef
139 |
140 | # Windows Store app package directory
141 | AppPackages/
142 |
143 | # Others
144 | sql/
145 | *.Cache
146 | ClientBin/
147 | [Ss]tyle[Cc]op.*
148 | ~$*
149 | *~
150 | *.dbmdl
151 | *.[Pp]ublish.xml
152 | *.pfx
153 | *.publishsettings
154 |
155 | # RIA/Silverlight projects
156 | Generated_Code/
157 |
158 | # Backup & report files from converting an old project file to a newer
159 | # Visual Studio version. Backup files are not needed, because we have git ;-)
160 | _UpgradeReport_Files/
161 | Backup*/
162 | UpgradeLog*.XML
163 | UpgradeLog*.htm
164 |
165 | # SQL Server files
166 | App_Data/*.mdf
167 | App_Data/*.ldf
168 |
169 | #############
170 | ## Windows detritus
171 | #############
172 |
173 | # Windows image file caches
174 | Thumbs.db
175 | ehthumbs.db
176 |
177 | # Folder config file
178 | Desktop.ini
179 |
180 | # Recycle Bin used on file shares
181 | $RECYCLE.BIN/
182 |
183 | # Mac crap
184 | .DS_Store
185 |
186 |
187 | #############
188 | ## Python
189 | #############
190 |
191 | *.py[cod]
192 |
193 | # Packages
194 | *.egg
195 | *.egg-info
196 | dist/
197 | build/
198 | eggs/
199 | parts/
200 | var/
201 | sdist/
202 | develop-eggs/
203 | .installed.cfg
204 |
205 | # Installer logs
206 | pip-log.txt
207 |
208 | # Unit test / coverage reports
209 | .coverage
210 | .tox
211 |
212 | #Translations
213 | *.mo
214 |
215 | #Mr Developer
216 | .mr.developer.cfg
217 |
218 | #checkpoints
219 | .ipynb_checkpoints
220 |
--------------------------------------------------------------------------------
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1 | 0 0 0
2 | 1 0.25 -0.25
3 | 2 0.5 -0.5
4 | 3 0.75 -0.75
5 | 4 1 -1
6 | 5 1.25 -1.25
7 | 6 1.5 -1.5
8 | 7 1.75 -1.75
9 | 8 2 -2
10 | 9 2.25 -2.25
11 | 10 2.5 -2.5
12 | 21 2.5 -3.5
13 | 20 2.25 -3.25
14 | 19 2 -3
15 | 18 1.75 -2.75
16 | 17 1.5 -2.5
17 | 16 1.25 -2.25
18 | 15 1 -2
19 | 14 0.75 -1.75
20 | 13 0.5 -1.5
21 | 12 0.25 -1.25
22 | 11 0 -1
23 | 22 0 -0.01
24 |
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1 |
2 |
3 |
4 |
5 |
6 |
126 |
142 |
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/Bornemeier/.ipynb_checkpoints/dataexportforxflr5-checkpoint.ipynb:
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1 | {
2 | "metadata": {
3 | "name": "",
4 | "signature": "sha256:d8d029696ab34ef5016656cf6baa84178105b3f1c2653c2eae51aaf2c9b6ba35"
5 | },
6 | "nbformat": 3,
7 | "nbformat_minor": 0,
8 | "worksheets": [
9 | {
10 | "cells": [
11 | {
12 | "cell_type": "code",
13 | "collapsed": false,
14 | "input": [
15 | "import math\n",
16 | "import numpy\n",
17 | "import sympy\n",
18 | "from matplotlib import pyplot\n",
19 | "% matplotlib inline\n",
20 | "import csv"
21 | ],
22 | "language": "python",
23 | "metadata": {},
24 | "outputs": [],
25 | "prompt_number": 2
26 | },
27 | {
28 | "cell_type": "code",
29 | "collapsed": false,
30 | "input": [
31 | "# This cell imports and plots the five airfoil variants of the Boeing 707.\n",
32 | "#####import the first airfoil 707a#####\n",
33 | "file_name = './b707a.txt' \n",
34 | "x,y = numpy.loadtxt(file_name,dtype=float,unpack=True )\n",
35 | "#Rearrange data into format that is expected from Barba's team code\n",
36 | "L = len(x);\n",
37 | "xpart1 = x[0:L/2];\n",
38 | "xpart2 = xpart1[::-1]\n",
39 | "xcont = numpy.linspace(0,L,L)\n",
40 | "xcont[:L/2]=xpart2;\n",
41 | "xcont[L/2:]=x[L/2:]\n",
42 | "x[0:L] = xcont[0:L]\n",
43 | "ypart1 = y[0:L/2];\n",
44 | "ypart2 = ypart1[::-1]\n",
45 | "ycont = numpy.linspace(0,L,L)\n",
46 | "ycont[:L/2]=ypart2;\n",
47 | "ycont[L/2:]=y[L/2:]\n",
48 | "y[0:L] = ycont[0:L]"
49 | ],
50 | "language": "python",
51 | "metadata": {},
52 | "outputs": [],
53 | "prompt_number": 3
54 | },
55 | {
56 | "cell_type": "code",
57 | "collapsed": false,
58 | "input": [
59 | "dataA = numpy.zeros((122,2));\n",
60 | "\n",
61 | "dataA.shape"
62 | ],
63 | "language": "python",
64 | "metadata": {},
65 | "outputs": [
66 | {
67 | "metadata": {},
68 | "output_type": "pyout",
69 | "prompt_number": 29,
70 | "text": [
71 | "(122L, 2L)"
72 | ]
73 | }
74 | ],
75 | "prompt_number": 29
76 | },
77 | {
78 | "cell_type": "code",
79 | "collapsed": false,
80 | "input": [
81 | "dataA[:,0] = x[:];\n",
82 | "dataA[:,0] = y[:];"
83 | ],
84 | "language": "python",
85 | "metadata": {},
86 | "outputs": [],
87 | "prompt_number": 30
88 | },
89 | {
90 | "cell_type": "code",
91 | "collapsed": false,
92 | "input": [
93 | "numpy.savetxt('./dataA.txt',dataA,delimiter =',')"
94 | ],
95 | "language": "python",
96 | "metadata": {},
97 | "outputs": [],
98 | "prompt_number": 24
99 | },
100 | {
101 | "cell_type": "code",
102 | "collapsed": false,
103 | "input": [
104 | "? datawriter"
105 | ],
106 | "language": "python",
107 | "metadata": {},
108 | "outputs": [],
109 | "prompt_number": 9
110 | },
111 | {
112 | "cell_type": "code",
113 | "collapsed": false,
114 | "input": [],
115 | "language": "python",
116 | "metadata": {},
117 | "outputs": []
118 | }
119 | ],
120 | "metadata": {}
121 | }
122 | ]
123 | }
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70 | 0.03000,-0.02900
71 | 0.04000,-0.03220
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73 | 0.06000,-0.03680
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75 | 0.10000,-0.04620
76 | 0.12000,-0.05030
77 | 0.14000,-0.05370
78 | 0.16000,-0.05670
79 | 0.18000,-0.05920
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81 | 0.22000,-0.06270
82 | 0.24000,-0.06410
83 | 0.26000,-0.06590
84 | 0.28000,-0.06790
85 | 0.30000,-0.06890
86 | 0.32000,-0.06900
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88 | 0.36000,-0.06710
89 | 0.38000,-0.06550
90 | 0.40000,-0.06360
91 | 0.42000,-0.06150
92 | 0.44000,-0.05950
93 | 0.46000,-0.05740
94 | 0.48000,-0.05530
95 | 0.50000,-0.05330
96 | 0.52000,-0.05120
97 | 0.54000,-0.04920
98 | 0.56000,-0.04720
99 | 0.58000,-0.04520
100 | 0.60000,-0.04310
101 | 0.62000,-0.04090
102 | 0.64000,-0.03880
103 | 0.66000,-0.03660
104 | 0.68000,-0.03430
105 | 0.70000,-0.03210
106 | 0.72000,-0.02990
107 | 0.74000,-0.02760
108 | 0.76000,-0.02540
109 | 0.78000,-0.02330
110 | 0.80000,-0.02120
111 | 0.82000,-0.01910
112 | 0.84000,-0.01710
113 | 0.86000,-0.01510
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1 | Airfoil A
2 |
3 | 1.00000,0.00000
4 | 0.99000,0.00123
5 | 0.98000,0.00245
6 | 0.97000,0.00367
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22 | 0.66000,0.02620
23 | 0.64000,0.02740
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26 | 0.58000,0.03070
27 | 0.56000,0.03180
28 | 0.54000,0.03280
29 | 0.52000,0.03400
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31 | 0.48000,0.03670
32 | 0.46000,0.03810
33 | 0.44000,0.03950
34 | 0.42000,0.04070
35 | 0.40000,0.04160
36 | 0.38000,0.04210
37 | 0.36000,0.04230
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39 | 0.32000,0.04300
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41 | 0.28000,0.04570
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43 | 0.24000,0.05020
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48 | 0.14000,0.05010
49 | 0.12000,0.04910
50 | 0.10000,0.04770
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52 | 0.06000,0.04140
53 | 0.05000,0.03880
54 | 0.04000,0.03610
55 | 0.03000,0.03270
56 | 0.02000,0.02720
57 | 0.01200,0.02100
58 | 0.00800,0.01750
59 | 0.00400,0.01400
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1 | 0.0000000 0.0000000
2 | 0.0005000 0.0064638
3 | 0.0010000 0.0084488
4 | 0.0020000 0.0110085
5 | 0.0040000 0.0140317
6 | 0.0080000 0.0175265
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9 | 0.0300000 0.0326742
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11 | 0.0500000 0.0387719
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13 | 0.0800000 0.0454360
14 | 0.1000000 0.0476525
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16 | 0.1400000 0.0500832
17 | 0.1600000 0.0504598
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19 | 0.2000000 0.0505076
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22 | 0.2600000 0.0482429
23 | 0.2800000 0.0456843
24 | 0.3000000 0.0439763
25 | 0.3200000 0.0430062
26 | 0.3400000 0.0425267
27 | 0.3600000 0.0422943
28 | 0.3800000 0.0420659
29 | 0.4000000 0.0416033
30 | 0.4200000 0.0407363
31 | 0.4400000 0.0395394
32 | 0.4600000 0.0381409
33 | 0.4800000 0.0366673
34 | 0.5000000 0.0352476
35 | 0.5200000 0.0339760
36 | 0.5400000 0.0328278
37 | 0.5600000 0.0317559
38 | 0.5800000 0.0307107
39 | 0.6000000 0.0296456
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41 | 0.6400000 0.0273739
42 | 0.6600000 0.0262196
43 | 0.6800000 0.0250949
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46 | 0.7400000 0.0221102
47 | 0.7600000 0.0211718
48 | 0.7800000 0.0201870
49 | 0.8000000 0.0191108
50 | 0.8200000 0.0179036
51 | 0.8400000 0.0165478
52 | 0.8600000 0.0150329
53 | 0.8800000 0.0133449
54 | 0.9000000 0.0114733
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56 | 0.9400000 0.0071976
57 | 0.9600000 0.0048649
58 | 0.9700000 0.0036652
59 | 0.9800000 0.0024506
60 | 0.9900000 0.0012275
61 | 1.0000000 0.0000000
62 |
63 | 0.0000000 0.0000000
64 | 0.0005000 -.0046938
65 | 0.0010000 -.0068122
66 | 0.0020000 -.0095513
67 | 0.0040000 -.0128330
68 | 0.0080000 -.0162748
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120 | 0.9700000 -.0033653
121 | 0.9800000 -.0022462
122 | 0.9900000 -.0011243
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1 |
2 | 0.000000 0.000000
3 | 0.004712 0.012211
4 | 0.007052 0.014766
5 | 0.012157 0.018787
6 | 0.024309 0.029274
7 | 0.049040 0.040657
8 | 0.073920 0.045745
9 | 0.098786 0.051431
10 | 0.148638 0.057708
11 | 0.198551 0.061386
12 | 0.248554 0.061266
13 | 0.298540 0.061846
14 | 0.398560 0.061006
15 | 0.498566 0.060766
16 | 0.598899 0.046634
17 | 1.000000 0.000000
18 |
19 | 0.000000 0.000000
20 | 0.005209 -0.008877
21 | 0.007681 -0.011919
22 | 0.012940 -0.014395
23 | 0.025467 -0.019799
24 | 0.050649 -0.027505
25 | 0.075755 -0.032012
26 | 0.100876 -0.037119
27 | 0.151044 -0.044235
28 | 0.201198 -0.050752
29 | 0.251319 -0.055869
30 | 0.301411 -0.059787
31 | 0.401417 -0.060027
32 | 0.501361 -0.057668
33 | 0.601185 -0.050212
34 | 1.000000 0.000000
35 |
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1 |
2 | 0.0000 0.0000
3 | 0.0050 0.0149
4 | 0.0083 0.0165
5 | 0.0125 0.0206
6 | 0.0249 0.0256
7 | 0.0500 0.0330
8 | 0.0748 0.0396
9 | 0.1000 0.0446
10 | 0.1500 0.0545
11 | 0.2000 0.0578
12 | 0.2500 0.0628
13 | 0.3000 0.0661
14 | 0.4000 0.0661
15 | 0.5000 0.0611
16 | 0.6000 0.0512
17 | 0.7000 0.0413
18 | 1.0000 0.0000
19 |
20 | 0.0000 0.0000
21 | 0.0050 -0.0066
22 | 0.0083 -0.0074
23 | 0.0125 -0.0083
24 | 0.0249 -0.0091
25 | 0.0500 -0.0099
26 | 0.0748 -0.0124
27 | 0.1000 -0.0132
28 | 0.1500 -0.0165
29 | 0.2000 -0.0215
30 | 0.2500 -0.0248
31 | 0.3000 -0.0297
32 | 0.4000 -0.0297
33 | 0.5000 -0.0289
34 | 0.6000 -0.0264
35 | 0.7000 -0.0198
36 | 1.0000 0.0000
37 |
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1 |
2 | 0.0000 0.0030
3 | 0.0050 0.0099
4 | 0.0074 0.0120
5 | 0.0126 0.0147
6 | 0.0250 0.0215
7 | 0.0500 0.0303
8 | 0.0753 0.0385
9 | 0.1000 0.0442
10 | 0.1500 0.0520
11 | 0.2000 0.0570
12 | 0.2500 0.0604
13 | 0.3000 0.0627
14 | 0.4000 0.0644
15 | 0.5000 0.0618
16 | 0.6000 0.0541
17 | 0.7000 0.0427
18 | 0.8000 0.0290
19 | 0.9000 0.0145
20 | 1.0000 0.0000
21 |
22 | 0.0000 0.0030
23 | 0.0050 -0.0046
24 | 0.0074 -0.0055
25 | 0.0126 -0.0065
26 | 0.0250 -0.0074
27 | 0.0500 -0.0090
28 | 0.0753 -0.0105
29 | 0.1000 -0.0118
30 | 0.1500 -0.0149
31 | 0.2000 -0.0177
32 | 0.2500 -0.0206
33 | 0.3000 -0.0227
34 | 0.4000 -0.0253
35 | 0.5000 -0.0250
36 | 0.6000 -0.0208
37 | 0.7000 -0.0156
38 | 0.8000 -0.0105
39 | 0.9000 -0.0051
40 | 1.0000 0.0000
41 |
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1 |
2 | 0.0000000 0.0000000
3 | 0.0005000 0.0017762
4 | 0.0010000 0.0026712
5 | 0.0020000 0.0039826
6 | 0.0040000 0.0059651
7 | 0.0080000 0.0093775
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13 | 0.0600000 0.0316763
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1 | {
2 | "metadata": {
3 | "name": "",
4 | "signature": "sha256:52576baa4c4fefe0c4446ea647b6975b869a8fc5e8b55c781d4efa484abca016"
5 | },
6 | "nbformat": 3,
7 | "nbformat_minor": 0,
8 | "worksheets": [
9 | {
10 | "cells": [
11 | {
12 | "cell_type": "code",
13 | "collapsed": false,
14 | "input": [
15 | "import math\n",
16 | "import numpy\n",
17 | "import sympy\n",
18 | "from matplotlib import pyplot\n",
19 | "% matplotlib inline\n",
20 | "import csv"
21 | ],
22 | "language": "python",
23 | "metadata": {},
24 | "outputs": [],
25 | "prompt_number": 1
26 | },
27 | {
28 | "cell_type": "code",
29 | "collapsed": false,
30 | "input": [
31 | "# This cell imports and plots the five airfoil variants of the Boeing 707.\n",
32 | "#####import the first airfoil 707a#####\n",
33 | "file_name = './b707a.txt' \n",
34 | "x,y = numpy.loadtxt(file_name,dtype=float,unpack=True )\n",
35 | "#Rearrange data into format that is expected from Barba's team code\n",
36 | "L = len(x);\n",
37 | "xpart1 = x[0:L/2];\n",
38 | "xpart2 = xpart1[::-1]\n",
39 | "xcont = numpy.linspace(0,L,L)\n",
40 | "xcont[:L/2]=xpart2;\n",
41 | "xcont[L/2:]=x[L/2:]\n",
42 | "x[0:L] = xcont[0:L]\n",
43 | "ypart1 = y[0:L/2];\n",
44 | "ypart2 = ypart1[::-1]\n",
45 | "ycont = numpy.linspace(0,L,L)\n",
46 | "ycont[:L/2]=ypart2;\n",
47 | "ycont[L/2:]=y[L/2:]\n",
48 | "y[0:L] = ycont[0:L]"
49 | ],
50 | "language": "python",
51 | "metadata": {},
52 | "outputs": [],
53 | "prompt_number": 2
54 | },
55 | {
56 | "cell_type": "code",
57 | "collapsed": false,
58 | "input": [
59 | "numpy.savetxt('./xdataA.txt',x,delimiter =',')\n",
60 | "numpy.savetxt('./ydataA.txt',y,delimiter =',')"
61 | ],
62 | "language": "python",
63 | "metadata": {},
64 | "outputs": [],
65 | "prompt_number": 3
66 | },
67 | {
68 | "cell_type": "code",
69 | "collapsed": false,
70 | "input": [],
71 | "language": "python",
72 | "metadata": {},
73 | "outputs": []
74 | }
75 | ],
76 | "metadata": {}
77 | }
78 | ]
79 | }
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1 | 0.0000000 0.0000000
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124 |
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/Bornemeier/resources/b707b.txt:
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1 |
2 | 0.000000 0.000000
3 | 0.004712 0.012211
4 | 0.007052 0.014766
5 | 0.012157 0.018787
6 | 0.024309 0.029274
7 | 0.049040 0.040657
8 | 0.073920 0.045745
9 | 0.098786 0.051431
10 | 0.148638 0.057708
11 | 0.198551 0.061386
12 | 0.248554 0.061266
13 | 0.298540 0.061846
14 | 0.398560 0.061006
15 | 0.498566 0.060766
16 | 0.598899 0.046634
17 | 1.000000 0.000000
18 |
19 | 0.000000 0.000000
20 | 0.005209 -0.008877
21 | 0.007681 -0.011919
22 | 0.012940 -0.014395
23 | 0.025467 -0.019799
24 | 0.050649 -0.027505
25 | 0.075755 -0.032012
26 | 0.100876 -0.037119
27 | 0.151044 -0.044235
28 | 0.201198 -0.050752
29 | 0.251319 -0.055869
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31 | 0.401417 -0.060027
32 | 0.501361 -0.057668
33 | 0.601185 -0.050212
34 | 1.000000 0.000000
35 |
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/Bornemeier/resources/b707c.txt:
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1 | BOEING 707 .40 SPAN AIRFOIL
2 | 17.0 17.0
3 |
4 | 0.0000 0.0000
5 | 0.0050 0.0149
6 | 0.0083 0.0165
7 | 0.0125 0.0206
8 | 0.0249 0.0256
9 | 0.0500 0.0330
10 | 0.0748 0.0396
11 | 0.1000 0.0446
12 | 0.1500 0.0545
13 | 0.2000 0.0578
14 | 0.2500 0.0628
15 | 0.3000 0.0661
16 | 0.4000 0.0661
17 | 0.5000 0.0611
18 | 0.6000 0.0512
19 | 0.7000 0.0413
20 | 1.0000 0.0000
21 |
22 | 0.0000 0.0000
23 | 0.0050 -0.0066
24 | 0.0083 -0.0074
25 | 0.0125 -0.0083
26 | 0.0249 -0.0091
27 | 0.0500 -0.0099
28 | 0.0748 -0.0124
29 | 0.1000 -0.0132
30 | 0.1500 -0.0165
31 | 0.2000 -0.0215
32 | 0.2500 -0.0248
33 | 0.3000 -0.0297
34 | 0.4000 -0.0297
35 | 0.5000 -0.0289
36 | 0.6000 -0.0264
37 | 0.7000 -0.0198
38 | 1.0000 0.0000
39 |
--------------------------------------------------------------------------------
/Bornemeier/resources/b707d.txt:
--------------------------------------------------------------------------------
1 | BOEING 707 .54 SPAN AIRFOIL
2 | 19.0 19.0
3 |
4 | 0.0000 0.0030
5 | 0.0050 0.0099
6 | 0.0074 0.0120
7 | 0.0126 0.0147
8 | 0.0250 0.0215
9 | 0.0500 0.0303
10 | 0.0753 0.0385
11 | 0.1000 0.0442
12 | 0.1500 0.0520
13 | 0.2000 0.0570
14 | 0.2500 0.0604
15 | 0.3000 0.0627
16 | 0.4000 0.0644
17 | 0.5000 0.0618
18 | 0.6000 0.0541
19 | 0.7000 0.0427
20 | 0.8000 0.0290
21 | 0.9000 0.0145
22 | 1.0000 0.0000
23 |
24 | 0.0000 0.0030
25 | 0.0050 -0.0046
26 | 0.0074 -0.0055
27 | 0.0126 -0.0065
28 | 0.0250 -0.0074
29 | 0.0500 -0.0090
30 | 0.0753 -0.0105
31 | 0.1000 -0.0118
32 | 0.1500 -0.0149
33 | 0.2000 -0.0177
34 | 0.2500 -0.0206
35 | 0.3000 -0.0227
36 | 0.4000 -0.0253
37 | 0.5000 -0.0250
38 | 0.6000 -0.0208
39 | 0.7000 -0.0156
40 | 0.8000 -0.0105
41 | 0.9000 -0.0051
42 | 1.0000 0.0000
43 |
--------------------------------------------------------------------------------
/Bornemeier/resources/b707e.txt:
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1 | BOEING 707 .99 SPAN AIRFOIL
2 | 61. 61.
3 |
4 | 0.0000000 0.0000000
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6 | 0.0010000 0.0026712
7 | 0.0020000 0.0039826
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27 | 0.3000000 0.0606677
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65 |
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126 | 1.0000000 0.0000000
127 |
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62 |
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123 | 1.0000000 0.0000000
124 |
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/Bornemeier/resources/others/b707b.dat:
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1 | BOEING 707 .19 SPAN AIRFOIL
2 | 16.0 16.0
3 |
4 | 0.000000 0.000000
5 | 0.004712 0.012211
6 | 0.007052 0.014766
7 | 0.012157 0.018787
8 | 0.024309 0.029274
9 | 0.049040 0.040657
10 | 0.073920 0.045745
11 | 0.098786 0.051431
12 | 0.148638 0.057708
13 | 0.198551 0.061386
14 | 0.248554 0.061266
15 | 0.298540 0.061846
16 | 0.398560 0.061006
17 | 0.498566 0.060766
18 | 0.598899 0.046634
19 | 1.000000 0.000000
20 |
21 | 0.000000 0.000000
22 | 0.005209 -0.008877
23 | 0.007681 -0.011919
24 | 0.012940 -0.014395
25 | 0.025467 -0.019799
26 | 0.050649 -0.027505
27 | 0.075755 -0.032012
28 | 0.100876 -0.037119
29 | 0.151044 -0.044235
30 | 0.201198 -0.050752
31 | 0.251319 -0.055869
32 | 0.301411 -0.059787
33 | 0.401417 -0.060027
34 | 0.501361 -0.057668
35 | 0.601185 -0.050212
36 | 1.000000 0.000000
37 |
--------------------------------------------------------------------------------
/Bornemeier/resources/others/b707c.dat:
--------------------------------------------------------------------------------
1 | BOEING 707 .40 SPAN AIRFOIL
2 | 17.0 17.0
3 |
4 | 0.0000 0.0000
5 | 0.0050 0.0149
6 | 0.0083 0.0165
7 | 0.0125 0.0206
8 | 0.0249 0.0256
9 | 0.0500 0.0330
10 | 0.0748 0.0396
11 | 0.1000 0.0446
12 | 0.1500 0.0545
13 | 0.2000 0.0578
14 | 0.2500 0.0628
15 | 0.3000 0.0661
16 | 0.4000 0.0661
17 | 0.5000 0.0611
18 | 0.6000 0.0512
19 | 0.7000 0.0413
20 | 1.0000 0.0000
21 |
22 | 0.0000 0.0000
23 | 0.0050 -0.0066
24 | 0.0083 -0.0074
25 | 0.0125 -0.0083
26 | 0.0249 -0.0091
27 | 0.0500 -0.0099
28 | 0.0748 -0.0124
29 | 0.1000 -0.0132
30 | 0.1500 -0.0165
31 | 0.2000 -0.0215
32 | 0.2500 -0.0248
33 | 0.3000 -0.0297
34 | 0.4000 -0.0297
35 | 0.5000 -0.0289
36 | 0.6000 -0.0264
37 | 0.7000 -0.0198
38 | 1.0000 0.0000
39 |
--------------------------------------------------------------------------------
/Bornemeier/resources/others/b707d.dat:
--------------------------------------------------------------------------------
1 | BOEING 707 .54 SPAN AIRFOIL
2 | 19.0 19.0
3 |
4 | 0.0000 0.0030
5 | 0.0050 0.0099
6 | 0.0074 0.0120
7 | 0.0126 0.0147
8 | 0.0250 0.0215
9 | 0.0500 0.0303
10 | 0.0753 0.0385
11 | 0.1000 0.0442
12 | 0.1500 0.0520
13 | 0.2000 0.0570
14 | 0.2500 0.0604
15 | 0.3000 0.0627
16 | 0.4000 0.0644
17 | 0.5000 0.0618
18 | 0.6000 0.0541
19 | 0.7000 0.0427
20 | 0.8000 0.0290
21 | 0.9000 0.0145
22 | 1.0000 0.0000
23 |
24 | 0.0000 0.0030
25 | 0.0050 -0.0046
26 | 0.0074 -0.0055
27 | 0.0126 -0.0065
28 | 0.0250 -0.0074
29 | 0.0500 -0.0090
30 | 0.0753 -0.0105
31 | 0.1000 -0.0118
32 | 0.1500 -0.0149
33 | 0.2000 -0.0177
34 | 0.2500 -0.0206
35 | 0.3000 -0.0227
36 | 0.4000 -0.0253
37 | 0.5000 -0.0250
38 | 0.6000 -0.0208
39 | 0.7000 -0.0156
40 | 0.8000 -0.0105
41 | 0.9000 -0.0051
42 | 1.0000 0.0000
43 |
--------------------------------------------------------------------------------
/Bornemeier/resources/others/b707e.dat:
--------------------------------------------------------------------------------
1 | BOEING 707 .99 SPAN AIRFOIL
2 | 61. 61.
3 |
4 | 0.0000000 0.0000000
5 | 0.0005000 0.0017762
6 | 0.0010000 0.0026712
7 | 0.0020000 0.0039826
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16 | 0.0800000 0.0368998
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23 | 0.2200000 0.0560793
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27 | 0.3000000 0.0606677
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29 | 0.3400000 0.0619894
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31 | 0.3800000 0.0626003
32 | 0.4000000 0.0626795
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36 | 0.4800000 0.0614093
37 | 0.5000000 0.0605710
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/Project - Michael J Carter/styles/custom.css:
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/README.md:
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1 | # AeroPython student projects, Spring 2015
2 |
3 | Students were requested to fork this repository, add their project as an IPython Notebook
4 | (with any dependencies, like figures, data or style sheets), and submit a pull request.
5 | The instructor will provide feedback as comments on the pull request, and merge the pull request
6 | when the project is good!
7 |
8 |
9 | **Please add all your files in one folder, named with your GitHub handle or last name.** And *please* do not include the notebook checkpoints in your commits (add the checkpoints folder to the ignore list).
10 |
11 | ## Index of merged student projects
12 |
13 | 1. [Vortex lattice method](http://nbviewer.ipython.org/github/barbagroup/AeroPython-studentprojects/blob/master/Bell_Christopher/VLM.ipynb), by Christopher Bell
14 | 2. [The effect of flap deflection wit a Junkers flap](http://nbviewer.ipython.org/github/barbagroup/AeroPython-studentprojects/blob/master/cparvini/FlapNotebook.ipynb), by Cameron Parvini
15 | 3. [Case study of Wing in Ground Effect with XFLR5: the A-90 Orlyonok (Орлёнок) Ekranoplan](http://nbviewer.ipython.org/github/barbagroup/AeroPython-studentprojects/blob/master/GeorgeTeel/Orlyonok%20Ekranoplan.ipynb), by George Teel
16 | 4. [The evolution of Boeing's 707 airliner: panel method applied to a family of B707 airfoils](http://nbviewer.ipython.org/github/barbagroup/AeroPython-studentprojects/blob/master/Bornemeier/Final%20Project.ipynb), by Matt Bornemeier
17 | 5. [Ground Effect with a Vortex Panel Method](http://nbviewer.ipython.org/github/barbagroup/AeroPython-studentprojects/blob/master/Ground-Effect-in-Vortex-Panel-Method/Ground-Effect-in-Vortex-Panel-Method.ipynb), by Tingyu Wang
18 | 6. [Further Study of Constant-Strength-Singularity Panel Methods](http://nbviewer.ipython.org/github/barbagroup/AeroPython-studentprojects/blob/master/Project%20-%20Michael%20J%20Carter/Project%20-%20Michael%20J%20Carter.ipynb), by Michael J. Carter
19 |
20 | ### Spring 2014
21 |
22 | * [Limitations of Inviscid Panel Method](http://nbviewer.ipython.org/github/LTChaseJohnson/MAE6226/blob/master/final%20project.ipynb), Chase Johnson
23 | * [Pterosaur wings: effect of the wing-tip twist on center-of-pressure location](http://nbviewer.ipython.org/github/colinparker/Pterosaur/blob/master/parker_pterosaur.ipynb) (following Palmer & Dyke, 2012; using XFLR)
24 | * [Boundary Layer Correction in Panel Methods](http://nbviewer.ipython.org/github/iancarr/AeroHydro/blob/master/final-project/BoundaryLayerCorrection.ipynb), Ian Carr.
25 | * [Stokes Flow with a Boundary Element Method](http://nbviewer.ipython.org/github/arm6226/mae6226/blob/master/project/MAE6226%20Project.ipynb), Abhilash Malipeddi
26 |
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