├── .github └── ISSUE_TEMPLATE │ └── codeheat-issue-template.md ├── LICENSE ├── MBDynOutputs ├── 19.log ├── 19.mov ├── 23.log ├── 23.mov ├── 26.log ├── 26.mov └── README.md ├── NetCDF ├── README.md ├── rotor.cc.patch └── rotor.h.patch ├── README.md ├── airfoilData ├── README.md ├── airfoil.mbd ├── cactusImport │ ├── LICENSE.TXT │ ├── NACA_0015.dat │ ├── NACA_0018.dat │ └── NACA_0021.dat ├── naca0012_free_format.c81 ├── sandiaImport │ ├── NACA_0012_Re1e6.dat │ └── NACA_0012_Re1e7.dat └── testNACA.blend └── manualImages ├── README.md ├── cardano.256.png ├── inline.256.png ├── input.pdf ├── revHinge.256.png ├── revolute.blend ├── revolute.txt └── spherHinge.256.png /.github/ISSUE_TEMPLATE/codeheat-issue-template.md: -------------------------------------------------------------------------------- 1 | --- 2 | name: Codeheat issue template 3 | about: Starter Issue 4 | title: '' 5 | labels: codeheat, starter 6 | assignees: '' 7 | 8 | --- 9 | 10 | This issue can be taken by multiple CodeHeat participants. 11 | 12 | ### OBJECTIVE 13 | An initial sentence or two that describes what the task entails and why someone would want to spend their time on it. 14 | 15 | ### REQUIREMENTS 16 | Several sentences/bullets that provide more detail into the task: What approach should people use? What level of detail are you looking for? How people should submit their work? Please keep CodeHeat registration as the first requirement. 17 | - Register as a CodeHeat participant if you haven't already done so https://codeheat.org/register 18 | 19 | ### EXPECTED OUTCOME 20 | What the expected deliverable is (a tutorial reviewed by at least one member of the documentation team and posted to the handbook, a patch in the core issue queue marked ready to be committed...). Please be specific as possible here. If people should create a patch, specify the branch against which the patch should be rolled. If a handbook page should be created, it's great to specify what you think the parent should be. 21 | 22 | ### HOW TO SUBMIT YOUR WORK 23 | 24 | ### QUESTIONS 25 | - If you have any questions, please comment on this issue directly, or reach out to us at https://gitter.im/fossasia/fossasia 26 | - If you identify any problem while working on this issue, take up [a related task](https://github.com/fossasia/Codeheat/issues/13) to file a bug report 27 | -------------------------------------------------------------------------------- /LICENSE: -------------------------------------------------------------------------------- 1 | GNU GENERAL PUBLIC LICENSE 2 | Version 2, June 1991 3 | 4 | Copyright (C) 1989, 1991 Free Software Foundation, Inc., 5 | 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301 USA 6 | Everyone is permitted to copy and distribute verbatim copies 7 | of this license document, but changing it is not allowed. 8 | 9 | Preamble 10 | 11 | The licenses for most software are designed to take away your 12 | freedom to share and change it. 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Of course, the commands you use may 322 | be called something other than `show w' and `show c'; they could even be 323 | mouse-clicks or menu items--whatever suits your program. 324 | 325 | You should also get your employer (if you work as a programmer) or your 326 | school, if any, to sign a "copyright disclaimer" for the program, if 327 | necessary. Here is a sample; alter the names: 328 | 329 | Yoyodyne, Inc., hereby disclaims all copyright interest in the program 330 | `Gnomovision' (which makes passes at compilers) written by James Hacker. 331 | 332 | {signature of Ty Coon}, 1 April 1989 333 | Ty Coon, President of Vice 334 | 335 | This General Public License does not permit incorporating your program into 336 | proprietary programs. If your program is a subroutine library, you may 337 | consider it more useful to permit linking proprietary applications with the 338 | library. If this is what you want to do, use the GNU Lesser General 339 | Public License instead of this License. 340 | -------------------------------------------------------------------------------- /MBDynOutputs/19.log: -------------------------------------------------------------------------------- 1 | output frequency: 1 2 | structural node: 1 0 0 0 euler123 -0 0 0 3 | structural node: 2 0.1 0 0 euler123 -0 0 0 4 | structural node: 3 0.398431 0.025 0 euler123 -0 0 7.18076 5 | structural node: 4 0.596863 0.05 0 euler123 -0 0 0 6 | body: 1 2 1 0 0 0 1 0 0 0 1 0 0 0 0.00333333 7 | body: 2 3 1 0 0 0 1 0 0 0 1 0 0 0 0.0133333 8 | body: 3 4 1 0 0 0 1 0 0 0 1 0 0 0 1 9 | clamp: 1 1 0 0 0 1 0 0 0 1 0 0 0 1 1 0 0 0 1 0 0 0 1 0 0 0 1 10 | axialrotation: 2 1 0 0 0 1 0 0 0 1 0 0 0 1 2 -0.1 0 0 1 0 0 0 1 0 0 0 1 11 | revolutehinge: 3 2 0.1 0 0 0.992157 -0.125 0 0.125 0.992157 0 0 0 1 3 -0.2 0 0 1 0 0 0 1 0 0 0 1 12 | inline: 4 3 0.2 0 0 1 0 0 0 1 0 0 0 1 4 0 0 0 1 0 0 0 1 0 0 0 1 13 | inline: 5 1 0 0.05 0 0 -0 1 0 1 0 -1 0 0 4 0 0 0 1 0 0 0 1 0 0 0 1 14 | prismatic: 6 1 0 0 0 1 0 0 0 1 0 0 0 1 4 0 0 0 1 0 0 0 1 0 0 0 1 15 | structural absolute force: 1 4 0 0 0 16 | struct node dofs: 0 6 18 30 17 | struct node eqs: 0 12 24 36 18 | struct node momentum dofs: 12 24 36 19 | struct node momentum eqs: 6 18 30 20 | struct displacement node dofs: 0 6 18 30 21 | struct displacement node eqs: 0 12 24 36 22 | struct displacement node momentum dofs: 12 24 36 23 | struct displacement node momentum eqs: 6 18 30 24 | struct node labels: 1 2 3 4 25 | struct displacement node labels: 1 2 3 4 26 | Symbol table: 27 | integer Body_Conrod = 2 28 | integer Body_Crank = 1 29 | integer Body_Slider = 3 30 | const bool FALSE = 0 31 | integer FoStr_Slider = 1 32 | const integer INT_MAX = 2147483647 33 | const integer INT_MIN = -2147483648 34 | real Izz_Conrod = 0.0133333 35 | real Izz_Crank = 0.00333333 36 | integer JoAxrot_Ground_Crank = 2 37 | integer JoClamp_Ground = 1 38 | integer JoInlin_Conrod_Slider = 4 39 | integer JoInlin_Ground_Slider = 5 40 | integer JoPrism_Ground_Slider = 6 41 | integer JoRevh_Crank_Conrod = 3 42 | real Length_Conrod = 0.4 43 | real Length_Crank = 0.2 44 | real Mass_Conrod = 1. 45 | real Mass_Crank = 1. 46 | real Mass_Slider = 1. 47 | integer Node_Conrod = 3 48 | integer Node_Crank = 2 49 | integer Node_Ground = 1 50 | integer Node_Slider = 4 51 | real Offset_Slider = 0.05 52 | const integer RAND_MAX = 2147483647 53 | const real REAL_MAX = 1.79769e+308 54 | const real REAL_MIN = 2.22507e-308 55 | integer Ref_Conrod = 1 56 | integer Step = 0 57 | const bool TRUE = 1 58 | real Time = 0. 59 | real TimeStep = 0. 60 | real Var = 0. 61 | const real deg2rad = 0.0174533 62 | const real e = 2.71828 63 | const real ft2m = 0.3048 64 | const real in2m = 0.0254 65 | const real in2mm = 25.4 66 | const real kg2lb = 2.20462 67 | const real kg2slug = 0.0685218 68 | const real lb2kg = 0.453592 69 | const real m2ft = 3.28084 70 | const real m2in = 39.3701 71 | const real mm2in = 0.0393701 72 | const real pi = 3.14159 73 | const real rad2deg = 57.2958 74 | const real slug2kg = 14.5939 75 | Environment: 76 | XDG_VTNR=7 77 | LC_PAPER=it_IT.UTF-8 78 | LC_ADDRESS=it_IT.UTF-8 79 | XDG_SESSION_ID=c2 80 | XDG_GREETER_DATA_DIR=/var/lib/lightdm-data/louis 81 | LC_MONETARY=it_IT.UTF-8 82 | CLUTTER_IM_MODULE=xim 83 | SESSION=ubuntu 84 | GPG_AGENT_INFO=/home/louis/.gnupg/S.gpg-agent:0:1 85 | TERM=xterm-256color 86 | VTE_VERSION=4205 87 | XDG_MENU_PREFIX=gnome- 88 | SHELL=/bin/bash 89 | OPENBLAS_NUM_THREADS=1 90 | QT_LINUX_ACCESSIBILITY_ALWAYS_ON=1 91 | WINDOWID=96469002 92 | LC_NUMERIC=it_IT.UTF-8 93 | UPSTART_SESSION=unix:abstract=/com/ubuntu/upstart-session/1000/1474 94 | GNOME_KEYRING_CONTROL= 95 | GTK_MODULES=gail:atk-bridge:unity-gtk-module 96 | USER=louis 97 | LD_LIBRARY_PATH=:/home/louis/bin/Dakota/bin:/home/louis/bin/Dakota/lib 98 | 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99 | QT_ACCESSIBILITY=1 100 | LC_TELEPHONE=it_IT.UTF-8 101 | XDG_SESSION_PATH=/org/freedesktop/DisplayManager/Session0 102 | XDG_SEAT_PATH=/org/freedesktop/DisplayManager/Seat0 103 | SSH_AUTH_SOCK=/run/user/1000/keyring/ssh 104 | SESSION_MANAGER=local/lati3:@/tmp/.ICE-unix/1855,unix/lati3:/tmp/.ICE-unix/1855 105 | DEFAULTS_PATH=/usr/share/gconf/ubuntu.default.path 106 | XDG_CONFIG_DIRS=/etc/xdg/xdg-ubuntu:/usr/share/upstart/xdg:/etc/xdg 107 | DESKTOP_SESSION=ubuntu 108 | PATH=/home/louis/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/louis/bin/Dakota/bin 109 | QT_IM_MODULE=ibus 110 | QT_QPA_PLATFORMTHEME=appmenu-qt5 111 | LC_IDENTIFICATION=it_IT.UTF-8 112 | XDG_SESSION_TYPE=x11 113 | PWD=/home/louis/b12/media/louis/SSD5/PIF2015/GSoC/Gci2016/mbdyn-gci/MBDynOutputs 114 | JOB=unity-settings-daemon 115 | XMODIFIERS=@im=ibus 116 | GNOME_KEYRING_PID= 117 | LANG=en_US.UTF-8 118 | GDM_LANG=en_US 119 | MANDATORY_PATH=/usr/share/gconf/ubuntu.mandatory.path 120 | LC_MEASUREMENT=it_IT.UTF-8 121 | COMPIZ_CONFIG_PROFILE=ubuntu 122 | IM_CONFIG_PHASE=1 123 | GDMSESSION=ubuntu 124 | SESSIONTYPE=gnome-session 125 | GTK2_MODULES=overlay-scrollbar 126 | SHLVL=1 127 | HOME=/home/louis 128 | XDG_SEAT=seat0 129 | LANGUAGE=en_US 130 | GNOME_DESKTOP_SESSION_ID=this-is-deprecated 131 | UPSTART_INSTANCE= 132 | UPSTART_EVENTS=xsession started 133 | XDG_SESSION_DESKTOP=ubuntu 134 | LOGNAME=louis 135 | COMPIZ_BIN_PATH=/usr/bin/ 136 | DBUS_SESSION_BUS_ADDRESS=unix:abstract=/tmp/dbus-l8xoaz3mxy 137 | XDG_DATA_DIRS=/usr/share/ubuntu:/usr/share/gnome:/usr/local/share:/usr/share:/var/lib/snapd/desktop:/var/lib/snapd/desktop 138 | QT4_IM_MODULE=xim 139 | LESSOPEN=| /usr/bin/lesspipe %s 140 | INSTANCE= 141 | UPSTART_JOB=unity7 142 | XDG_RUNTIME_DIR=/run/user/1000 143 | DISPLAY=:0 144 | XDG_CURRENT_DESKTOP=Unity 145 | GTK_IM_MODULE=ibus 146 | LESSCLOSE=/usr/bin/lesspipe %s %s 147 | LC_TIME=it_IT.UTF-8 148 | LC_NAME=it_IT.UTF-8 149 | XAUTHORITY=/home/louis/.Xauthority 150 | OLDPWD=/home/louis/b12/media/louis/SSD5/PIF2015/GSoC/Gci2016/mbdyn-gci 151 | _=/home/louis/bin/mbdyn-1.7.3/bin/mbdyn 152 | -------------------------------------------------------------------------------- /MBDynOutputs/23.log: -------------------------------------------------------------------------------- 1 | output frequency: 10 2 | structural node: 1 0 0 0 euler123 -0 0 0 3 | structural node: 2 0 0 -1 euler123 -0 0 0 4 | body: 1 2 1 0 0 0 1 0 0 0 1 0 0 0 1 5 | clamp: 1 1 0 0 0 1 0 0 0 1 0 0 0 1 1 0 0 0 1 0 0 0 1 0 0 0 1 6 | inline: 2 1 0 0 0 1 0 0 0 1 0 0 0 1 2 0 0 0 1 0 0 0 1 0 0 0 1 7 | prismatic: 3 1 0 0 0 1 0 0 0 1 0 0 0 1 2 0 0 0 1 0 0 0 1 0 0 0 1 8 | deformabledisplacementjoint: 4 1 0 0 0 1 0 0 0 1 0 0 0 1 2 0 0 0 1 0 0 0 1 0 0 0 1 9 | struct node dofs: 0 6 10 | struct node eqs: 0 12 11 | struct node momentum dofs: 12 12 | struct node momentum eqs: 6 13 | struct displacement node dofs: 0 6 14 | struct displacement node eqs: 0 12 15 | struct displacement node momentum dofs: 12 16 | struct displacement node momentum eqs: 6 17 | struct node labels: 1 2 18 | struct displacement node labels: 1 2 19 | Symbol table: 20 | integer Body_Mass = 1 21 | real C = 1. 22 | const bool FALSE = 0 23 | const integer INT_MAX = 2147483647 24 | const integer INT_MIN = -2147483648 25 | integer JoClamp_Ground = 1 26 | integer JoDfmd_SpringDamper = 4 27 | integer JoInLin_Ground_Mass = 2 28 | integer JoPrism_Ground_Mass = 3 29 | real K = 20. 30 | real L = 1. 31 | real M = 1. 32 | integer Node_Ground = 1 33 | integer Node_Mass = 2 34 | const integer RAND_MAX = 2147483647 35 | const real REAL_MAX = 1.79769e+308 36 | const real REAL_MIN = 2.22507e-308 37 | integer Step = 0 38 | const bool TRUE = 1 39 | real Time = 0. 40 | real TimeStep = 0. 41 | real Var = 0. 42 | const real deg2rad = 0.0174533 43 | const real e = 2.71828 44 | const real ft2m = 0.3048 45 | const real in2m = 0.0254 46 | const real in2mm = 25.4 47 | const real kg2lb = 2.20462 48 | const real kg2slug = 0.0685218 49 | const real lb2kg = 0.453592 50 | const real m2ft = 3.28084 51 | const real m2in = 39.3701 52 | const real mm2in = 0.0393701 53 | const real pi = 3.14159 54 | const real rad2deg = 57.2958 55 | const real slug2kg = 14.5939 56 | Environment: 57 | XDG_VTNR=7 58 | LC_PAPER=it_IT.UTF-8 59 | LC_ADDRESS=it_IT.UTF-8 60 | XDG_SESSION_ID=c2 61 | XDG_GREETER_DATA_DIR=/var/lib/lightdm-data/louis 62 | LC_MONETARY=it_IT.UTF-8 63 | CLUTTER_IM_MODULE=xim 64 | SESSION=ubuntu 65 | GPG_AGENT_INFO=/home/louis/.gnupg/S.gpg-agent:0:1 66 | TERM=xterm-256color 67 | VTE_VERSION=4205 68 | XDG_MENU_PREFIX=gnome- 69 | SHELL=/bin/bash 70 | OPENBLAS_NUM_THREADS=1 71 | QT_LINUX_ACCESSIBILITY_ALWAYS_ON=1 72 | WINDOWID=96469002 73 | LC_NUMERIC=it_IT.UTF-8 74 | UPSTART_SESSION=unix:abstract=/com/ubuntu/upstart-session/1000/1474 75 | GNOME_KEYRING_CONTROL= 76 | GTK_MODULES=gail:atk-bridge:unity-gtk-module 77 | USER=louis 78 | LD_LIBRARY_PATH=:/home/louis/bin/Dakota/bin:/home/louis/bin/Dakota/lib 79 | LS_COLORS=rs=0:di=01;34:ln=01;36:mh=00:pi=40;33:so=01;35:do=01;35:bd=40;33;01:cd=40;33;01:or=40;31;01:mi=00:su=37;41:sg=30;43:ca=30;41:tw=30;42:ow=34;42:st=37;44:ex=01;32:*.tar=01;31:*.tgz=01;31:*.arc=01;31:*.arj=01;31:*.taz=01;31:*.lha=01;31:*.lz4=01;31:*.lzh=01;31:*.lzma=01;31:*.tlz=01;31:*.txz=01;31:*.tzo=01;31:*.t7z=01;31:*.zip=01;31:*.z=01;31:*.Z=01;31:*.dz=01;31:*.gz=01;31:*.lrz=01;31:*.lz=01;31:*.lzo=01;31:*.xz=01;31:*.bz2=01;31:*.bz=01;31:*.tbz=01;31:*.tbz2=01;31:*.tz=01;31:*.deb=01;31:*.rpm=01;31:*.jar=01;31:*.war=01;31:*.ear=01;31:*.sar=01;31:*.rar=01;31:*.alz=01;31:*.ace=01;31:*.zoo=01;31:*.cpio=01;31:*.7z=01;31:*.rz=01;31:*.cab=01;31:*.jpg=01;35:*.jpeg=01;35:*.gif=01;35:*.bmp=01;35:*.pbm=01;35:*.pgm=01;35:*.ppm=01;35:*.tga=01;35:*.xbm=01;35:*.xpm=01;35:*.tif=01;35:*.tiff=01;35:*.png=01;35:*.svg=01;35:*.svgz=01;35:*.mng=01;35:*.pcx=01;35:*.mov=01;35:*.mpg=01;35:*.mpeg=01;35:*.m2v=01;35:*.mkv=01;35:*.webm=01;35:*.ogm=01;35:*.mp4=01;35:*.m4v=01;35:*.mp4v=01;35:*.vob=01;35:*.qt=01;35:*.nuv=01;35:*.wmv=01;35:*.asf=01;35:*.rm=01;35:*.rmvb=01;35:*.flc=01;35:*.avi=01;35:*.fli=01;35:*.flv=01;35:*.gl=01;35:*.dl=01;35:*.xcf=01;35:*.xwd=01;35:*.yuv=01;35:*.cgm=01;35:*.emf=01;35:*.ogv=01;35:*.ogx=01;35:*.aac=00;36:*.au=00;36:*.flac=00;36:*.m4a=00;36:*.mid=00;36:*.midi=00;36:*.mka=00;36:*.mp3=00;36:*.mpc=00;36:*.ogg=00;36:*.ra=00;36:*.wav=00;36:*.oga=00;36:*.opus=00;36:*.spx=00;36:*.xspf=00;36: 80 | QT_ACCESSIBILITY=1 81 | LC_TELEPHONE=it_IT.UTF-8 82 | XDG_SESSION_PATH=/org/freedesktop/DisplayManager/Session0 83 | XDG_SEAT_PATH=/org/freedesktop/DisplayManager/Seat0 84 | SSH_AUTH_SOCK=/run/user/1000/keyring/ssh 85 | SESSION_MANAGER=local/lati3:@/tmp/.ICE-unix/1855,unix/lati3:/tmp/.ICE-unix/1855 86 | DEFAULTS_PATH=/usr/share/gconf/ubuntu.default.path 87 | XDG_CONFIG_DIRS=/etc/xdg/xdg-ubuntu:/usr/share/upstart/xdg:/etc/xdg 88 | DESKTOP_SESSION=ubuntu 89 | PATH=/home/louis/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/louis/bin/Dakota/bin 90 | QT_IM_MODULE=ibus 91 | QT_QPA_PLATFORMTHEME=appmenu-qt5 92 | LC_IDENTIFICATION=it_IT.UTF-8 93 | XDG_SESSION_TYPE=x11 94 | PWD=/home/louis/b12/media/louis/SSD5/PIF2015/GSoC/Gci2016/mbdyn-gci/MBDynOutputs 95 | JOB=unity-settings-daemon 96 | XMODIFIERS=@im=ibus 97 | GNOME_KEYRING_PID= 98 | LANG=en_US.UTF-8 99 | GDM_LANG=en_US 100 | MANDATORY_PATH=/usr/share/gconf/ubuntu.mandatory.path 101 | LC_MEASUREMENT=it_IT.UTF-8 102 | COMPIZ_CONFIG_PROFILE=ubuntu 103 | IM_CONFIG_PHASE=1 104 | GDMSESSION=ubuntu 105 | SESSIONTYPE=gnome-session 106 | GTK2_MODULES=overlay-scrollbar 107 | SHLVL=1 108 | HOME=/home/louis 109 | XDG_SEAT=seat0 110 | LANGUAGE=en_US 111 | GNOME_DESKTOP_SESSION_ID=this-is-deprecated 112 | UPSTART_INSTANCE= 113 | UPSTART_EVENTS=xsession started 114 | XDG_SESSION_DESKTOP=ubuntu 115 | LOGNAME=louis 116 | COMPIZ_BIN_PATH=/usr/bin/ 117 | DBUS_SESSION_BUS_ADDRESS=unix:abstract=/tmp/dbus-l8xoaz3mxy 118 | XDG_DATA_DIRS=/usr/share/ubuntu:/usr/share/gnome:/usr/local/share:/usr/share:/var/lib/snapd/desktop:/var/lib/snapd/desktop 119 | QT4_IM_MODULE=xim 120 | LESSOPEN=| /usr/bin/lesspipe %s 121 | INSTANCE= 122 | UPSTART_JOB=unity7 123 | XDG_RUNTIME_DIR=/run/user/1000 124 | DISPLAY=:0 125 | XDG_CURRENT_DESKTOP=Unity 126 | GTK_IM_MODULE=ibus 127 | LESSCLOSE=/usr/bin/lesspipe %s %s 128 | LC_TIME=it_IT.UTF-8 129 | LC_NAME=it_IT.UTF-8 130 | XAUTHORITY=/home/louis/.Xauthority 131 | OLDPWD=/home/louis/b12/media/louis/SSD5/PIF2015/GSoC/Gci2016/mbdyn-gci 132 | _=/home/louis/bin/mbdyn-1.7.3/bin/mbdyn 133 | -------------------------------------------------------------------------------- /MBDynOutputs/26.log: -------------------------------------------------------------------------------- 1 | output frequency: 10 2 | structural node: 1 0 0 0 euler123 -0 0 0 3 | structural node: 2 0 0 -1 euler123 -0 0 0 4 | structural node: 3 0 0 0 euler123 -0 0 0 5 | body: 1 2 1 0 0 0 1 0 0 0 1 0 0 0 1 6 | drivedisplacementpin: 1 1 0 0 0 0 0 0 7 | inline: 2 1 0 0 0 1 0 0 0 1 0 0 0 1 2 0 0 0 1 0 0 0 1 0 0 0 1 8 | prismatic: 3 1 0 0 0 1 0 0 0 1 0 0 0 1 2 0 0 0 1 0 0 0 1 0 0 0 1 9 | deformabledisplacementjoint: 4 1 0 0 0 1 0 0 0 1 0 0 0 1 2 0 0 0 1 0 0 0 1 0 0 0 1 10 | clamp: 5 3 0 0 0 1 0 0 0 1 0 0 0 1 3 0 0 0 1 0 0 0 1 0 0 0 1 11 | structural absolute force: 1 2 0 0 0 12 | struct node dofs: 0 12 24 13 | struct node eqs: 6 18 24 14 | struct node momentum dofs: 6 18 15 | struct node momentum eqs: 0 12 16 | struct displacement node dofs: 0 12 24 17 | struct displacement node eqs: 6 18 24 18 | struct displacement node momentum dofs: 6 18 19 | struct displacement node momentum eqs: 0 12 20 | struct node labels: 1 2 3 21 | struct displacement node labels: 1 2 3 22 | Symbol table: 23 | integer Body_Mass = 1 24 | real Cc = 10. 25 | const real DZ = -1.23927 26 | real Dc = 0.0001 27 | real Ec = 1.2 28 | const bool FALSE = 0 29 | integer FoStr_Contact_Mass = 1 30 | real H = -1.5 31 | const integer INT_MAX = 2147483647 32 | const integer INT_MIN = -2147483648 33 | integer JoClamp_Ground = 5 34 | integer JoDfmd_Spring = 4 35 | integer JoDrivp_Actuator = 1 36 | integer JoInlin_Actuator_Mass = 2 37 | integer JoPrism_Actuator_Mass = 3 38 | real K = 40. 39 | real Kc = 10000. 40 | real L = 1. 41 | real M = 1. 42 | integer Node_Actuator = 1 43 | integer Node_Ground = 3 44 | integer Node_Mass = 2 45 | const integer RAND_MAX = 2147483647 46 | const real REAL_MAX = 1.79769e+308 47 | const real REAL_MIN = 2.22507e-308 48 | integer Step = 0 49 | const bool TRUE = 1 50 | real Time = 0. 51 | real TimeStep = 0. 52 | const real VZ = 0. 53 | real Var = 0. 54 | const real deg2rad = 0.0174533 55 | const real e = 2.71828 56 | const real ft2m = 0.3048 57 | const real in2m = 0.0254 58 | const real in2mm = 25.4 59 | const real kg2lb = 2.20462 60 | const real kg2slug = 0.0685218 61 | const real lb2kg = 0.453592 62 | const real m2ft = 3.28084 63 | const real m2in = 39.3701 64 | const real mm2in = 0.0393701 65 | const real pi = 3.14159 66 | const real rad2deg = 57.2958 67 | const real slug2kg = 14.5939 68 | Environment: 69 | LC_PAPER=it_IT.UTF-8 70 | XDG_SESSION_ID=5 71 | LC_ADDRESS=it_IT.UTF-8 72 | LC_MONETARY=it_IT.UTF-8 73 | TERM=xterm-256color 74 | SHELL=/bin/bash 75 | XDG_SESSION_COOKIE=b04fcab5174057844d2afb5f00000009-1511339551.954970-510931847 76 | SSH_CLIENT=131.175.154.200 53210 22 77 | OPENBLAS_NUM_THREADS=1 78 | LC_NUMERIC=it_IT.UTF-8 79 | SSH_TTY=/dev/pts/17 80 | USER=louis 81 | LD_LIBRARY_PATH=:/home/louis/bin/dakota-6.5.0.Linux.x86_64/lib:/home/louis/bin/dakota-6.5.0.Linux.x86_64/bin 82 | LS_COLORS=rs=0:di=01;34:ln=01;36:mh=00:pi=40;33:so=01;35:do=01;35:bd=40;33;01:cd=40;33;01:or=40;31;01:su=37;41:sg=30;43:ca=30;41:tw=30;42:ow=34;42:st=37;44:ex=01;32:*.tar=01;31:*.tgz=01;31:*.arj=01;31:*.taz=01;31:*.lzh=01;31:*.lzma=01;31:*.tlz=01;31:*.txz=01;31:*.zip=01;31:*.z=01;31:*.Z=01;31:*.dz=01;31:*.gz=01;31:*.lz=01;31:*.xz=01;31:*.bz2=01;31:*.bz=01;31:*.tbz=01;31:*.tbz2=01;31:*.tz=01;31:*.deb=01;31:*.rpm=01;31:*.jar=01;31:*.war=01;31:*.ear=01;31:*.sar=01;31:*.rar=01;31:*.ace=01;31:*.zoo=01;31:*.cpio=01;31:*.7z=01;31:*.rz=01;31:*.jpg=01;35:*.jpeg=01;35:*.gif=01;35:*.bmp=01;35:*.pbm=01;35:*.pgm=01;35:*.ppm=01;35:*.tga=01;35:*.xbm=01;35:*.xpm=01;35:*.tif=01;35:*.tiff=01;35:*.png=01;35:*.svg=01;35:*.svgz=01;35:*.mng=01;35:*.pcx=01;35:*.mov=01;35:*.mpg=01;35:*.mpeg=01;35:*.m2v=01;35:*.mkv=01;35:*.webm=01;35:*.ogm=01;35:*.mp4=01;35:*.m4v=01;35:*.mp4v=01;35:*.vob=01;35:*.qt=01;35:*.nuv=01;35:*.wmv=01;35:*.asf=01;35:*.rm=01;35:*.rmvb=01;35:*.flc=01;35:*.avi=01;35:*.fli=01;35:*.flv=01;35:*.gl=01;35:*.dl=01;35:*.xcf=01;35:*.xwd=01;35:*.yuv=01;35:*.cgm=01;35:*.emf=01;35:*.axv=01;35:*.anx=01;35:*.ogv=01;35:*.ogx=01;35:*.aac=00;36:*.au=00;36:*.flac=00;36:*.mid=00;36:*.midi=00;36:*.mka=00;36:*.mp3=00;36:*.mpc=00;36:*.ogg=00;36:*.ra=00;36:*.wav=00;36:*.axa=00;36:*.oga=00;36:*.spx=00;36:*.xspf=00;36: 83 | LC_TELEPHONE=it_IT.UTF-8 84 | MAIL=/var/mail/louis 85 | PATH=/home/louis/bin:/home/louis/miniconda3/bin:/home/louis/bin/dakota-6.5.0.Linux.x86_64/bin:/home/louis/bin/dakota-6.5.0.Linux.x86_64/test:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games 86 | LC_MESSAGES=en_CA.UTF-8 87 | QT_QPA_PLATFORMTHEME=appmenu-qt5 88 | LC_COLLATE=en_CA.UTF-8 89 | LC_IDENTIFICATION=it_IT.UTF-8 90 | PWD=/home/louis/PIF/GSoC/Gci2016/mbdyn-gci/MBDynOutputs 91 | LANG=en_CA.UTF-8 92 | LC_MEASUREMENT=it_IT.UTF-8 93 | SHLVL=1 94 | HOME=/home/louis 95 | LANGUAGE=en_CA:en 96 | LOGNAME=louis 97 | LC_CTYPE=en_CA.UTF-8 98 | SSH_CONNECTION=131.175.154.200 53210 10.48.68.233 22 99 | LESSOPEN=| /usr/bin/lesspipe %s 100 | XDG_RUNTIME_DIR=/run/user/1000 101 | LESSCLOSE=/usr/bin/lesspipe %s %s 102 | LC_TIME=it_IT.UTF-8 103 | LC_NAME=it_IT.UTF-8 104 | OLDPWD=/home/louis/PIF/GSoC/Gci2016/mbdyn-gci 105 | _=/usr/bin/mbdyn 106 | -------------------------------------------------------------------------------- /MBDynOutputs/README.md: -------------------------------------------------------------------------------- 1 | # mbdyn-outputs 2 | 3 | The following files are node (.mov which is not a movie file) and .log outputs from MBDyn tutorial cases of http://www.sky-engin.jp/en/MBDynTutorial/ 4 | 5 | The numbers correspond to the tutorial numbers. 6 | -------------------------------------------------------------------------------- /NetCDF/README.md: -------------------------------------------------------------------------------- 1 | # mbdyn-netcdf 2 | 3 | the two patch files given in this repository show the work necessary to implement the NetCDF output on one MBDyn element; they consist of the addition of the NetCDF output to the rotor element and can be applied to MBDyn-1.7.1 4 | 5 | the submission of your code is expected to be done through a similar patch, using the patch command given here: https://www.mbdyn.org/?Documentation___Official_Documentation___FAQ#HOW_DO_I_SUBMIT_A_PATCH_TO_MBDYN 6 | 7 | you are encouraged to submit your patch directly to the Github repository 8 | -------------------------------------------------------------------------------- /NetCDF/rotor.cc.patch: -------------------------------------------------------------------------------- 1 | --- rotor.cc 2016-04-24 21:10:42.000000000 +0200 2 | +++ rotor.cc.lg 2016-09-08 14:39:20.501815000 +0200 3 | @@ -66,7 +66,7 @@ 4 | iCurrIter(0), 5 | dTolerance(0), 6 | dEta(0), 7 | -bUMeanRefConverged(false), 8 | +bUMeanRefConverged(0), 9 | Weight(), dWeight(0.), 10 | dHoverCorrection(1.), dForwardFlightCorrection(1.), 11 | RRotTranspose(::Zero3x3), RRot(::Eye3), RRot3(::Zero3), 12 | @@ -95,7 +95,7 @@ 13 | iCurrIter(0), 14 | dTolerance(0), 15 | dEta(0), 16 | -bUMeanRefConverged(false), 17 | +bUMeanRefConverged(0), 18 | Weight(), dWeight(0.), 19 | dHoverCorrection(1.), dForwardFlightCorrection(1.), 20 | RRotTranspose(::Zero3x3), RRot(::Eye3), RRot3(::Zero3), 21 | @@ -103,6 +103,19 @@ 22 | dPsi0(0.), dSinAlphad(1.), dCosAlphad(0.), 23 | dMu(0.), dLambda(1.), dChi(0.), 24 | dVelocity(0.), dOmega(0.), 25 | +#ifdef USE_NETCDF 26 | +Var_F(0), 27 | +Var_M(0), 28 | +Var_dUMean(0), 29 | +Var_dVelocity(0), 30 | +Var_dAngle(0), 31 | +Var_dMu(0), 32 | +Var_dLambda(0), 33 | +Var_dChi(0), 34 | +Var_dPsi0(0), 35 | +Var_bUMeanRef(0), 36 | +Var_iCurrIter(0), 37 | +#endif // USE_NETCDF 38 | iNumSteps(0) 39 | { 40 | Init(pC, rrot, pR, pG, ppres, dR, iMaxIt, dTol, dE, fOut); 41 | @@ -177,9 +190,215 @@ 42 | } 43 | 44 | InducedVelocity::AfterConvergence(X, XP); 45 | + 46 | +#ifdef USE_NETCDF 47 | + // calculations to do before output, 48 | +#ifdef USE_MPI 49 | +#else /* !USE_MPI */ 50 | + F = RRotTranspose*Res.Force(); 51 | + M = RRotTranspose*Res.Moment(); 52 | + dAngle = atan2(dSinAlphad,dCosAlphad); 53 | + // ,calculations to do before output 54 | +#endif /* !USE_MPI */ 55 | +#endif /* USE_NETCDF */ 56 | +} 57 | + 58 | +void 59 | +Rotor::OutputPrepare_int(const std::string& type, OutputHandler& OH, std::string& name) 60 | +{ 61 | +#ifdef USE_NETCDF 62 | + ASSERT(OH.IsOpen(OutputHandler::NETCDF)); 63 | + std::ostringstream os; 64 | + os << "elem.inducedvelocity." << GetLabel(); 65 | + (void)OH.CreateVar(os.str(), type); 66 | + os << "."; 67 | + name = os.str(); 68 | +#endif // USE_NETCDF 69 | +} 70 | + 71 | + 72 | +void 73 | +Rotor::OutputPrepare(OutputHandler &OH) 74 | +{ 75 | +#ifdef USE_NETCDF 76 | + if (bToBeOutput()) { 77 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 78 | + std::string name; 79 | + OutputPrepare_int("rotor", OH, name); 80 | + OutputPrepare_F(OH, name); 81 | + OutputPrepare_M(OH, name); 82 | + OutputPrepare_UMean(OH, name); 83 | + OutputPrepare_dVelocity(OH, name); 84 | + OutputPrepare_dAngle(OH, name); 85 | + OutputPrepare_dMu(OH, name); 86 | + OutputPrepare_dLambda(OH, name); 87 | + OutputPrepare_dChi(OH, name); 88 | + OutputPrepare_Psi0(OH, name); 89 | + OutputPrepare_bUMeanRef(OH, name); 90 | + OutputPrepare_iCurrIter(OH, name); 91 | + } 92 | + } 93 | +#endif // USE_NETCDF 94 | +} 95 | + 96 | +void 97 | +Rotor::OutputPrepare_F(OutputHandler& OH, std::string& name) 98 | +{ 99 | +#ifdef USE_NETCDF 100 | + if (bToBeOutput()) { 101 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 102 | + Var_F = OH.CreateVar(name + "F", "N", "rotor force in x, y and z directions (longitudinal, lateral and thrust components)"); 103 | + } 104 | + } 105 | +#endif // USE_NETCDF 106 | +} 107 | + 108 | +void 109 | +Rotor::OutputPrepare_M(OutputHandler& OH, std::string& name){ 110 | +#ifdef USE_NETCDF 111 | + if (bToBeOutput()) { 112 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 113 | + Var_M = OH.CreateVar(name + "M", "Nm", "rotor moment about x, y and z directions (roll, pitch and torque components)"); 114 | + } 115 | + } 116 | +#endif // USE_NETCDF 117 | +} 118 | + 119 | +void 120 | +Rotor::OutputPrepare_UMean(OutputHandler& OH, std::string& name){ 121 | +#ifdef USE_NETCDF 122 | + if (bToBeOutput()) { 123 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 124 | + Var_dUMean = OH.CreateVar(name + "dUMean", "m/s", "mean inflow velocity, based on momentum theory"); 125 | + } 126 | + } 127 | +#endif // USE_NETCDF 128 | +} 129 | + 130 | +void 131 | +Rotor::OutputPrepare_dVelocity(OutputHandler& OH, std::string& name){ 132 | +#ifdef USE_NETCDF 133 | + if (bToBeOutput()) { 134 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 135 | + Var_dVelocity = OH.CreateVar(name + "dVelocity", "m/s", "reference velocity at rotor center, sum of airstream and craft node velocity"); 136 | + } 137 | + } 138 | +#endif // USE_NETCDF 139 | +} 140 | + 141 | +void 142 | +Rotor::OutputPrepare_dAngle(OutputHandler& OH, std::string& name){ 143 | +#ifdef USE_NETCDF 144 | + if (bToBeOutput()) { 145 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 146 | + Var_dAngle = OH.CreateVar(name + "dAngle", "rad", "rotor disk angle"); 147 | + } 148 | + } 149 | +#endif // USE_NETCDF 150 | +} 151 | + 152 | +void 153 | +Rotor::OutputPrepare_dMu(OutputHandler& OH, std::string& name){ 154 | +#ifdef USE_NETCDF 155 | + if (bToBeOutput()) { 156 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 157 | + Var_dMu = OH.CreateVar(name + "dMu", "NA", "advance parameter mu"); 158 | + } 159 | + } 160 | +#endif // USE_NETCDF 161 | +} 162 | + 163 | +void 164 | +Rotor::OutputPrepare_dLambda(OutputHandler& OH, std::string& name){ 165 | +#ifdef USE_NETCDF 166 | + if (bToBeOutput()) { 167 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 168 | + Var_dLambda = OH.CreateVar(name + "dLambda", "NA", "inflow parameter lambda"); 169 | + } 170 | + } 171 | +#endif // USE_NETCDF 172 | +} 173 | + 174 | +void 175 | +Rotor::OutputPrepare_dChi(OutputHandler& OH, std::string& name){ 176 | +#ifdef USE_NETCDF 177 | + if (bToBeOutput()) { 178 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 179 | + Var_dChi = OH.CreateVar(name + "dChi", "rad", "advance/inflow angle, definition in manual"); 180 | + } 181 | + } 182 | +#endif // USE_NETCDF 183 | +} 184 | + 185 | +void 186 | +Rotor::OutputPrepare_Psi0(OutputHandler& OH, std::string& name){ 187 | +#ifdef USE_NETCDF 188 | + if (bToBeOutput()) { 189 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 190 | + Var_dPsi0 = OH.CreateVar(name + "dPsi0", "rad", "reference azimuthal direction related to rotor yaw angle"); 191 | + } 192 | + } 193 | +#endif // USE_NETCDF 194 | +} 195 | + 196 | +void 197 | +Rotor::OutputPrepare_bUMeanRef(OutputHandler& OH, std::string& name){ 198 | +#ifdef USE_NETCDF 199 | + if (bToBeOutput()) { 200 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 201 | + Var_bUMeanRef = OH.CreateVar(name + "bUMeanRef", "NA", "boolean flag indicating convergence"); 202 | + } 203 | + } 204 | +#endif // USE_NETCDF 205 | +} 206 | + 207 | +void 208 | +Rotor::OutputPrepare_iCurrIter(OutputHandler& OH, std::string& name){ 209 | +#ifdef USE_NETCDF 210 | + if (bToBeOutput()) { 211 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 212 | + Var_iCurrIter = OH.CreateVar(name + "iCurrIterVoid", "NA", "number of iterations required for convergence"); 213 | + } 214 | + } 215 | +#endif // USE_NETCDF 216 | +} 217 | + 218 | +void 219 | +Rotor::OutputPrepare_dVConst(OutputHandler& OH, std::string& name){ 220 | +#ifdef USE_NETCDF 221 | + if (bToBeOutput()) { 222 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 223 | + Var_dVConst = OH.CreateVar(name + "dVConst", "NA", "constant inflow state"); 224 | + } 225 | + } 226 | +#endif // USE_NETCDF 227 | } 228 | 229 | void 230 | +Rotor::OutputPrepare_dVSine(OutputHandler& OH, std::string& name){ 231 | +#ifdef USE_NETCDF 232 | + if (bToBeOutput()) { 233 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 234 | + Var_dVSine = OH.CreateVar(name + "dVSine", "NA", "sine inflow state (lateral)"); 235 | + } 236 | + } 237 | +#endif // USE_NETCDF 238 | +} 239 | + 240 | +void 241 | +Rotor::OutputPrepare_dVCosine(OutputHandler& OH, std::string& name){ 242 | +#ifdef USE_NETCDF 243 | + if (bToBeOutput()) { 244 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 245 | + Var_dVCosine = OH.CreateVar(name + "dVCosine", "NA", "cosine inflow state (longitudinal)"); 246 | + } 247 | + } 248 | +#endif // USE_NETCDF 249 | +} 250 | + 251 | + 252 | + 253 | +void 254 | Rotor::Output(OutputHandler& OH) const 255 | { 256 | if (bToBeOutput()) { 257 | @@ -243,6 +462,21 @@ 258 | } 259 | 260 | #else /* !USE_MPI */ 261 | +#ifdef USE_NETCDF 262 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 263 | + Var_F->put_rec(F.pGetVec(), OH.GetCurrentStep()); 264 | + Var_M->put_rec(M.pGetVec(), OH.GetCurrentStep()); 265 | + Var_dUMean->put_rec(&dUMean, OH.GetCurrentStep()); 266 | + Var_dVelocity->put_rec((&dVelocity), OH.GetCurrentStep()); 267 | + Var_dAngle->put_rec((&dAngle), OH.GetCurrentStep()); 268 | + Var_dMu->put_rec((&dMu), OH.GetCurrentStep()); 269 | + Var_dLambda->put_rec((&dLambda), OH.GetCurrentStep()); 270 | + Var_dChi->put_rec((&dChi), OH.GetCurrentStep()); 271 | + Var_dPsi0->put_rec((&dPsi0), OH.GetCurrentStep()); 272 | + Var_bUMeanRef->put_rec((&bUMeanRefConverged), OH.GetCurrentStep()); 273 | + Var_iCurrIter->put_rec((&iCurrIter), OH.GetCurrentStep()); 274 | + } 275 | +#endif /* USE_NETCDF */ 276 | OH.Rotors() 277 | << std::setw(8) << GetLabel() /* 1 */ 278 | << " " << RRotTranspose*Res.Force() /* 2-4 */ 279 | @@ -425,7 +659,7 @@ 280 | dGE -= 1./(z*z); 281 | } 282 | 283 | - bUMeanRefConverged = false; 284 | + bUMeanRefConverged = 0; 285 | if (dVTip > dVTipTreshold*dVTipRef) { 286 | doublereal dCt = dT/(dRho*dArea*dVTip*dVTip); 287 | doublereal dLambda0 = dVelocity*dSinAlphad/dVTip; 288 | @@ -459,7 +693,7 @@ 289 | #endif 290 | 291 | if (std::abs(dF) <= dTolerance) { 292 | - bUMeanRefConverged = true; 293 | + bUMeanRefConverged = 1; 294 | break; 295 | } 296 | } 297 | @@ -1615,6 +1849,38 @@ 298 | 299 | 300 | void 301 | +DynamicInflowRotor::OutputPrepare(OutputHandler &OH) 302 | +{ 303 | +#ifdef USE_NETCDF 304 | + if (bToBeOutput()) { 305 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 306 | +#ifdef USE_MPI 307 | +#else /* !USE_MPI */ 308 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 309 | + std::string name; 310 | + OutputPrepare_int("rotor", OH, name); 311 | + OutputPrepare_F(OH, name); 312 | + OutputPrepare_M(OH, name); 313 | + OutputPrepare_UMean(OH, name); 314 | + OutputPrepare_dVelocity(OH, name); 315 | + OutputPrepare_dAngle(OH, name); 316 | + OutputPrepare_dMu(OH, name); 317 | + OutputPrepare_dLambda(OH, name); 318 | + OutputPrepare_dChi(OH, name); 319 | + OutputPrepare_Psi0(OH, name); 320 | + OutputPrepare_bUMeanRef(OH, name); 321 | + OutputPrepare_iCurrIter(OH, name); 322 | + OutputPrepare_dVConst(OH, name); 323 | + OutputPrepare_dVSine(OH, name); 324 | + OutputPrepare_dVCosine(OH, name); 325 | + } 326 | +#endif /* !USE_MPI */ 327 | + } 328 | + } 329 | +#endif // USE_NETCDF 330 | +} 331 | + 332 | +void 333 | DynamicInflowRotor::Output(OutputHandler& OH) const 334 | { 335 | /* 336 | @@ -1687,6 +1953,24 @@ 337 | } 338 | 339 | #else /* !USE_MPI */ 340 | +#ifdef USE_NETCDF 341 | + if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) { 342 | + Var_F->put_rec(F.pGetVec(), OH.GetCurrentStep()); 343 | + Var_M->put_rec(M.pGetVec(), OH.GetCurrentStep()); 344 | + Var_dUMean->put_rec(&dUMean, OH.GetCurrentStep()); 345 | + Var_dVelocity->put_rec((&dVelocity), OH.GetCurrentStep()); 346 | + Var_dAngle->put_rec((&dAngle), OH.GetCurrentStep()); 347 | + Var_dMu->put_rec((&dMu), OH.GetCurrentStep()); 348 | + Var_dLambda->put_rec((&dLambda), OH.GetCurrentStep()); 349 | + Var_dChi->put_rec((&dChi), OH.GetCurrentStep()); 350 | + Var_dPsi0->put_rec((&dPsi0), OH.GetCurrentStep()); 351 | + Var_bUMeanRef->put_rec((&bUMeanRefConverged), OH.GetCurrentStep()); 352 | + Var_iCurrIter->put_rec((&iCurrIter), OH.GetCurrentStep()); 353 | + Var_dVConst->put_rec((&dVConst), OH.GetCurrentStep()); 354 | + Var_dVSine->put_rec((&dVSine), OH.GetCurrentStep()); 355 | + Var_dVCosine->put_rec((&dVCosine), OH.GetCurrentStep()); 356 | + } 357 | +#endif /* USE_NETCDF */ 358 | OH.Rotors() 359 | << std::setw(8) << GetLabel() /* 1 */ 360 | << " " << RRotTranspose*Res.Force() /* 2-4 */ 361 | -------------------------------------------------------------------------------- /NetCDF/rotor.h.patch: -------------------------------------------------------------------------------- 1 | --- rotor.h 2015-10-30 06:05:37.000000000 +0100 2 | +++ rotor.h.lg 2016-09-08 14:41:21.069817000 +0200 3 | @@ -57,10 +57,10 @@ 4 | 5 | // iterations for dUMeanRef 6 | unsigned int iMaxIter; 7 | - unsigned int iCurrIter; 8 | + int iCurrIter; 9 | doublereal dTolerance; 10 | doublereal dEta; 11 | - bool bUMeanRefConverged; 12 | + int bUMeanRefConverged; 13 | 14 | DriveOwner Weight; 15 | // Peso della velocita' indotta media 16 | @@ -113,6 +113,41 @@ 17 | const doublereal& dTol, 18 | const doublereal& dE, 19 | flag fOut); 20 | + 21 | +#ifdef USE_NETCDF 22 | + Vec3 F; 23 | + Vec3 M; 24 | + doublereal dAngle; 25 | + NcVar *Var_F; 26 | + NcVar *Var_M; 27 | + NcVar *Var_dUMean; 28 | + NcVar *Var_dVelocity; 29 | + NcVar *Var_dAngle; 30 | + NcVar *Var_dMu; 31 | + NcVar *Var_dLambda; 32 | + NcVar *Var_dChi; 33 | + NcVar *Var_dPsi0; 34 | + NcVar *Var_bUMeanRef; 35 | + NcVar *Var_iCurrIter; 36 | + NcVar *Var_dVConst; 37 | + NcVar *Var_dVSine; 38 | + NcVar *Var_dVCosine; 39 | + virtual void OutputPrepare_int(const std::string& type, OutputHandler& OH, std::string& name); 40 | + void OutputPrepare_F(OutputHandler& OH, std::string& name); 41 | + void OutputPrepare_M(OutputHandler& OH, std::string& name); 42 | + void OutputPrepare_UMean(OutputHandler& OH, std::string& name); 43 | + void OutputPrepare_dVelocity(OutputHandler& OH, std::string& name); 44 | + void OutputPrepare_dAngle(OutputHandler& OH, std::string& name); 45 | + void OutputPrepare_dMu(OutputHandler& OH, std::string& name); 46 | + void OutputPrepare_dLambda(OutputHandler& OH, std::string& name); 47 | + void OutputPrepare_dChi(OutputHandler& OH, std::string& name); 48 | + void OutputPrepare_Psi0(OutputHandler& OH, std::string& name); 49 | + void OutputPrepare_bUMeanRef(OutputHandler& OH, std::string& name); 50 | + void OutputPrepare_iCurrIter(OutputHandler& OH, std::string& name); 51 | + void OutputPrepare_dVConst(OutputHandler& OH, std::string& name); 52 | + void OutputPrepare_dVSine(OutputHandler& OH, std::string& name); 53 | + void OutputPrepare_dVCosine(OutputHandler& OH, std::string& name); 54 | +#endif /* USE_NETCDF */ 55 | 56 | public: 57 | Rotor(unsigned int uL, const DofOwner* pDO); 58 | @@ -133,6 +168,9 @@ 59 | 60 | // output; si assume che ogni tipo di elemento sappia, 61 | // attraverso l'OutputHandler, dove scrivere il proprio output 62 | +#ifdef USE_NETCDF 63 | + virtual void OutputPrepare(OutputHandler &OH); // for NETCDF 64 | +#endif /* USE_NETCDF */ 65 | virtual void Output(OutputHandler& OH) const; 66 | 67 | // Contributo al file di Restart 68 | @@ -596,6 +634,9 @@ 69 | return 3; 70 | }; 71 | 72 | +#ifdef USE_NETCDF 73 | + virtual void OutputPrepare(OutputHandler &OH); // for NETCDF 74 | +#endif /* USE_NETCDF */ 75 | // output; si assume che ogni tipo di elemento sappia, 76 | // attraverso l'OutputHandler, dove scrivere il proprio output 77 | virtual void Output(OutputHandler& OH) const; 78 | -------------------------------------------------------------------------------- /README.md: -------------------------------------------------------------------------------- 1 | # Codeheat 2 | 3 | Join us for the Codeheat contest at https://codeheat.org 4 | 5 | # Archive 6 | 7 | ### mbdyn tasks archive 8 | 9 | MBDyn tasks for Code-in. Look for your specific task in the given subfolders. 10 | -------------------------------------------------------------------------------- /airfoilData/README.md: -------------------------------------------------------------------------------- 1 | # mbdyn-airfoils 2 | Instructions for eventual contributors 3 | 4 | **Google code-in Warning:** this may be a challenging task! Unless you really know what you are doing, follow the instructions of the "Google code-in" section below to avoid a very long task. 5 | 6 | repository of c81 airfoil data to use with MBDyn 7 | 8 | You can generate the data using the software of your choice (such as XFLR5 or Xfoil) or get the data from the cactus released airfoil data for NACA0015, 18, and 21 airfoils in the cactusImport subdirectory. 9 | 10 | WARNING: you must however check the proper Mach number of these files, and it is not always available. Other data can be also gathered from the following document and converted using OCR: http://www.osti.gov/servlets/purl/6548367 Some of the data in that document is also available in numerical format inside the cactusImport directory. 11 | 12 | Example OCR procedure: 1. if the document is in pdf extract the desired page; 2. convert it to an image with high definition: `convert -density 300 ddddd.pdf ddd.png` 3. run ocr on it: `tesseract ./ddd.png ./d2` 4. manually check every number as some errors always occur, especially between 3 and 8 and between 5 and 6. 13 | 14 | 15 | Most data you will be able to obtain will be for low Mach number, thus, in the event that you are not able to get airfoil data at higher Mach numbers, it is reasonable to produce a low Mach C81 file. You have two options: either use only Mach 0 column and chose a best estimate of your application's Reynolds/Mach number combination. Or better, make a series of Mach columns that are the corresponding Machs for the Reynolds numbers for which you have data available. This will allow you to perform analyses that consider the influence of the Reynolds number of the airfoil properties but ignore the compressibility effects... 16 | 17 | Another source of drag and lift coefficient is available here: http://www.dtic.mil/dtic/tr/fulltext/u2/a420649.pdf however, no clear coefficients of moment are given. See the code in the appendices. The data comes from http://oai.dtic.mil/oai/oai?verb=getRecord&metadataPrefix=html&identifier=AD0911537 but no information on coefficient of moment was found outside the [-10°, 22°] angle of attack range. 18 | 19 | Other airfoil data is also available in the following documents: https://ntrs.nasa.gov/search.jsp?R=19880002258 and https://ntrs.nasa.gov/search.jsp?R=19840020737 and http://www.nrel.gov/docs/legosti/old/2559.pdf 20 | 21 | Finally, a plot digitizer tool may be useful if you are to get data points from old plots inside digitial documents: http://markummitchell.github.io/engauge-digitizer/ 22 | 23 | The following procedure is suggested for testing your newly created C81 file, but not required. You can have your own testing procedure for the newly created airfoil data file: 24 | 25 | 26 | 1. run MBDyn with the new c81 input file using the airfoil.mbd from this repository: 27 | 28 | `mbdyn airfoil.mbd -o DEL` 29 | 30 | 2. observe your resulting lift, drag, and moment coefficients when running MBDyn: 31 | 32 | for lift coefficient: `cat DEL.aer |grep " 1"|awk {'print $2, $5'}|feedgnuplot --domain` 33 | 34 | for drag coefficient: `cat DEL.aer |grep " 1"|awk {'print $2, $6'}|feedgnuplot --domain` 35 | 36 | for moment coefficient: `cat DEL.aer |grep " 1"|awk {'print $2, $7'}|feedgnuplot --domain` 37 | 38 | 39 | Instructions for the Google code-in 40 | ====== 41 | 42 | --- 43 | 44 | 1. take one of the three airfoil properties file from the cactusImport directories 45 | 46 | 2. convert the Reynolds numbers into Mach numbers using the following rule which applies only to the cactusImport dataset for 15.24cm chord airfoils: Mach = Reynolds * 2.8177e-07 47 | 48 | 3. prepare the C81 free format file, as described on p.35 of the MBDyn manual (https://www.mbdyn.org/userfiles/documents/mbdyn-input-1.7.1.pdf) and as shown in the NACA0012 example file "naca0012_free_format.c81" 49 | 50 | 4. to increase the chances that your task gets accepted on your first try, you may check that your new file works and gives the results similar as the default naca0012 file by running the MBDyn testing procedure given above 51 | 52 | 5. upload your c81 file in the "gci_submissions" folder 53 | 54 | 55 | --- 56 | -------------------------------------------------------------------------------- /airfoilData/airfoil.mbd: -------------------------------------------------------------------------------- 1 | # $Header: /var/cvs/mbdyn/mbdyn/mbdyn-web/documentation/examples/rigidbody,v 1.6 2009/07/04 17:36:08 masarati Exp $ 2 | # modified example case to allow testing of airfoil aerodynamic properties 3 | 4 | begin: data; 5 | problem: initial value; # the default 6 | end: data; 7 | 8 | set: const integer GROUND = 0; 9 | set: integer AERO_INTEGRATION_POINTS = 1; 10 | set: const real SPAN = 0.8; # m 11 | set: const real CHORD = 0.15; # m; estimated 12 | set: const integer NACA0012 = 12; 13 | c81 data: NACA0012, "naca0012.c81"; 14 | 15 | begin: initial value; 16 | initial time: 0.; 17 | final time: 10.; 18 | time step: 1.e-3; 19 | 20 | max iterations: 10; 21 | tolerance: 1.e-6; 22 | 23 | derivatives coefficient: 1.e-6; 24 | end: initial value; 25 | 26 | begin: control data; 27 | output results: netcdf; 28 | structural nodes: 2; 29 | # rigid bodies: 1; 30 | aerodynamic elements: 1; 31 | air properties; 32 | joints: 2; 33 | end: control data; 34 | 35 | reference: GROUND, 36 | reference, global, null, 37 | reference, global, eye, 38 | reference, global, null, 39 | reference, global, null; 40 | 41 | begin: nodes; 42 | # in zero, with horizontal speed 43 | structural: 1, 44 | dynamic, 45 | null, 46 | euler, 0, 0*5./180.*pi, 0, 47 | 0.,0.,0., 48 | null; 49 | 50 | structural: GROUND, static, 51 | reference, GROUND, null, 52 | reference, GROUND, eye, 53 | reference, GROUND, null, 54 | reference, GROUND, null; 55 | end: nodes; 56 | 57 | begin: elements; 58 | # body: 1, 1, 1., null, eye; 59 | 60 | joint: GROUND, clamp, GROUND, node, node; 61 | 62 | 63 | joint: 1, axial rotation, # drum rotation 64 | GROUND, 65 | position, null, 66 | orientation, 67 | 3, 0., 0., 1., 68 | 1, 1., 0., 0., 69 | 1, 70 | position, null, 71 | orientation, 72 | 3, 0., 0., 1., 73 | 1, 1., 0., 0., 74 | const, 8.; # ang. vel. 75 | 76 | aerodynamic body: 1, 77 | 1, 78 | reference, node, 79 | 0., 0., 0., 80 | reference, node, 81 | 1, 1., 0., 0., 82 | 2, 0., 1., 0., 83 | SPAN, 84 | const, CHORD, # chord 85 | const, CHORD/4, # aero center (approx) 86 | const, CHORD*0, # b c point 87 | const, 0., # twist 88 | # tip loss, const, 0.95, 89 | AERO_INTEGRATION_POINTS, 90 | # theodorsen, 91 | c81, NACA0012, 92 | jacobian, no; 93 | 94 | air properties: 95 | 1.204, 343., 96 | 1.0, 0., 0., const, 20.; # air velocity 97 | end: elements; 98 | 99 | -------------------------------------------------------------------------------- /airfoilData/cactusImport/LICENSE.TXT: -------------------------------------------------------------------------------- 1 | The airfoil data files contained in this directory were released along 2 | with the Cactus code 3 | http://energy.sandia.gov/energy/renewable-energy/wind-power/wind-resources/wind-software-downloads/cactus-software-download/ 4 | and thus the original license is copied below for reference. 5 | 6 | Copyright (c) 2013, Sandia Corporation. Under the terms of Contract 7 | DE-AC04-94AL85000 with Sandia Corporation, the U.S. Government retains 8 | certain rights in this software. 9 | 10 | Redistribution and use in source and binary forms, with or without 11 | modification, are permitted provided that the following conditions are 12 | met: 13 | 14 | o Redistributions of source code must retain the above copyright 15 | notice, this list of conditions and the following disclaimer. 16 | 17 | o Redistributions in binary form must reproduce the above copyright 18 | notice, this list of conditions and the following disclaimer in the 19 | documentation and/or other materials provided with the distribution. 20 | 21 | o Neither the name of Sandia Corporation nor the names of its 22 | contributors may be used to endorse or promote products derived from 23 | this software without specific prior written permission. 24 | 25 | 26 | THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS 27 | "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT 28 | LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR 29 | A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT 30 | HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, 31 | SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT 32 | LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, 33 | DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ANY 34 | THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT 35 | (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE 36 | OF THIS SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE. 37 | -------------------------------------------------------------------------------- /airfoilData/cactusImport/NACA_0015.dat: -------------------------------------------------------------------------------- 1 | Title: NACA0015 2 | Thickness to Chord Ratio: 0.15 3 | Zero Lift AOA (deg): 0.0 4 | Reverse Camber Direction: 0 5 | 6 | Reynolds Number: 1e4 7 | BV Dyn. Stall Model - Positive Stall AOA (deg): 1.0 8 | BV Dyn. Stall Model - Negative Stall AOA (deg): -1.0 9 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 5.73 10 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1 11 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1 12 | AOA (deg) CL CD Cm25 13 | -180.0000 0.0000 0.0250 0.0000 14 | -175.0000 0.6600 0.0550 0.0000 15 | -170.0000 0.8500 0.1400 0.0000 16 | -165.0000 0.6800 0.2300 0.0000 17 | -160.0000 0.6350 0.3200 0.0000 18 | -155.0000 0.6700 0.4200 0.0000 19 | -150.0000 0.7700 0.5750 0.0000 20 | -145.0000 0.9000 0.7550 0.0000 21 | -140.0000 0.9800 0.9250 0.0000 22 | -135.0000 0.9300 1.0850 0.0000 23 | -130.0000 0.8500 1.2250 0.0000 24 | -125.0000 0.7600 1.3500 0.0000 25 | -120.0000 0.6700 1.4650 0.0000 26 | -115.0000 0.5750 1.5550 0.0000 27 | -110.0000 0.4500 1.6350 0.0000 28 | -105.0000 0.3200 1.7000 0.0000 29 | -100.0000 0.1850 1.7500 0.0000 30 | -95.0000 0.0500 1.7800 0.0000 31 | -90.0000 -0.0900 1.8000 0.0000 32 | -85.0000 -0.2300 1.8000 0.0000 33 | -80.0000 -0.3650 1.7800 0.0000 34 | -75.0000 -0.5000 1.7350 0.0000 35 | -70.0000 -0.6300 1.6650 0.0000 36 | -65.0000 -0.7600 1.5750 0.0000 37 | -60.0000 -0.8750 1.4700 0.0000 38 | -55.0000 -0.9550 1.3450 0.0000 39 | -50.0000 -1.0200 1.2150 0.0000 40 | -45.0000 -1.0500 1.0750 0.0000 41 | -40.0000 -1.0350 0.9200 0.0000 42 | -35.0000 -0.9800 0.7450 0.0000 43 | -30.0000 -0.8550 0.5700 0.0000 44 | -27.0000 -0.8174 0.4600 0.0000 45 | -26.0000 -0.7639 0.4320 0.0000 46 | -25.0000 -0.7099 0.4050 0.0000 47 | -24.0000 -0.6559 0.3790 0.0000 48 | -23.0000 -0.6019 0.3540 0.0000 49 | -22.0000 -0.5479 0.3290 0.0000 50 | -21.0000 -0.4939 0.3050 0.0000 51 | -20.0000 -0.4399 0.2820 0.0000 52 | -19.0000 -0.3859 0.2600 0.0000 53 | -18.0000 -0.3319 0.2380 0.0000 54 | -17.0000 -0.2780 0.2170 0.0000 55 | -16.0000 -0.2242 0.1960 0.0000 56 | -15.0000 -0.1706 0.1770 0.0000 57 | -14.0000 -0.1172 0.1580 0.0000 58 | -13.0000 -0.0649 0.1400 0.0000 59 | -12.0000 -0.0138 0.1230 0.0000 60 | -11.0000 0.0348 0.1070 0.0000 61 | -10.0000 0.0791 0.0910 0.0000 62 | -9.0000 0.1194 0.0770 0.0000 63 | -8.0000 0.1484 0.0640 0.0000 64 | -7.0000 0.1517 0.0510 0.0000 65 | -6.0000 0.0781 0.0400 0.0000 66 | -5.0000 -0.0162 0.0393 0.0000 67 | -4.0000 -0.0581 0.0383 0.0000 68 | -3.0000 -0.0725 0.0373 0.0000 69 | -2.0000 -0.0715 0.0366 0.0000 70 | -1.0000 -0.0434 0.0362 0.0000 71 | 0.0000 0.0000 0.0360 0.0000 72 | 1.0000 0.0434 0.0362 0.0000 73 | 2.0000 0.0715 0.0366 0.0000 74 | 3.0000 0.0725 0.0373 0.0000 75 | 4.0000 0.0581 0.0383 0.0000 76 | 5.0000 0.0162 0.0393 0.0000 77 | 6.0000 -0.0781 0.0400 0.0000 78 | 7.0000 -0.1517 0.0510 0.0000 79 | 8.0000 -0.1484 0.0640 0.0000 80 | 9.0000 -0.1194 0.0770 0.0000 81 | 10.0000 -0.0791 0.0910 0.0000 82 | 11.0000 -0.0348 0.1070 0.0000 83 | 12.0000 0.0138 0.1230 0.0000 84 | 13.0000 0.0649 0.1400 0.0000 85 | 14.0000 0.1172 0.1580 0.0000 86 | 15.0000 0.1706 0.1770 0.0000 87 | 16.0000 0.2242 0.1960 0.0000 88 | 17.0000 0.2780 0.2170 0.0000 89 | 18.0000 0.3319 0.2380 0.0000 90 | 19.0000 0.3859 0.2600 0.0000 91 | 20.0000 0.4399 0.2820 0.0000 92 | 21.0000 0.4939 0.3050 0.0000 93 | 22.0000 0.5479 0.3290 0.0000 94 | 23.0000 0.6019 0.3540 0.0000 95 | 24.0000 0.6559 0.3790 0.0000 96 | 25.0000 0.7099 0.4050 0.0000 97 | 26.0000 0.7639 0.4320 0.0000 98 | 27.0000 0.8174 0.4600 0.0000 99 | 30.0000 0.8550 0.5700 0.0000 100 | 35.0000 0.9800 0.7450 0.0000 101 | 40.0000 1.0350 0.9200 0.0000 102 | 45.0000 1.0500 1.0750 0.0000 103 | 50.0000 1.0200 1.2150 0.0000 104 | 55.0000 0.9550 1.3450 0.0000 105 | 60.0000 0.8750 1.4700 0.0000 106 | 65.0000 0.7600 1.5750 0.0000 107 | 70.0000 0.6300 1.6650 0.0000 108 | 75.0000 0.5000 1.7350 0.0000 109 | 80.0000 0.3650 1.7800 0.0000 110 | 85.0000 0.2300 1.8000 0.0000 111 | 90.0000 0.0900 1.8000 0.0000 112 | 95.0000 -0.0500 1.7800 0.0000 113 | 100.0000 -0.1850 1.7500 0.0000 114 | 105.0000 -0.3200 1.7000 0.0000 115 | 110.0000 -0.4500 1.6350 0.0000 116 | 115.0000 -0.5750 1.5550 0.0000 117 | 120.0000 -0.6700 1.4650 0.0000 118 | 125.0000 -0.7600 1.3500 0.0000 119 | 130.0000 -0.8500 1.2250 0.0000 120 | 135.0000 -0.9300 1.0850 0.0000 121 | 140.0000 -0.9800 0.9250 0.0000 122 | 145.0000 -0.9000 0.7550 0.0000 123 | 150.0000 -0.7700 0.5750 0.0000 124 | 155.0000 -0.6700 0.4200 0.0000 125 | 160.0000 -0.6350 0.3200 0.0000 126 | 165.0000 -0.6800 0.2300 0.0000 127 | 170.0000 -0.8500 0.1400 0.0000 128 | 175.0000 -0.6600 0.0550 0.0000 129 | 180.0000 0.0000 0.0250 0.0000 130 | 131 | Reynolds Number: 2e4 132 | BV Dyn. Stall Model - Positive Stall AOA (deg): 2.0 133 | BV Dyn. Stall Model - Negative Stall AOA (deg): -2.0 134 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 5.73 135 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1 136 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1 137 | AOA (deg) CL CD Cm25 138 | -180.0000 0.0000 0.0250 0.0000 139 | -175.0000 0.6600 0.0550 0.0000 140 | -170.0000 0.8500 0.1400 0.0000 141 | -165.0000 0.6800 0.2300 0.0000 142 | -160.0000 0.6350 0.3200 0.0000 143 | -155.0000 0.6700 0.4200 0.0000 144 | -150.0000 0.7700 0.5750 0.0000 145 | -145.0000 0.9000 0.7550 0.0000 146 | -140.0000 0.9800 0.9250 0.0000 147 | -135.0000 0.9300 1.0850 0.0000 148 | -130.0000 0.8500 1.2250 0.0000 149 | -125.0000 0.7600 1.3500 0.0000 150 | -120.0000 0.6700 1.4650 0.0000 151 | -115.0000 0.5750 1.5550 0.0000 152 | -110.0000 0.4500 1.6350 0.0000 153 | -105.0000 0.3200 1.7000 0.0000 154 | -100.0000 0.1850 1.7500 0.0000 155 | -95.0000 0.0500 1.7800 0.0000 156 | -90.0000 -0.0900 1.8000 0.0000 157 | -85.0000 -0.2300 1.8000 0.0000 158 | -80.0000 -0.3650 1.7800 0.0000 159 | -75.0000 -0.5000 1.7350 0.0000 160 | -70.0000 -0.6300 1.6650 0.0000 161 | -65.0000 -0.7600 1.5750 0.0000 162 | -60.0000 -0.8750 1.4700 0.0000 163 | -55.0000 -0.9550 1.3450 0.0000 164 | -50.0000 -1.0200 1.2150 0.0000 165 | -45.0000 -1.0500 1.0750 0.0000 166 | -40.0000 -1.0350 0.9200 0.0000 167 | -35.0000 -0.9800 0.7450 0.0000 168 | -30.0000 -0.8550 0.5700 0.0000 169 | -27.0000 -0.8191 0.4600 0.0000 170 | -26.0000 -0.7649 0.4320 0.0000 171 | -25.0000 -0.7109 0.4050 0.0000 172 | -24.0000 -0.6569 0.3790 0.0000 173 | -23.0000 -0.6029 0.3540 0.0000 174 | -22.0000 -0.5489 0.3290 0.0000 175 | -21.0000 -0.4949 0.3050 0.0000 176 | -20.0000 -0.4409 0.2820 0.0000 177 | -19.0000 -0.3869 0.2600 0.0000 178 | -18.0000 -0.3331 0.2380 0.0000 179 | -17.0000 -0.2792 0.2170 0.0000 180 | -16.0000 -0.2256 0.1960 0.0000 181 | -15.0000 -0.1721 0.1770 0.0000 182 | -14.0000 -0.1193 0.1580 0.0000 183 | -13.0000 -0.0678 0.1400 0.0000 184 | -12.0000 -0.0173 0.1230 0.0000 185 | -11.0000 0.0300 0.1070 0.0000 186 | -10.0000 0.0728 0.0910 0.0000 187 | -9.0000 0.1050 0.0770 0.0000 188 | -8.0000 0.1104 0.0640 0.0000 189 | -7.0000 -0.0570 0.0510 0.0000 190 | -6.0000 -0.3001 0.0410 0.0000 191 | -5.0000 -0.3359 0.0303 0.0000 192 | -4.0000 -0.3041 0.0290 0.0000 193 | -3.0000 -0.2452 0.0279 0.0000 194 | -2.0000 -0.1740 0.0271 0.0000 195 | -1.0000 -0.0891 0.0267 0.0000 196 | 0.0000 0.0000 0.0265 0.0000 197 | 1.0000 0.0891 0.0267 0.0000 198 | 2.0000 0.1740 0.0271 0.0000 199 | 3.0000 0.2452 0.0279 0.0000 200 | 4.0000 0.3041 0.0290 0.0000 201 | 5.0000 0.3359 0.0303 0.0000 202 | 6.0000 0.3001 0.0410 0.0000 203 | 7.0000 0.0570 0.0510 0.0000 204 | 8.0000 -0.1104 0.0640 0.0000 205 | 9.0000 -0.1050 0.0770 0.0000 206 | 10.0000 -0.0728 0.0910 0.0000 207 | 11.0000 -0.0300 0.1070 0.0000 208 | 12.0000 0.0173 0.1230 0.0000 209 | 13.0000 0.0678 0.1400 0.0000 210 | 14.0000 0.1193 0.1580 0.0000 211 | 15.0000 0.1721 0.1770 0.0000 212 | 16.0000 0.2256 0.1960 0.0000 213 | 17.0000 0.2792 0.2170 0.0000 214 | 18.0000 0.3331 0.2380 0.0000 215 | 19.0000 0.3869 0.2600 0.0000 216 | 20.0000 0.4409 0.2820 0.0000 217 | 21.0000 0.4949 0.3050 0.0000 218 | 22.0000 0.5489 0.3290 0.0000 219 | 23.0000 0.6029 0.3540 0.0000 220 | 24.0000 0.6569 0.3790 0.0000 221 | 25.0000 0.7109 0.4050 0.0000 222 | 26.0000 0.7649 0.4320 0.0000 223 | 27.0000 0.8191 0.4600 0.0000 224 | 30.0000 0.8550 0.5700 0.0000 225 | 35.0000 0.9800 0.7450 0.0000 226 | 40.0000 1.0350 0.9200 0.0000 227 | 45.0000 1.0500 1.0750 0.0000 228 | 50.0000 1.0200 1.2150 0.0000 229 | 55.0000 0.9550 1.3450 0.0000 230 | 60.0000 0.8750 1.4700 0.0000 231 | 65.0000 0.7600 1.5750 0.0000 232 | 70.0000 0.6300 1.6650 0.0000 233 | 75.0000 0.5000 1.7350 0.0000 234 | 80.0000 0.3650 1.7800 0.0000 235 | 85.0000 0.2300 1.8000 0.0000 236 | 90.0000 0.0900 1.8000 0.0000 237 | 95.0000 -0.0500 1.7800 0.0000 238 | 100.0000 -0.1850 1.7500 0.0000 239 | 105.0000 -0.3200 1.7000 0.0000 240 | 110.0000 -0.4500 1.6350 0.0000 241 | 115.0000 -0.5750 1.5550 0.0000 242 | 120.0000 -0.6700 1.4650 0.0000 243 | 125.0000 -0.7600 1.3500 0.0000 244 | 130.0000 -0.8500 1.2250 0.0000 245 | 135.0000 -0.9300 1.0850 0.0000 246 | 140.0000 -0.9800 0.9250 0.0000 247 | 145.0000 -0.9000 0.7550 0.0000 248 | 150.0000 -0.7700 0.5750 0.0000 249 | 155.0000 -0.6700 0.4200 0.0000 250 | 160.0000 -0.6350 0.3200 0.0000 251 | 165.0000 -0.6800 0.2300 0.0000 252 | 170.0000 -0.8500 0.1400 0.0000 253 | 175.0000 -0.6600 0.0550 0.0000 254 | 180.0000 0.0000 0.0250 0.0000 255 | 256 | Reynolds Number: 4e4 257 | BV Dyn. Stall Model - Positive Stall AOA (deg): 4.0 258 | BV Dyn. Stall Model - Negative Stall AOA (deg): -4.0 259 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 5.879 260 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 0.72 261 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -0.72 262 | AOA (deg) CL CD Cm25 263 | -180.0000 0.0000 0.0250 0.0000 264 | -175.0000 0.6600 0.0550 0.0000 265 | -170.0000 0.8500 0.1400 0.0000 266 | -165.0000 0.6800 0.2300 0.0000 267 | -160.0000 0.6350 0.3200 0.0000 268 | -155.0000 0.6700 0.4200 0.0000 269 | -150.0000 0.7700 0.5750 0.0000 270 | -145.0000 0.9000 0.7550 0.0000 271 | -140.0000 0.9800 0.9250 0.0000 272 | -135.0000 0.9300 1.0850 0.0000 273 | -130.0000 0.8500 1.2250 0.0000 274 | -125.0000 0.7600 1.3500 0.0000 275 | -120.0000 0.6700 1.4650 0.0000 276 | -115.0000 0.5750 1.5550 0.0000 277 | -110.0000 0.4500 1.6350 0.0000 278 | -105.0000 0.3200 1.7000 0.0000 279 | -100.0000 0.1850 1.7500 0.0000 280 | -95.0000 0.0500 1.7800 0.0000 281 | -90.0000 -0.0900 1.8000 0.0000 282 | -85.0000 -0.2300 1.8000 0.0000 283 | -80.0000 -0.3650 1.7800 0.0000 284 | -75.0000 -0.5000 1.7350 0.0000 285 | -70.0000 -0.6300 1.6650 0.0000 286 | -65.0000 -0.7600 1.5750 0.0000 287 | -60.0000 -0.8750 1.4700 0.0000 288 | -55.0000 -0.9550 1.3450 0.0000 289 | -50.0000 -1.0200 1.2150 0.0000 290 | -45.0000 -1.0500 1.0750 0.0000 291 | -40.0000 -1.0350 0.9200 0.0000 292 | -35.0000 -0.9800 0.7450 0.0000 293 | -30.0000 -0.8550 0.5700 0.0000 294 | -27.0000 -0.8222 0.4600 0.0000 295 | -26.0000 -0.7666 0.4320 0.0000 296 | -25.0000 -0.7125 0.4050 0.0000 297 | -24.0000 -0.6585 0.3790 0.0000 298 | -23.0000 -0.6045 0.3540 0.0000 299 | -22.0000 -0.5506 0.3290 0.0000 300 | -21.0000 -0.4966 0.3050 0.0000 301 | -20.0000 -0.4427 0.2820 0.0000 302 | -19.0000 -0.3889 0.2600 0.0000 303 | -18.0000 -0.3351 0.2380 0.0000 304 | -17.0000 -0.2815 0.2170 0.0000 305 | -16.0000 -0.2280 0.1960 0.0000 306 | -15.0000 -0.1756 0.1770 0.0000 307 | -14.0000 -0.1244 0.1580 0.0000 308 | -13.0000 -0.0741 0.1400 0.0000 309 | -12.0000 -0.0261 0.1230 0.0000 310 | -11.0000 0.0144 0.1070 0.0000 311 | -10.0000 0.0413 0.0910 0.0000 312 | -9.0000 -0.0433 0.0770 0.0000 313 | -8.0000 -0.4663 0.0520 0.0000 314 | -7.0000 -0.5730 0.0267 0.0000 315 | -6.0000 -0.5551 0.0249 0.0000 316 | -5.0000 -0.4871 0.0232 0.0000 317 | -4.0000 -0.4017 0.0219 0.0000 318 | -3.0000 -0.3078 0.0209 0.0000 319 | -2.0000 -0.2099 0.0202 0.0000 320 | -1.0000 -0.1054 0.0198 0.0000 321 | 0.0000 0.0000 0.0196 0.0000 322 | 1.0000 0.1054 0.0198 0.0000 323 | 2.0000 0.2099 0.0202 0.0000 324 | 3.0000 0.3078 0.0209 0.0000 325 | 4.0000 0.4017 0.0219 0.0000 326 | 5.0000 0.4871 0.0232 0.0000 327 | 6.0000 0.5551 0.0249 0.0000 328 | 7.0000 0.5730 0.0267 0.0000 329 | 8.0000 0.4663 0.0520 0.0000 330 | 9.0000 0.0433 0.0770 0.0000 331 | 10.0000 -0.0413 0.0910 0.0000 332 | 11.0000 -0.0144 0.1070 0.0000 333 | 12.0000 0.0261 0.1230 0.0000 334 | 13.0000 0.0741 0.1400 0.0000 335 | 14.0000 0.1244 0.1580 0.0000 336 | 15.0000 0.1756 0.1770 0.0000 337 | 16.0000 0.2280 0.1960 0.0000 338 | 17.0000 0.2815 0.2170 0.0000 339 | 18.0000 0.3351 0.2380 0.0000 340 | 19.0000 0.3889 0.2600 0.0000 341 | 20.0000 0.4427 0.2820 0.0000 342 | 21.0000 0.4966 0.3050 0.0000 343 | 22.0000 0.5506 0.3290 0.0000 344 | 23.0000 0.6045 0.3540 0.0000 345 | 24.0000 0.6585 0.3790 0.0000 346 | 25.0000 0.7125 0.4050 0.0000 347 | 26.0000 0.7666 0.4320 0.0000 348 | 27.0000 0.8222 0.4600 0.0000 349 | 30.0000 0.8550 0.5700 0.0000 350 | 35.0000 0.9800 0.7450 0.0000 351 | 40.0000 1.0350 0.9200 0.0000 352 | 45.0000 1.0500 1.0750 0.0000 353 | 50.0000 1.0200 1.2150 0.0000 354 | 55.0000 0.9550 1.3450 0.0000 355 | 60.0000 0.8750 1.4700 0.0000 356 | 65.0000 0.7600 1.5750 0.0000 357 | 70.0000 0.6300 1.6650 0.0000 358 | 75.0000 0.5000 1.7350 0.0000 359 | 80.0000 0.3650 1.7800 0.0000 360 | 85.0000 0.2300 1.8000 0.0000 361 | 90.0000 0.0900 1.8000 0.0000 362 | 95.0000 -0.0500 1.7800 0.0000 363 | 100.0000 -0.1850 1.7500 0.0000 364 | 105.0000 -0.3200 1.7000 0.0000 365 | 110.0000 -0.4500 1.6350 0.0000 366 | 115.0000 -0.5750 1.5550 0.0000 367 | 120.0000 -0.6700 1.4650 0.0000 368 | 125.0000 -0.7600 1.3500 0.0000 369 | 130.0000 -0.8500 1.2250 0.0000 370 | 135.0000 -0.9300 1.0850 0.0000 371 | 140.0000 -0.9800 0.9250 0.0000 372 | 145.0000 -0.9000 0.7550 0.0000 373 | 150.0000 -0.7700 0.5750 0.0000 374 | 155.0000 -0.6700 0.4200 0.0000 375 | 160.0000 -0.6350 0.3200 0.0000 376 | 165.0000 -0.6800 0.2300 0.0000 377 | 170.0000 -0.8500 0.1400 0.0000 378 | 175.0000 -0.6600 0.0550 0.0000 379 | 180.0000 0.0000 0.0250 0.0000 380 | 381 | Reynolds Number: 8e4 382 | BV Dyn. Stall Model - Positive Stall AOA (deg): 5.0 383 | BV Dyn. Stall Model - Negative Stall AOA (deg): -5.0 384 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 385 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 0.88 386 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -0.88 387 | AOA (deg) CL CD Cm25 388 | -180.0000 0.0000 0.0250 0.0000 389 | -175.0000 0.6600 0.0550 0.0000 390 | -170.0000 0.8500 0.1400 0.0000 391 | -165.0000 0.6800 0.2300 0.0000 392 | -160.0000 0.6350 0.3200 0.0000 393 | -155.0000 0.6700 0.4200 0.0000 394 | -150.0000 0.7700 0.5750 0.0000 395 | -145.0000 0.9000 0.7550 0.0000 396 | -140.0000 0.9800 0.9250 0.0000 397 | -135.0000 0.9300 1.0850 0.0000 398 | -130.0000 0.8500 1.2250 0.0000 399 | -125.0000 0.7600 1.3500 0.0000 400 | -120.0000 0.6700 1.4650 0.0000 401 | -115.0000 0.5750 1.5550 0.0000 402 | -110.0000 0.4500 1.6350 0.0000 403 | -105.0000 0.3200 1.7000 0.0000 404 | -100.0000 0.1850 1.7500 0.0000 405 | -95.0000 0.0500 1.7800 0.0000 406 | -90.0000 -0.0900 1.8000 0.0000 407 | -85.0000 -0.2300 1.8000 0.0000 408 | -80.0000 -0.3650 1.7800 0.0000 409 | -75.0000 -0.5000 1.7350 0.0000 410 | -70.0000 -0.6300 1.6650 0.0000 411 | -65.0000 -0.7600 1.5750 0.0000 412 | -60.0000 -0.8750 1.4700 0.0000 413 | -55.0000 -0.9550 1.3450 0.0000 414 | -50.0000 -1.0200 1.2150 0.0000 415 | -45.0000 -1.0500 1.0750 0.0000 416 | -40.0000 -1.0350 0.9200 0.0000 417 | -35.0000 -0.9800 0.7450 0.0000 418 | -30.0000 -0.8550 0.5700 0.0000 419 | -27.0000 -0.8277 0.4600 0.0000 420 | -26.0000 -0.7700 0.4320 0.0000 421 | -25.0000 -0.7156 0.4050 0.0000 422 | -24.0000 -0.6617 0.3790 0.0000 423 | -23.0000 -0.6078 0.3540 0.0000 424 | -22.0000 -0.5539 0.3290 0.0000 425 | -21.0000 -0.5001 0.3050 0.0000 426 | -20.0000 -0.4463 0.2820 0.0000 427 | -19.0000 -0.3927 0.2600 0.0000 428 | -18.0000 -0.3393 0.2380 0.0000 429 | -17.0000 -0.2873 0.2170 0.0000 430 | -16.0000 -0.2364 0.1960 0.0000 431 | -15.0000 -0.1861 0.1770 0.0000 432 | -14.0000 -0.1382 0.1580 0.0000 433 | -13.0000 -0.0967 0.1400 0.0000 434 | -12.0000 -0.0749 0.1230 0.0000 435 | -11.0000 -0.1642 0.0760 0.0000 436 | -10.0000 -0.5122 0.0277 0.0000 437 | -9.0000 -0.6969 0.0255 0.0000 438 | -8.0000 -0.7189 0.0234 0.0000 439 | -7.0000 -0.6760 0.0214 0.0000 440 | -6.0000 -0.6048 0.0197 0.0000 441 | -5.0000 -0.5180 0.0181 0.0000 442 | -4.0000 -0.4186 0.0168 0.0000 443 | -3.0000 -0.3300 0.0156 0.0000 444 | -2.0000 -0.2200 0.0151 0.0000 445 | -1.0000 -0.1100 0.0148 0.0000 446 | 0.0000 0.0000 0.0147 0.0000 447 | 1.0000 0.1100 0.0148 0.0000 448 | 2.0000 0.2200 0.0151 0.0000 449 | 3.0000 0.3300 0.0156 0.0000 450 | 4.0000 0.4186 0.0168 0.0000 451 | 5.0000 0.5180 0.0181 0.0000 452 | 6.0000 0.6048 0.0197 0.0000 453 | 7.0000 0.6760 0.0214 0.0000 454 | 8.0000 0.7189 0.0234 0.0000 455 | 9.0000 0.6969 0.0255 0.0000 456 | 10.0000 0.5122 0.0277 0.0000 457 | 11.0000 0.1642 0.0760 0.0000 458 | 12.0000 0.0749 0.1230 0.0000 459 | 13.0000 0.0967 0.1400 0.0000 460 | 14.0000 0.1382 0.1580 0.0000 461 | 15.0000 0.1861 0.1770 0.0000 462 | 16.0000 0.2364 0.1960 0.0000 463 | 17.0000 0.2873 0.2170 0.0000 464 | 18.0000 0.3393 0.2380 0.0000 465 | 19.0000 0.3927 0.2600 0.0000 466 | 20.0000 0.4463 0.2820 0.0000 467 | 21.0000 0.5001 0.3050 0.0000 468 | 22.0000 0.5539 0.3290 0.0000 469 | 23.0000 0.6078 0.3540 0.0000 470 | 24.0000 0.6617 0.3790 0.0000 471 | 25.0000 0.7156 0.4050 0.0000 472 | 26.0000 0.7700 0.4320 0.0000 473 | 27.0000 0.8277 0.4600 0.0000 474 | 30.0000 0.8550 0.5700 0.0000 475 | 35.0000 0.9800 0.7450 0.0000 476 | 40.0000 1.0350 0.9200 0.0000 477 | 45.0000 1.0500 1.0750 0.0000 478 | 50.0000 1.0200 1.2150 0.0000 479 | 55.0000 0.9550 1.3450 0.0000 480 | 60.0000 0.8750 1.4700 0.0000 481 | 65.0000 0.7600 1.5750 0.0000 482 | 70.0000 0.6300 1.6650 0.0000 483 | 75.0000 0.5000 1.7350 0.0000 484 | 80.0000 0.3650 1.7800 0.0000 485 | 85.0000 0.2300 1.8000 0.0000 486 | 90.0000 0.0900 1.8000 0.0000 487 | 95.0000 -0.0500 1.7800 0.0000 488 | 100.0000 -0.1850 1.7500 0.0000 489 | 105.0000 -0.3200 1.7000 0.0000 490 | 110.0000 -0.4500 1.6350 0.0000 491 | 115.0000 -0.5750 1.5550 0.0000 492 | 120.0000 -0.6700 1.4650 0.0000 493 | 125.0000 -0.7600 1.3500 0.0000 494 | 130.0000 -0.8500 1.2250 0.0000 495 | 135.0000 -0.9300 1.0850 0.0000 496 | 140.0000 -0.9800 0.9250 0.0000 497 | 145.0000 -0.9000 0.7550 0.0000 498 | 150.0000 -0.7700 0.5750 0.0000 499 | 155.0000 -0.6700 0.4200 0.0000 500 | 160.0000 -0.6350 0.3200 0.0000 501 | 165.0000 -0.6800 0.2300 0.0000 502 | 170.0000 -0.8500 0.1400 0.0000 503 | 175.0000 -0.6600 0.0550 0.0000 504 | 180.0000 0.0000 0.0250 0.0000 505 | 506 | Reynolds Number: 1.6e5 507 | BV Dyn. Stall Model - Positive Stall AOA (deg): 5.0 508 | BV Dyn. Stall Model - Negative Stall AOA (deg): -5.0 509 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 510 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 0.99 511 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -0.99 512 | AOA (deg) CL CD Cm25 513 | -180.0000 0.0000 0.0250 0.0000 514 | -175.0000 0.6600 0.0550 0.0000 515 | -170.0000 0.8500 0.1400 0.0000 516 | -165.0000 0.6800 0.2300 0.0000 517 | -160.0000 0.6350 0.3200 0.0000 518 | -155.0000 0.6700 0.4200 0.0000 519 | -150.0000 0.7700 0.5750 0.0000 520 | -145.0000 0.9000 0.7550 0.0000 521 | -140.0000 0.9800 0.9250 0.0000 522 | -135.0000 0.9300 1.0850 0.0000 523 | -130.0000 0.8500 1.2250 0.0000 524 | -125.0000 0.7600 1.3500 0.0000 525 | -120.0000 0.6700 1.4650 0.0000 526 | -115.0000 0.5750 1.5550 0.0000 527 | -110.0000 0.4500 1.6350 0.0000 528 | -105.0000 0.3200 1.7000 0.0000 529 | -100.0000 0.1850 1.7500 0.0000 530 | -95.0000 0.0500 1.7800 0.0000 531 | -90.0000 -0.0900 1.8000 0.0000 532 | -85.0000 -0.2300 1.8000 0.0000 533 | -80.0000 -0.3650 1.7800 0.0000 534 | -75.0000 -0.5000 1.7350 0.0000 535 | -70.0000 -0.6300 1.6650 0.0000 536 | -65.0000 -0.7600 1.5750 0.0000 537 | -60.0000 -0.8750 1.4700 0.0000 538 | -55.0000 -0.9550 1.3450 0.0000 539 | -50.0000 -1.0200 1.2150 0.0000 540 | -45.0000 -1.0500 1.0750 0.0000 541 | -40.0000 -1.0350 0.9200 0.0000 542 | -35.0000 -0.9800 0.7450 0.0000 543 | -30.0000 -0.8550 0.5700 0.0000 544 | -27.0000 -0.8382 0.4600 0.0000 545 | -26.0000 -0.7771 0.4320 0.0000 546 | -25.0000 -0.7224 0.4050 0.0000 547 | -24.0000 -0.6685 0.3790 0.0000 548 | -23.0000 -0.6148 0.3540 0.0000 549 | -22.0000 -0.5611 0.3290 0.0000 550 | -21.0000 -0.5087 0.3050 0.0000 551 | -20.0000 -0.4575 0.2820 0.0000 552 | -19.0000 -0.4066 0.2600 0.0000 553 | -18.0000 -0.3567 0.2380 0.0000 554 | -17.0000 -0.3098 0.2170 0.0000 555 | -16.0000 -0.2665 0.1970 0.0000 556 | -15.0000 -0.2376 0.1770 0.0000 557 | -14.0000 -0.2371 0.1040 0.0000 558 | -13.0000 -0.3548 0.0302 0.0000 559 | -12.0000 -0.5936 0.0281 0.0000 560 | -11.0000 -0.7623 0.0256 0.0000 561 | -10.0000 -0.8322 0.0233 0.0000 562 | -9.0000 -0.8311 0.0212 0.0000 563 | -8.0000 -0.7851 0.0193 0.0000 564 | -7.0000 -0.7150 0.0176 0.0000 565 | -6.0000 -0.6299 0.0160 0.0000 566 | -5.0000 -0.5500 0.0142 0.0000 567 | -4.0000 -0.4400 0.0132 0.0000 568 | -3.0000 -0.3300 0.0124 0.0000 569 | -2.0000 -0.2200 0.0120 0.0000 570 | -1.0000 -0.1100 0.0117 0.0000 571 | 0.0000 0.0000 0.0116 0.0000 572 | 1.0000 0.1100 0.0117 0.0000 573 | 2.0000 0.2200 0.0120 0.0000 574 | 3.0000 0.3300 0.0124 0.0000 575 | 4.0000 0.4400 0.0132 0.0000 576 | 5.0000 0.5500 0.0142 0.0000 577 | 6.0000 0.6299 0.0160 0.0000 578 | 7.0000 0.7150 0.0176 0.0000 579 | 8.0000 0.7851 0.0193 0.0000 580 | 9.0000 0.8311 0.0212 0.0000 581 | 10.0000 0.8322 0.0233 0.0000 582 | 11.0000 0.7623 0.0256 0.0000 583 | 12.0000 0.5936 0.0281 0.0000 584 | 13.0000 0.3548 0.0302 0.0000 585 | 14.0000 0.2371 0.1040 0.0000 586 | 15.0000 0.2376 0.1770 0.0000 587 | 16.0000 0.2665 0.1970 0.0000 588 | 17.0000 0.3098 0.2170 0.0000 589 | 18.0000 0.3567 0.2380 0.0000 590 | 19.0000 0.4066 0.2600 0.0000 591 | 20.0000 0.4575 0.2820 0.0000 592 | 21.0000 0.5087 0.3050 0.0000 593 | 22.0000 0.5611 0.3290 0.0000 594 | 23.0000 0.6148 0.3540 0.0000 595 | 24.0000 0.6685 0.3790 0.0000 596 | 25.0000 0.7224 0.4050 0.0000 597 | 26.0000 0.7771 0.4320 0.0000 598 | 27.0000 0.8382 0.4600 0.0000 599 | 30.0000 0.8550 0.5700 0.0000 600 | 35.0000 0.9800 0.7450 0.0000 601 | 40.0000 1.0350 0.9200 0.0000 602 | 45.0000 1.0500 1.0750 0.0000 603 | 50.0000 1.0200 1.2150 0.0000 604 | 55.0000 0.9550 1.3450 0.0000 605 | 60.0000 0.8750 1.4700 0.0000 606 | 65.0000 0.7600 1.5750 0.0000 607 | 70.0000 0.6300 1.6650 0.0000 608 | 75.0000 0.5000 1.7350 0.0000 609 | 80.0000 0.3650 1.7800 0.0000 610 | 85.0000 0.2300 1.8000 0.0000 611 | 90.0000 0.0900 1.8000 0.0000 612 | 95.0000 -0.0500 1.7800 0.0000 613 | 100.0000 -0.1850 1.7500 0.0000 614 | 105.0000 -0.3200 1.7000 0.0000 615 | 110.0000 -0.4500 1.6350 0.0000 616 | 115.0000 -0.5750 1.5550 0.0000 617 | 120.0000 -0.6700 1.4650 0.0000 618 | 125.0000 -0.7600 1.3500 0.0000 619 | 130.0000 -0.8500 1.2250 0.0000 620 | 135.0000 -0.9300 1.0850 0.0000 621 | 140.0000 -0.9800 0.9250 0.0000 622 | 145.0000 -0.9000 0.7550 0.0000 623 | 150.0000 -0.7700 0.5750 0.0000 624 | 155.0000 -0.6700 0.4200 0.0000 625 | 160.0000 -0.6350 0.3200 0.0000 626 | 165.0000 -0.6800 0.2300 0.0000 627 | 170.0000 -0.8500 0.1400 0.0000 628 | 175.0000 -0.6600 0.0550 0.0000 629 | 180.0000 0.0000 0.0250 0.0000 630 | 631 | Reynolds Number: 3.6e5 632 | BV Dyn. Stall Model - Positive Stall AOA (deg): 6.0 633 | BV Dyn. Stall Model - Negative Stall AOA (deg): -6.0 634 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 635 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.21 636 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.21 637 | AOA (deg) CL CD Cm25 638 | -180.0000 0.0000 0.0250 0.0000 639 | -175.0000 0.6600 0.0550 0.0000 640 | -170.0000 0.8500 0.1400 0.0000 641 | -165.0000 0.6800 0.2300 0.0000 642 | -160.0000 0.6350 0.3200 0.0000 643 | -155.0000 0.6700 0.4200 0.0000 644 | -150.0000 0.7700 0.5750 0.0000 645 | -145.0000 0.9000 0.7550 0.0000 646 | -140.0000 0.9800 0.9250 0.0000 647 | -135.0000 0.9300 1.0850 0.0000 648 | -130.0000 0.8500 1.2250 0.0000 649 | -125.0000 0.7600 1.3500 0.0000 650 | -120.0000 0.6700 1.4650 0.0000 651 | -115.0000 0.5750 1.5550 0.0000 652 | -110.0000 0.4500 1.6350 0.0000 653 | -105.0000 0.3200 1.7000 0.0000 654 | -100.0000 0.1850 1.7500 0.0000 655 | -95.0000 0.0500 1.7800 0.0000 656 | -90.0000 -0.0900 1.8000 0.0000 657 | -85.0000 -0.2300 1.8000 0.0000 658 | -80.0000 -0.3650 1.7800 0.0000 659 | -75.0000 -0.5000 1.7350 0.0000 660 | -70.0000 -0.6300 1.6650 0.0000 661 | -65.0000 -0.7600 1.5750 0.0000 662 | -60.0000 -0.8750 1.4700 0.0000 663 | -55.0000 -0.9550 1.3450 0.0000 664 | -50.0000 -1.0200 1.2150 0.0000 665 | -45.0000 -1.0500 1.0750 0.0000 666 | -40.0000 -1.0350 0.9200 0.0000 667 | -35.0000 -0.9800 0.7450 0.0000 668 | -30.0000 -0.8550 0.5700 0.0000 669 | -27.0000 -0.8788 0.4600 0.0000 670 | -26.0000 -0.8055 0.4320 0.0000 671 | -25.0000 -0.7511 0.4050 0.0000 672 | -24.0000 -0.7015 0.3790 0.0000 673 | -23.0000 -0.6528 0.3540 0.0000 674 | -22.0000 -0.6045 0.3290 0.0000 675 | -21.0000 -0.5616 0.3050 0.0000 676 | -20.0000 -0.5247 0.2820 0.0000 677 | -19.0000 -0.4908 0.2600 0.0000 678 | -18.0000 -0.4782 0.2380 0.0000 679 | -17.0000 -0.4851 0.2170 0.0000 680 | -16.0000 -0.5384 0.1240 0.0000 681 | -15.0000 -0.6350 0.0312 0.0000 682 | -14.0000 -0.7483 0.0283 0.0000 683 | -13.0000 -0.8562 0.0257 0.0000 684 | -12.0000 -0.9285 0.0233 0.0000 685 | -11.0000 -0.9572 0.0211 0.0000 686 | -10.0000 -0.9440 0.0191 0.0000 687 | -9.0000 -0.8946 0.0173 0.0000 688 | -8.0000 -0.8240 0.0157 0.0000 689 | -7.0000 -0.7390 0.0143 0.0000 690 | -6.0000 -0.6600 0.0126 0.0000 691 | -5.0000 -0.5500 0.0114 0.0000 692 | -4.0000 -0.4400 0.0105 0.0000 693 | -3.0000 -0.3300 0.0098 0.0000 694 | -2.0000 -0.2200 0.0094 0.0000 695 | -1.0000 -0.1100 0.0092 0.0000 696 | 0.0000 0.0000 0.0091 0.0000 697 | 1.0000 0.1100 0.0092 0.0000 698 | 2.0000 0.2200 0.0094 0.0000 699 | 3.0000 0.3300 0.0098 0.0000 700 | 4.0000 0.4400 0.0105 0.0000 701 | 5.0000 0.5500 0.0114 0.0000 702 | 6.0000 0.6600 0.0126 0.0000 703 | 7.0000 0.7390 0.0143 0.0000 704 | 8.0000 0.8240 0.0157 0.0000 705 | 9.0000 0.8946 0.0173 0.0000 706 | 10.0000 0.9440 0.0191 0.0000 707 | 11.0000 0.9572 0.0211 0.0000 708 | 12.0000 0.9285 0.0233 0.0000 709 | 13.0000 0.8562 0.0257 0.0000 710 | 14.0000 0.7483 0.0283 0.0000 711 | 15.0000 0.6350 0.0312 0.0000 712 | 16.0000 0.5384 0.1240 0.0000 713 | 17.0000 0.4851 0.2170 0.0000 714 | 18.0000 0.4782 0.2380 0.0000 715 | 19.0000 0.4908 0.2600 0.0000 716 | 20.0000 0.5247 0.2820 0.0000 717 | 21.0000 0.5616 0.3050 0.0000 718 | 22.0000 0.6045 0.3290 0.0000 719 | 23.0000 0.6528 0.3540 0.0000 720 | 24.0000 0.7015 0.3790 0.0000 721 | 25.0000 0.7511 0.4050 0.0000 722 | 26.0000 0.8055 0.4320 0.0000 723 | 27.0000 0.8788 0.4600 0.0000 724 | 30.0000 0.8550 0.5700 0.0000 725 | 35.0000 0.9800 0.7450 0.0000 726 | 40.0000 1.0350 0.9200 0.0000 727 | 45.0000 1.0500 1.0750 0.0000 728 | 50.0000 1.0200 1.2150 0.0000 729 | 55.0000 0.9550 1.3450 0.0000 730 | 60.0000 0.8750 1.4700 0.0000 731 | 65.0000 0.7600 1.5750 0.0000 732 | 70.0000 0.6300 1.6650 0.0000 733 | 75.0000 0.5000 1.7350 0.0000 734 | 80.0000 0.3650 1.7800 0.0000 735 | 85.0000 0.2300 1.8000 0.0000 736 | 90.0000 0.0900 1.8000 0.0000 737 | 95.0000 -0.0500 1.7800 0.0000 738 | 100.0000 -0.1850 1.7500 0.0000 739 | 105.0000 -0.3200 1.7000 0.0000 740 | 110.0000 -0.4500 1.6350 0.0000 741 | 115.0000 -0.5750 1.5550 0.0000 742 | 120.0000 -0.6700 1.4650 0.0000 743 | 125.0000 -0.7600 1.3500 0.0000 744 | 130.0000 -0.8500 1.2250 0.0000 745 | 135.0000 -0.9300 1.0850 0.0000 746 | 140.0000 -0.9800 0.9250 0.0000 747 | 145.0000 -0.9000 0.7550 0.0000 748 | 150.0000 -0.7700 0.5750 0.0000 749 | 155.0000 -0.6700 0.4200 0.0000 750 | 160.0000 -0.6350 0.3200 0.0000 751 | 165.0000 -0.6800 0.2300 0.0000 752 | 170.0000 -0.8500 0.1400 0.0000 753 | 175.0000 -0.6600 0.0550 0.0000 754 | 180.0000 0.0000 0.0250 0.0000 755 | 756 | Reynolds Number: 7e5 757 | BV Dyn. Stall Model - Positive Stall AOA (deg): 6.0 758 | BV Dyn. Stall Model - Negative Stall AOA (deg): -6.0 759 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 760 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.32 761 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.32 762 | AOA (deg) CL CD Cm25 763 | -180.0000 0.0000 0.0250 0.0000 764 | -175.0000 0.6600 0.0550 0.0000 765 | -170.0000 0.8500 0.1400 0.0000 766 | -165.0000 0.6800 0.2300 0.0000 767 | -160.0000 0.6350 0.3200 0.0000 768 | -155.0000 0.6700 0.4200 0.0000 769 | -150.0000 0.7700 0.5750 0.0000 770 | -145.0000 0.9000 0.7550 0.0000 771 | -140.0000 0.9800 0.9250 0.0000 772 | -135.0000 0.9300 1.0850 0.0000 773 | -130.0000 0.8500 1.2250 0.0000 774 | -125.0000 0.7600 1.3500 0.0000 775 | -120.0000 0.6700 1.4650 0.0000 776 | -115.0000 0.5750 1.5550 0.0000 777 | -110.0000 0.4500 1.6350 0.0000 778 | -105.0000 0.3200 1.7000 0.0000 779 | -100.0000 0.1850 1.7500 0.0000 780 | -95.0000 0.0500 1.7800 0.0000 781 | -90.0000 -0.0900 1.8000 0.0000 782 | -85.0000 -0.2300 1.8000 0.0000 783 | -80.0000 -0.3650 1.7800 0.0000 784 | -75.0000 -0.5000 1.7350 0.0000 785 | -70.0000 -0.6300 1.6650 0.0000 786 | -65.0000 -0.7600 1.5750 0.0000 787 | -60.0000 -0.8750 1.4700 0.0000 788 | -55.0000 -0.9550 1.3450 0.0000 789 | -50.0000 -1.0200 1.2150 0.0000 790 | -45.0000 -1.0500 1.0750 0.0000 791 | -40.0000 -1.0350 0.9200 0.0000 792 | -35.0000 -0.9800 0.7450 0.0000 793 | -30.0000 -0.8550 0.5700 0.0000 794 | -27.0000 -0.9473 0.4600 0.0000 795 | -26.0000 -0.8838 0.4320 0.0000 796 | -25.0000 -0.8353 0.4050 0.0000 797 | -24.0000 -0.7961 0.3790 0.0000 798 | -23.0000 -0.7593 0.3540 0.0000 799 | -22.0000 -0.7298 0.3290 0.0000 800 | -21.0000 -0.7097 0.3050 0.0000 801 | -20.0000 -0.6990 0.2820 0.0000 802 | -19.0000 -0.7041 0.2600 0.0000 803 | -18.0000 -0.7305 0.2380 0.0000 804 | -17.0000 -0.7799 0.1340 0.0000 805 | -16.0000 -0.8401 0.0297 0.0000 806 | -15.0000 -0.9119 0.0269 0.0000 807 | -14.0000 -0.9801 0.0244 0.0000 808 | -13.0000 -1.0302 0.0221 0.0000 809 | -12.0000 -1.0508 0.0200 0.0000 810 | -11.0000 -1.0363 0.0182 0.0000 811 | -10.0000 -0.9937 0.0164 0.0000 812 | -9.0000 -0.9260 0.0149 0.0000 813 | -8.0000 -0.8442 0.0135 0.0000 814 | -7.0000 -0.7483 0.0122 0.0000 815 | -6.0000 -0.6600 0.0108 0.0000 816 | -5.0000 -0.5500 0.0098 0.0000 817 | -4.0000 -0.4400 0.0089 0.0000 818 | -3.0000 -0.3300 0.0083 0.0000 819 | -2.0000 -0.2200 0.0080 0.0000 820 | -1.0000 -0.1100 0.0078 0.0000 821 | 0.0000 0.0000 0.0077 0.0000 822 | 1.0000 0.1100 0.0078 0.0000 823 | 2.0000 0.2200 0.0080 0.0000 824 | 3.0000 0.3300 0.0083 0.0000 825 | 4.0000 0.4400 0.0089 0.0000 826 | 5.0000 0.5500 0.0098 0.0000 827 | 6.0000 0.6600 0.0108 0.0000 828 | 7.0000 0.7483 0.0122 0.0000 829 | 8.0000 0.8442 0.0135 0.0000 830 | 9.0000 0.9260 0.0149 0.0000 831 | 10.0000 0.9937 0.0164 0.0000 832 | 11.0000 1.0363 0.0182 0.0000 833 | 12.0000 1.0508 0.0200 0.0000 834 | 13.0000 1.0302 0.0221 0.0000 835 | 14.0000 0.9801 0.0244 0.0000 836 | 15.0000 0.9119 0.0269 0.0000 837 | 16.0000 0.8401 0.0297 0.0000 838 | 17.0000 0.7799 0.1340 0.0000 839 | 18.0000 0.7305 0.2380 0.0000 840 | 19.0000 0.7041 0.2600 0.0000 841 | 20.0000 0.6990 0.2820 0.0000 842 | 21.0000 0.7097 0.3050 0.0000 843 | 22.0000 0.7298 0.3290 0.0000 844 | 23.0000 0.7593 0.3540 0.0000 845 | 24.0000 0.7961 0.3790 0.0000 846 | 25.0000 0.8353 0.4050 0.0000 847 | 26.0000 0.8838 0.4320 0.0000 848 | 27.0000 0.9473 0.4600 0.0000 849 | 30.0000 0.8550 0.5700 0.0000 850 | 35.0000 0.9800 0.7450 0.0000 851 | 40.0000 1.0350 0.9200 0.0000 852 | 45.0000 1.0500 1.0750 0.0000 853 | 50.0000 1.0200 1.2150 0.0000 854 | 55.0000 0.9550 1.3450 0.0000 855 | 60.0000 0.8750 1.4700 0.0000 856 | 65.0000 0.7600 1.5750 0.0000 857 | 70.0000 0.6300 1.6650 0.0000 858 | 75.0000 0.5000 1.7350 0.0000 859 | 80.0000 0.3650 1.7800 0.0000 860 | 85.0000 0.2300 1.8000 0.0000 861 | 90.0000 0.0900 1.8000 0.0000 862 | 95.0000 -0.0500 1.7800 0.0000 863 | 100.0000 -0.1850 1.7500 0.0000 864 | 105.0000 -0.3200 1.7000 0.0000 865 | 110.0000 -0.4500 1.6350 0.0000 866 | 115.0000 -0.5750 1.5550 0.0000 867 | 120.0000 -0.6700 1.4650 0.0000 868 | 125.0000 -0.7600 1.3500 0.0000 869 | 130.0000 -0.8500 1.2250 0.0000 870 | 135.0000 -0.9300 1.0850 0.0000 871 | 140.0000 -0.9800 0.9250 0.0000 872 | 145.0000 -0.9000 0.7550 0.0000 873 | 150.0000 -0.7700 0.5750 0.0000 874 | 155.0000 -0.6700 0.4200 0.0000 875 | 160.0000 -0.6350 0.3200 0.0000 876 | 165.0000 -0.6800 0.2300 0.0000 877 | 170.0000 -0.8500 0.1400 0.0000 878 | 175.0000 -0.6600 0.0550 0.0000 879 | 180.0000 0.0000 0.0250 0.0000 880 | 881 | Reynolds Number: 1e6 882 | BV Dyn. Stall Model - Positive Stall AOA (deg): 7.0 883 | BV Dyn. Stall Model - Negative Stall AOA (deg): -7.0 884 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 885 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.32 886 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.32 887 | AOA (deg) CL CD Cm25 888 | -180.0000 0.0000 0.0250 0.0000 889 | -175.0000 0.6600 0.0550 0.0000 890 | -170.0000 0.8500 0.1400 0.0000 891 | -165.0000 0.6800 0.2300 0.0000 892 | -160.0000 0.6350 0.3200 0.0000 893 | -155.0000 0.6700 0.4200 0.0000 894 | -150.0000 0.7700 0.5750 0.0000 895 | -145.0000 0.9000 0.7550 0.0000 896 | -140.0000 0.9800 0.9250 0.0000 897 | -135.0000 0.9300 1.0850 0.0000 898 | -130.0000 0.8500 1.2250 0.0000 899 | -125.0000 0.7600 1.3500 0.0000 900 | -120.0000 0.6700 1.4650 0.0000 901 | -115.0000 0.5750 1.5550 0.0000 902 | -110.0000 0.4500 1.6350 0.0000 903 | -105.0000 0.3200 1.7000 0.0000 904 | -100.0000 0.1850 1.7500 0.0000 905 | -95.0000 0.0500 1.7800 0.0000 906 | -90.0000 -0.0900 1.8000 0.0000 907 | -85.0000 -0.2300 1.8000 0.0000 908 | -80.0000 -0.3650 1.7800 0.0000 909 | -75.0000 -0.5000 1.7350 0.0000 910 | -70.0000 -0.6300 1.6650 0.0000 911 | -65.0000 -0.7600 1.5750 0.0000 912 | -60.0000 -0.8750 1.4700 0.0000 913 | -55.0000 -0.9550 1.3450 0.0000 914 | -50.0000 -1.0200 1.2150 0.0000 915 | -45.0000 -1.0500 1.0750 0.0000 916 | -40.0000 -1.0350 0.9200 0.0000 917 | -35.0000 -0.9800 0.7450 0.0000 918 | -30.0000 -0.8550 0.5700 0.0000 919 | -27.0000 -0.9912 0.4600 0.0000 920 | -26.0000 -0.9406 0.4320 0.0000 921 | -25.0000 -0.9023 0.4050 0.0000 922 | -24.0000 -0.8668 0.3790 0.0000 923 | -23.0000 -0.8408 0.3540 0.0000 924 | -22.0000 -0.8189 0.3290 0.0000 925 | -21.0000 -0.8063 0.3050 0.0000 926 | -20.0000 -0.8089 0.2820 0.0000 927 | -19.0000 -0.8226 0.2600 0.0000 928 | -18.0000 -0.8566 0.1450 0.0000 929 | -17.0000 -0.8996 0.0303 0.0000 930 | -16.0000 -0.9567 0.0275 0.0000 931 | -15.0000 -1.0145 0.0249 0.0000 932 | -14.0000 -1.0656 0.0225 0.0000 933 | -13.0000 -1.0957 0.0205 0.0000 934 | -12.0000 -1.0971 0.0186 0.0000 935 | -11.0000 -1.0686 0.0168 0.0000 936 | -10.0000 -1.0141 0.0152 0.0000 937 | -9.0000 -0.9387 0.0138 0.0000 938 | -8.0000 -0.8504 0.0126 0.0000 939 | -7.0000 -0.7700 0.0111 0.0000 940 | -6.0000 -0.6600 0.0101 0.0000 941 | -5.0000 -0.5500 0.0091 0.0000 942 | -4.0000 -0.4400 0.0083 0.0000 943 | -3.0000 -0.3300 0.0079 0.0000 944 | -2.0000 -0.2200 0.0076 0.0000 945 | -1.0000 -0.1100 0.0075 0.0000 946 | 0.0000 0.0000 0.0074 0.0000 947 | 1.0000 0.1100 0.0075 0.0000 948 | 2.0000 0.2200 0.0076 0.0000 949 | 3.0000 0.3300 0.0079 0.0000 950 | 4.0000 0.4400 0.0083 0.0000 951 | 5.0000 0.5500 0.0091 0.0000 952 | 6.0000 0.6600 0.0101 0.0000 953 | 7.0000 0.7700 0.0111 0.0000 954 | 8.0000 0.8504 0.0126 0.0000 955 | 9.0000 0.9387 0.0138 0.0000 956 | 10.0000 1.0141 0.0152 0.0000 957 | 11.0000 1.0686 0.0168 0.0000 958 | 12.0000 1.0971 0.0186 0.0000 959 | 13.0000 1.0957 0.0205 0.0000 960 | 14.0000 1.0656 0.0225 0.0000 961 | 15.0000 1.0145 0.0249 0.0000 962 | 16.0000 0.9567 0.0275 0.0000 963 | 17.0000 0.8996 0.0303 0.0000 964 | 18.0000 0.8566 0.1450 0.0000 965 | 19.0000 0.8226 0.2600 0.0000 966 | 20.0000 0.8089 0.2820 0.0000 967 | 21.0000 0.8063 0.3050 0.0000 968 | 22.0000 0.8189 0.3290 0.0000 969 | 23.0000 0.8408 0.3540 0.0000 970 | 24.0000 0.8668 0.3790 0.0000 971 | 25.0000 0.9023 0.4050 0.0000 972 | 26.0000 0.9406 0.4320 0.0000 973 | 27.0000 0.9912 0.4600 0.0000 974 | 30.0000 0.8550 0.5700 0.0000 975 | 35.0000 0.9800 0.7450 0.0000 976 | 40.0000 1.0350 0.9200 0.0000 977 | 45.0000 1.0500 1.0750 0.0000 978 | 50.0000 1.0200 1.2150 0.0000 979 | 55.0000 0.9550 1.3450 0.0000 980 | 60.0000 0.8750 1.4700 0.0000 981 | 65.0000 0.7600 1.5750 0.0000 982 | 70.0000 0.6300 1.6650 0.0000 983 | 75.0000 0.5000 1.7350 0.0000 984 | 80.0000 0.3650 1.7800 0.0000 985 | 85.0000 0.2300 1.8000 0.0000 986 | 90.0000 0.0900 1.8000 0.0000 987 | 95.0000 -0.0500 1.7800 0.0000 988 | 100.0000 -0.1850 1.7500 0.0000 989 | 105.0000 -0.3200 1.7000 0.0000 990 | 110.0000 -0.4500 1.6350 0.0000 991 | 115.0000 -0.5750 1.5550 0.0000 992 | 120.0000 -0.6700 1.4650 0.0000 993 | 125.0000 -0.7600 1.3500 0.0000 994 | 130.0000 -0.8500 1.2250 0.0000 995 | 135.0000 -0.9300 1.0850 0.0000 996 | 140.0000 -0.9800 0.9250 0.0000 997 | 145.0000 -0.9000 0.7550 0.0000 998 | 150.0000 -0.7700 0.5750 0.0000 999 | 155.0000 -0.6700 0.4200 0.0000 1000 | 160.0000 -0.6350 0.3200 0.0000 1001 | 165.0000 -0.6800 0.2300 0.0000 1002 | 170.0000 -0.8500 0.1400 0.0000 1003 | 175.0000 -0.6600 0.0550 0.0000 1004 | 180.0000 0.0000 0.0250 0.0000 1005 | 1006 | Reynolds Number: 2e6 1007 | BV Dyn. Stall Model - Positive Stall AOA (deg): 8.0 1008 | BV Dyn. Stall Model - Negative Stall AOA (deg): -8.0 1009 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 1010 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.43 1011 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.43 1012 | AOA (deg) CL CD Cm25 1013 | -180.0000 0.0000 0.0250 0.0000 1014 | -175.0000 0.6600 0.0550 0.0000 1015 | -170.0000 0.8500 0.1400 0.0000 1016 | -165.0000 0.6800 0.2300 0.0000 1017 | -160.0000 0.6350 0.3200 0.0000 1018 | -155.0000 0.6700 0.4200 0.0000 1019 | -150.0000 0.7700 0.5750 0.0000 1020 | -145.0000 0.9000 0.7550 0.0000 1021 | -140.0000 0.9800 0.9250 0.0000 1022 | -135.0000 0.9300 1.0850 0.0000 1023 | -130.0000 0.8500 1.2250 0.0000 1024 | -125.0000 0.7600 1.3500 0.0000 1025 | -120.0000 0.6700 1.4650 0.0000 1026 | -115.0000 0.5750 1.5550 0.0000 1027 | -110.0000 0.4500 1.6350 0.0000 1028 | -105.0000 0.3200 1.7000 0.0000 1029 | -100.0000 0.1850 1.7500 0.0000 1030 | -95.0000 0.0500 1.7800 0.0000 1031 | -90.0000 -0.0900 1.8000 0.0000 1032 | -85.0000 -0.2300 1.8000 0.0000 1033 | -80.0000 -0.3650 1.7800 0.0000 1034 | -75.0000 -0.5000 1.7350 0.0000 1035 | -70.0000 -0.6300 1.6650 0.0000 1036 | -65.0000 -0.7600 1.5750 0.0000 1037 | -60.0000 -0.8750 1.4700 0.0000 1038 | -55.0000 -0.9550 1.3450 0.0000 1039 | -50.0000 -1.0200 1.2150 0.0000 1040 | -45.0000 -1.0500 1.0750 0.0000 1041 | -40.0000 -1.0350 0.9200 0.0000 1042 | -35.0000 -0.9800 0.7450 0.0000 1043 | -30.0000 -0.8550 0.5700 0.0000 1044 | -27.0000 -1.0810 0.4600 0.0000 1045 | -26.0000 -1.0591 0.4320 0.0000 1046 | -25.0000 -1.0317 0.4050 0.0000 1047 | -24.0000 -1.0078 0.3790 0.0000 1048 | -23.0000 -0.9910 0.3540 0.0000 1049 | -22.0000 -0.9827 0.3290 0.0000 1050 | -21.0000 -0.9837 0.3050 0.0000 1051 | -20.0000 -0.9954 0.2820 0.0000 1052 | -19.0000 -1.0173 0.1550 0.0000 1053 | -18.0000 -1.0510 0.0288 0.0000 1054 | -17.0000 -1.0921 0.0261 0.0000 1055 | -16.0000 -1.1356 0.0237 0.0000 1056 | -15.0000 -1.1744 0.0215 0.0000 1057 | -14.0000 -1.1962 0.0195 0.0000 1058 | -13.0000 -1.1948 0.0177 0.0000 1059 | -12.0000 -1.1667 0.0161 0.0000 1060 | -11.0000 -1.1138 0.0146 0.0000 1061 | -10.0000 -1.0433 0.0133 0.0000 1062 | -9.0000 -0.9574 0.0121 0.0000 1063 | -8.0000 -0.8800 0.0108 0.0000 1064 | -7.0000 -0.7700 0.0098 0.0000 1065 | -6.0000 -0.6600 0.0090 0.0000 1066 | -5.0000 -0.5500 0.0083 0.0000 1067 | -4.0000 -0.4400 0.0078 0.0000 1068 | -3.0000 -0.3300 0.0075 0.0000 1069 | -2.0000 -0.2200 0.0072 0.0000 1070 | -1.0000 -0.1100 0.0071 0.0000 1071 | 0.0000 0.0000 0.0070 0.0000 1072 | 1.0000 0.1100 0.0071 0.0000 1073 | 2.0000 0.2200 0.0072 0.0000 1074 | 3.0000 0.3300 0.0075 0.0000 1075 | 4.0000 0.4400 0.0078 0.0000 1076 | 5.0000 0.5500 0.0083 0.0000 1077 | 6.0000 0.6600 0.0090 0.0000 1078 | 7.0000 0.7700 0.0098 0.0000 1079 | 8.0000 0.8800 0.0108 0.0000 1080 | 9.0000 0.9574 0.0121 0.0000 1081 | 10.0000 1.0433 0.0133 0.0000 1082 | 11.0000 1.1138 0.0146 0.0000 1083 | 12.0000 1.1667 0.0161 0.0000 1084 | 13.0000 1.1948 0.0177 0.0000 1085 | 14.0000 1.1962 0.0195 0.0000 1086 | 15.0000 1.1744 0.0215 0.0000 1087 | 16.0000 1.1356 0.0237 0.0000 1088 | 17.0000 1.0921 0.0261 0.0000 1089 | 18.0000 1.0510 0.0288 0.0000 1090 | 19.0000 1.0173 0.1550 0.0000 1091 | 20.0000 0.9954 0.2820 0.0000 1092 | 21.0000 0.9837 0.3050 0.0000 1093 | 22.0000 0.9827 0.3290 0.0000 1094 | 23.0000 0.9910 0.3540 0.0000 1095 | 24.0000 1.0078 0.3790 0.0000 1096 | 25.0000 1.0317 0.4050 0.0000 1097 | 26.0000 1.0591 0.4320 0.0000 1098 | 27.0000 1.0810 0.4600 0.0000 1099 | 30.0000 0.8550 0.5700 0.0000 1100 | 35.0000 0.9800 0.7450 0.0000 1101 | 40.0000 1.0350 0.9200 0.0000 1102 | 45.0000 1.0500 1.0750 0.0000 1103 | 50.0000 1.0200 1.2150 0.0000 1104 | 55.0000 0.9550 1.3450 0.0000 1105 | 60.0000 0.8750 1.4700 0.0000 1106 | 65.0000 0.7600 1.5750 0.0000 1107 | 70.0000 0.6300 1.6650 0.0000 1108 | 75.0000 0.5000 1.7350 0.0000 1109 | 80.0000 0.3650 1.7800 0.0000 1110 | 85.0000 0.2300 1.8000 0.0000 1111 | 90.0000 0.0900 1.8000 0.0000 1112 | 95.0000 -0.0500 1.7800 0.0000 1113 | 100.0000 -0.1850 1.7500 0.0000 1114 | 105.0000 -0.3200 1.7000 0.0000 1115 | 110.0000 -0.4500 1.6350 0.0000 1116 | 115.0000 -0.5750 1.5550 0.0000 1117 | 120.0000 -0.6700 1.4650 0.0000 1118 | 125.0000 -0.7600 1.3500 0.0000 1119 | 130.0000 -0.8500 1.2250 0.0000 1120 | 135.0000 -0.9300 1.0850 0.0000 1121 | 140.0000 -0.9800 0.9250 0.0000 1122 | 145.0000 -0.9000 0.7550 0.0000 1123 | 150.0000 -0.7700 0.5750 0.0000 1124 | 155.0000 -0.6700 0.4200 0.0000 1125 | 160.0000 -0.6350 0.3200 0.0000 1126 | 165.0000 -0.6800 0.2300 0.0000 1127 | 170.0000 -0.8500 0.1400 0.0000 1128 | 175.0000 -0.6600 0.0550 0.0000 1129 | 180.0000 0.0000 0.0250 0.0000 1130 | 1131 | Reynolds Number: 5e6 1132 | BV Dyn. Stall Model - Positive Stall AOA (deg): 9.0 1133 | BV Dyn. Stall Model - Negative Stall AOA (deg): -9.0 1134 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 1135 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.65 1136 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.65 1137 | AOA (deg) CL CD Cm25 1138 | -180.0000 0.0000 0.0250 0.0000 1139 | -175.0000 0.6600 0.0550 0.0000 1140 | -170.0000 0.8500 0.1400 0.0000 1141 | -165.0000 0.6800 0.2300 0.0000 1142 | -160.0000 0.6350 0.3200 0.0000 1143 | -155.0000 0.6700 0.4200 0.0000 1144 | -150.0000 0.7700 0.5750 0.0000 1145 | -145.0000 0.9000 0.7550 0.0000 1146 | -140.0000 0.9800 0.9250 0.0000 1147 | -135.0000 0.9300 1.0850 0.0000 1148 | -130.0000 0.8500 1.2250 0.0000 1149 | -125.0000 0.7600 1.3500 0.0000 1150 | -120.0000 0.6700 1.4650 0.0000 1151 | -115.0000 0.5750 1.5550 0.0000 1152 | -110.0000 0.4500 1.6350 0.0000 1153 | -105.0000 0.3200 1.7000 0.0000 1154 | -100.0000 0.1850 1.7500 0.0000 1155 | -95.0000 0.0500 1.7800 0.0000 1156 | -90.0000 -0.0900 1.8000 0.0000 1157 | -85.0000 -0.2300 1.8000 0.0000 1158 | -80.0000 -0.3650 1.7800 0.0000 1159 | -75.0000 -0.5000 1.7350 0.0000 1160 | -70.0000 -0.6300 1.6650 0.0000 1161 | -65.0000 -0.7600 1.5750 0.0000 1162 | -60.0000 -0.8750 1.4700 0.0000 1163 | -55.0000 -0.9550 1.3450 0.0000 1164 | -50.0000 -1.0200 1.2150 0.0000 1165 | -45.0000 -1.0500 1.0750 0.0000 1166 | -40.0000 -1.0350 0.9200 0.0000 1167 | -35.0000 -0.9800 0.7450 0.0000 1168 | -30.0000 -0.8550 0.5700 0.0000 1169 | -27.0000 -1.1397 0.4600 0.0000 1170 | -26.0000 -1.1268 0.4320 0.0000 1171 | -25.0000 -1.1322 0.4050 0.0000 1172 | -24.0000 -1.1563 0.3790 0.0000 1173 | -23.0000 -1.1611 0.3540 0.0000 1174 | -22.0000 -1.1647 0.3290 0.0000 1175 | -21.0000 -1.1771 0.3050 0.0000 1176 | -20.0000 -1.1965 0.1660 0.0000 1177 | -19.0000 -1.2242 0.0265 0.0000 1178 | -18.0000 -1.2576 0.0240 0.0000 1179 | -17.0000 -1.2917 0.0218 0.0000 1180 | -16.0000 -1.3186 0.0198 0.0000 1181 | -15.0000 -1.3298 0.0180 0.0000 1182 | -14.0000 -1.3187 0.0164 0.0000 1183 | -13.0000 -1.2847 0.0149 0.0000 1184 | -12.0000 -1.2290 0.0136 0.0000 1185 | -11.0000 -1.1553 0.0124 0.0000 1186 | -10.0000 -1.0685 0.0113 0.0000 1187 | -9.0000 -0.9900 0.0102 0.0000 1188 | -8.0000 -0.8800 0.0095 0.0000 1189 | -7.0000 -0.7700 0.0089 0.0000 1190 | -6.0000 -0.6600 0.0084 0.0000 1191 | -5.0000 -0.5500 0.0080 0.0000 1192 | -4.0000 -0.4400 0.0075 0.0000 1193 | -3.0000 -0.3300 0.0073 0.0000 1194 | -2.0000 -0.2200 0.0070 0.0000 1195 | -1.0000 -0.1100 0.0069 0.0000 1196 | 0.0000 0.0000 0.0068 0.0000 1197 | 1.0000 0.1100 0.0069 0.0000 1198 | 2.0000 0.2200 0.0070 0.0000 1199 | 3.0000 0.3300 0.0073 0.0000 1200 | 4.0000 0.4400 0.0075 0.0000 1201 | 5.0000 0.5500 0.0080 0.0000 1202 | 6.0000 0.6600 0.0084 0.0000 1203 | 7.0000 0.7700 0.0089 0.0000 1204 | 8.0000 0.8800 0.0095 0.0000 1205 | 9.0000 0.9900 0.0102 0.0000 1206 | 10.0000 1.0685 0.0113 0.0000 1207 | 11.0000 1.1553 0.0124 0.0000 1208 | 12.0000 1.2290 0.0136 0.0000 1209 | 13.0000 1.2847 0.0149 0.0000 1210 | 14.0000 1.3187 0.0164 0.0000 1211 | 15.0000 1.3298 0.0180 0.0000 1212 | 16.0000 1.3186 0.0198 0.0000 1213 | 17.0000 1.2917 0.0218 0.0000 1214 | 18.0000 1.2576 0.0240 0.0000 1215 | 19.0000 1.2242 0.0265 0.0000 1216 | 20.0000 1.1965 0.1660 0.0000 1217 | 21.0000 1.1771 0.3050 0.0000 1218 | 22.0000 1.1647 0.3290 0.0000 1219 | 23.0000 1.1611 0.3540 0.0000 1220 | 24.0000 1.1563 0.3790 0.0000 1221 | 25.0000 1.1322 0.4050 0.0000 1222 | 26.0000 1.1268 0.4320 0.0000 1223 | 27.0000 1.1397 0.4600 0.0000 1224 | 30.0000 0.8550 0.5700 0.0000 1225 | 35.0000 0.9800 0.7450 0.0000 1226 | 40.0000 1.0350 0.9200 0.0000 1227 | 45.0000 1.0500 1.0750 0.0000 1228 | 50.0000 1.0200 1.2150 0.0000 1229 | 55.0000 0.9550 1.3450 0.0000 1230 | 60.0000 0.8750 1.4700 0.0000 1231 | 65.0000 0.7600 1.5750 0.0000 1232 | 70.0000 0.6300 1.6650 0.0000 1233 | 75.0000 0.5000 1.7350 0.0000 1234 | 80.0000 0.3650 1.7800 0.0000 1235 | 85.0000 0.2300 1.8000 0.0000 1236 | 90.0000 0.0900 1.8000 0.0000 1237 | 95.0000 -0.0500 1.7800 0.0000 1238 | 100.0000 -0.1850 1.7500 0.0000 1239 | 105.0000 -0.3200 1.7000 0.0000 1240 | 110.0000 -0.4500 1.6350 0.0000 1241 | 115.0000 -0.5750 1.5550 0.0000 1242 | 120.0000 -0.6700 1.4650 0.0000 1243 | 125.0000 -0.7600 1.3500 0.0000 1244 | 130.0000 -0.8500 1.2250 0.0000 1245 | 135.0000 -0.9300 1.0850 0.0000 1246 | 140.0000 -0.9800 0.9250 0.0000 1247 | 145.0000 -0.9000 0.7550 0.0000 1248 | 150.0000 -0.7700 0.5750 0.0000 1249 | 155.0000 -0.6700 0.4200 0.0000 1250 | 160.0000 -0.6350 0.3200 0.0000 1251 | 165.0000 -0.6800 0.2300 0.0000 1252 | 170.0000 -0.8500 0.1400 0.0000 1253 | 175.0000 -0.6600 0.0550 0.0000 1254 | 180.0000 0.0000 0.0250 0.0000 1255 | 1256 | Reynolds Number: 1e7 1257 | BV Dyn. Stall Model - Positive Stall AOA (deg): 10.0 1258 | BV Dyn. Stall Model - Negative Stall AOA (deg): -10.0 1259 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 1260 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.65 1261 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.65 1262 | AOA (deg) CL CD Cm25 1263 | -180.0000 0.0000 0.0250 0.0000 1264 | -175.0000 0.6600 0.0550 0.0000 1265 | -170.0000 0.8500 0.1400 0.0000 1266 | -165.0000 0.6800 0.2300 0.0000 1267 | -160.0000 0.6350 0.3200 0.0000 1268 | -155.0000 0.6700 0.4200 0.0000 1269 | -150.0000 0.7700 0.5750 0.0000 1270 | -145.0000 0.9000 0.7550 0.0000 1271 | -140.0000 0.9800 0.9250 0.0000 1272 | -135.0000 0.9300 1.0850 0.0000 1273 | -130.0000 0.8500 1.2250 0.0000 1274 | -125.0000 0.7600 1.3500 0.0000 1275 | -120.0000 0.6700 1.4650 0.0000 1276 | -115.0000 0.5750 1.5550 0.0000 1277 | -110.0000 0.4500 1.6350 0.0000 1278 | -105.0000 0.3200 1.7000 0.0000 1279 | -100.0000 0.1850 1.7500 0.0000 1280 | -95.0000 0.0500 1.7800 0.0000 1281 | -90.0000 -0.0900 1.8000 0.0000 1282 | -85.0000 -0.2300 1.8000 0.0000 1283 | -80.0000 -0.3650 1.7800 0.0000 1284 | -75.0000 -0.5000 1.7350 0.0000 1285 | -70.0000 -0.6300 1.6650 0.0000 1286 | -65.0000 -0.7600 1.5750 0.0000 1287 | -60.0000 -0.8750 1.4700 0.0000 1288 | -55.0000 -0.9550 1.3450 0.0000 1289 | -50.0000 -1.0200 1.2150 0.0000 1290 | -45.0000 -1.0500 1.0750 0.0000 1291 | -40.0000 -1.0350 0.9200 0.0000 1292 | -35.0000 -0.9800 0.7450 0.0000 1293 | -30.0000 -0.8550 0.5700 0.0000 1294 | -27.0000 -1.1519 0.4600 0.0000 1295 | -26.0000 -1.1374 0.4320 0.0000 1296 | -25.0000 -1.1380 0.4050 0.0000 1297 | -24.0000 -1.1538 0.3790 0.0000 1298 | -23.0000 -1.1981 0.3540 0.0000 1299 | -22.0000 -1.2767 0.3290 0.0000 1300 | -21.0000 -1.3077 0.1770 0.0000 1301 | -20.0000 -1.3325 0.0257 0.0000 1302 | -19.0000 -1.3608 0.0234 0.0000 1303 | -18.0000 -1.3897 0.0213 0.0000 1304 | -17.0000 -1.4136 0.0194 0.0000 1305 | -16.0000 -1.4233 0.0176 0.0000 1306 | -15.0000 -1.4136 0.0161 0.0000 1307 | -14.0000 -1.3825 0.0147 0.0000 1308 | -13.0000 -1.3300 0.0134 0.0000 1309 | -12.0000 -1.2591 0.0123 0.0000 1310 | -11.0000 -1.1749 0.0114 0.0000 1311 | -10.0000 -1.1000 0.0103 0.0000 1312 | -9.0000 -0.9900 0.0096 0.0000 1313 | -8.0000 -0.8800 0.0090 0.0000 1314 | -7.0000 -0.7700 0.0086 0.0000 1315 | -6.0000 -0.6600 0.0081 0.0000 1316 | -5.0000 -0.5500 0.0077 0.0000 1317 | -4.0000 -0.4400 0.0074 0.0000 1318 | -3.0000 -0.3300 0.0071 0.0000 1319 | -2.0000 -0.2200 0.0069 0.0000 1320 | -1.0000 -0.1100 0.0068 0.0000 1321 | 0.0000 0.0000 0.0068 0.0000 1322 | 1.0000 0.1100 0.0068 0.0000 1323 | 2.0000 0.2200 0.0069 0.0000 1324 | 3.0000 0.3300 0.0071 0.0000 1325 | 4.0000 0.4400 0.0074 0.0000 1326 | 5.0000 0.5500 0.0077 0.0000 1327 | 6.0000 0.6600 0.0081 0.0000 1328 | 7.0000 0.7700 0.0086 0.0000 1329 | 8.0000 0.8800 0.0090 0.0000 1330 | 9.0000 0.9900 0.0096 0.0000 1331 | 10.0000 1.1000 0.0103 0.0000 1332 | 11.0000 1.1749 0.0114 0.0000 1333 | 12.0000 1.2591 0.0123 0.0000 1334 | 13.0000 1.3300 0.0134 0.0000 1335 | 14.0000 1.3825 0.0147 0.0000 1336 | 15.0000 1.4136 0.0161 0.0000 1337 | 16.0000 1.4233 0.0176 0.0000 1338 | 17.0000 1.4136 0.0194 0.0000 1339 | 18.0000 1.3897 0.0213 0.0000 1340 | 19.0000 1.3608 0.0234 0.0000 1341 | 20.0000 1.3325 0.0257 0.0000 1342 | 21.0000 1.3077 0.1770 0.0000 1343 | 22.0000 1.2767 0.3290 0.0000 1344 | 23.0000 1.1981 0.3540 0.0000 1345 | 24.0000 1.1538 0.3790 0.0000 1346 | 25.0000 1.1380 0.4050 0.0000 1347 | 26.0000 1.1374 0.4320 0.0000 1348 | 27.0000 1.1519 0.4600 0.0000 1349 | 30.0000 0.8550 0.5700 0.0000 1350 | 35.0000 0.9800 0.7450 0.0000 1351 | 40.0000 1.0350 0.9200 0.0000 1352 | 45.0000 1.0500 1.0750 0.0000 1353 | 50.0000 1.0200 1.2150 0.0000 1354 | 55.0000 0.9550 1.3450 0.0000 1355 | 60.0000 0.8750 1.4700 0.0000 1356 | 65.0000 0.7600 1.5750 0.0000 1357 | 70.0000 0.6300 1.6650 0.0000 1358 | 75.0000 0.5000 1.7350 0.0000 1359 | 80.0000 0.3650 1.7800 0.0000 1360 | 85.0000 0.2300 1.8000 0.0000 1361 | 90.0000 0.0900 1.8000 0.0000 1362 | 95.0000 -0.0500 1.7800 0.0000 1363 | 100.0000 -0.1850 1.7500 0.0000 1364 | 105.0000 -0.3200 1.7000 0.0000 1365 | 110.0000 -0.4500 1.6350 0.0000 1366 | 115.0000 -0.5750 1.5550 0.0000 1367 | 120.0000 -0.6700 1.4650 0.0000 1368 | 125.0000 -0.7600 1.3500 0.0000 1369 | 130.0000 -0.8500 1.2250 0.0000 1370 | 135.0000 -0.9300 1.0850 0.0000 1371 | 140.0000 -0.9800 0.9250 0.0000 1372 | 145.0000 -0.9000 0.7550 0.0000 1373 | 150.0000 -0.7700 0.5750 0.0000 1374 | 155.0000 -0.6700 0.4200 0.0000 1375 | 160.0000 -0.6350 0.3200 0.0000 1376 | 165.0000 -0.6800 0.2300 0.0000 1377 | 170.0000 -0.8500 0.1400 0.0000 1378 | 175.0000 -0.6600 0.0550 0.0000 1379 | 180.0000 0.0000 0.0250 0.0000 1380 | -------------------------------------------------------------------------------- /airfoilData/cactusImport/NACA_0018.dat: -------------------------------------------------------------------------------- 1 | Title: NACA0018 2 | Thickness to Chord Ratio: 0.18 3 | Zero Lift AOA (deg): 0.0 4 | Reverse Camber Direction: 0 5 | 6 | Reynolds Number: 1e4 7 | BV Dyn. Stall Model - Positive Stall AOA (deg): 1.0 8 | BV Dyn. Stall Model - Negative Stall AOA (deg): -1.0 9 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 5.73 10 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1 11 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1 12 | AOA (deg) CL CD Cm25 13 | -180 0 0.0250000000000000 0 14 | -175 0.660000000000000 0.0550000000000000 0 15 | -170 0.850000000000000 0.140000000000000 0 16 | -165 0.680000000000000 0.230000000000000 0 17 | -160 0.635000000000000 0.320000000000000 0 18 | -155 0.670000000000000 0.420000000000000 0 19 | -150 0.770000000000000 0.575000000000000 0 20 | -145 0.900000000000000 0.755000000000000 0 21 | -140 0.980000000000000 0.925000000000000 0 22 | -135 0.930000000000000 1.08500000000000 0 23 | -130 0.850000000000000 1.22500000000000 0 24 | -125 0.760000000000000 1.35000000000000 0 25 | -120 0.670000000000000 1.46500000000000 0 26 | -115 0.575000000000000 1.55500000000000 0 27 | -110 0.450000000000000 1.63500000000000 0 28 | -105 0.320000000000000 1.70000000000000 0 29 | -100 0.185000000000000 1.75000000000000 0 30 | -95 0.0500000000000000 1.78000000000000 0 31 | -90 -0.0900000000000000 1.80000000000000 0 32 | -85 -0.230000000000000 1.80000000000000 0 33 | -80 -0.365000000000000 1.78000000000000 0 34 | -75 -0.500000000000000 1.73500000000000 0 35 | -70 -0.630000000000000 1.66500000000000 0 36 | -65 -0.760000000000000 1.57500000000000 0 37 | -60 -0.875000000000000 1.47000000000000 0 38 | -55 -0.955000000000000 1.34500000000000 0 39 | -50 -1.02000000000000 1.21500000000000 0 40 | -45 -1.05000000000000 1.07500000000000 0 41 | -40 -1.03500000000000 0.920000000000000 0 42 | -35 -0.980000000000000 0.745000000000000 0 43 | -30 -0.855000000000000 0.570000000000000 0 44 | -25 -0.577500000000000 0.405000000000000 0 45 | -22 -0.417200000000000 0.329000000000000 0 46 | -20 -0.311100000000000 0.282000000000000 0 47 | -18 -0.207000000000000 0.238000000000000 0 48 | -16 -0.105100000000000 0.196000000000000 0 49 | -14 -0.00850000000000000 0.158000000000000 0 50 | -12 0.0767000000000000 0.123000000000000 0 51 | -11 0.112500000000000 0.0800000000000000 0 52 | -10 0.142300000000000 0.0574000000000000 0 53 | -9 0.158400000000000 0.0525000000000000 0 54 | -8 0.150100000000000 0.0489000000000000 0 55 | -7 0.118200000000000 0.0463000000000000 0 56 | -6 0.0839000000000000 0.0443000000000000 0 57 | -5 0.0577000000000000 0.0425000000000000 0 58 | -4 0.0368000000000000 0.0410000000000000 0 59 | -3 0.0233000000000000 0.0399000000000000 0 60 | -2 0.0154000000000000 0.0391000000000000 0 61 | -1 0.00450000000000000 0.0387000000000000 0 62 | 0 0 0.0385000000000000 0 63 | 1 -0.00450000000000000 0.0387000000000000 0 64 | 2 -0.0154000000000000 0.0391000000000000 0 65 | 3 -0.0233000000000000 0.0399000000000000 0 66 | 4 -0.0368000000000000 0.0410000000000000 0 67 | 5 -0.0577000000000000 0.0425000000000000 0 68 | 6 -0.0839000000000000 0.0443000000000000 0 69 | 7 -0.118200000000000 0.0463000000000000 0 70 | 8 -0.150100000000000 0.0489000000000000 0 71 | 9 -0.158400000000000 0.0525000000000000 0 72 | 10 -0.142300000000000 0.0574000000000000 0 73 | 11 -0.112500000000000 0.0800000000000000 0 74 | 12 -0.0767000000000000 0.123000000000000 0 75 | 14 0.00850000000000000 0.158000000000000 0 76 | 16 0.105100000000000 0.196000000000000 0 77 | 18 0.207000000000000 0.238000000000000 0 78 | 20 0.311100000000000 0.282000000000000 0 79 | 22 0.417200000000000 0.329000000000000 0 80 | 25 0.577500000000000 0.405000000000000 0 81 | 30 0.855000000000000 0.570000000000000 0 82 | 35 0.980000000000000 0.745000000000000 0 83 | 40 1.03500000000000 0.920000000000000 0 84 | 45 1.05000000000000 1.07500000000000 0 85 | 50 1.02000000000000 1.21500000000000 0 86 | 55 0.955000000000000 1.34500000000000 0 87 | 60 0.875000000000000 1.47000000000000 0 88 | 65 0.760000000000000 1.57500000000000 0 89 | 70 0.630000000000000 1.66500000000000 0 90 | 75 0.500000000000000 1.73500000000000 0 91 | 80 0.365000000000000 1.78000000000000 0 92 | 85 0.230000000000000 1.80000000000000 0 93 | 90 0.0900000000000000 1.80000000000000 0 94 | 95 -0.0500000000000000 1.78000000000000 0 95 | 100 -0.185000000000000 1.75000000000000 0 96 | 105 -0.320000000000000 1.70000000000000 0 97 | 110 -0.450000000000000 1.63500000000000 0 98 | 115 -0.575000000000000 1.55500000000000 0 99 | 120 -0.670000000000000 1.46500000000000 0 100 | 125 -0.760000000000000 1.35000000000000 0 101 | 130 -0.850000000000000 1.22500000000000 0 102 | 135 -0.930000000000000 1.08500000000000 0 103 | 140 -0.980000000000000 0.925000000000000 0 104 | 145 -0.900000000000000 0.755000000000000 0 105 | 150 -0.770000000000000 0.575000000000000 0 106 | 155 -0.670000000000000 0.420000000000000 0 107 | 160 -0.635000000000000 0.320000000000000 0 108 | 165 -0.680000000000000 0.230000000000000 0 109 | 170 -0.850000000000000 0.140000000000000 0 110 | 175 -0.660000000000000 0.0550000000000000 0 111 | 180 0 0.0250000000000000 0 112 | 113 | Reynolds Number: 2e4 114 | BV Dyn. Stall Model - Positive Stall AOA (deg): 1.0 115 | BV Dyn. Stall Model - Negative Stall AOA (deg): -1.0 116 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 5.73 117 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1 118 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1 119 | AOA (deg) CL CD Cm25 120 | -180 0 0.0250000000000000 0 121 | -175 0.660000000000000 0.0550000000000000 0 122 | -170 0.850000000000000 0.140000000000000 0 123 | -165 0.680000000000000 0.230000000000000 0 124 | -160 0.635000000000000 0.320000000000000 0 125 | -155 0.670000000000000 0.420000000000000 0 126 | -150 0.770000000000000 0.575000000000000 0 127 | -145 0.900000000000000 0.755000000000000 0 128 | -140 0.980000000000000 0.925000000000000 0 129 | -135 0.930000000000000 1.08500000000000 0 130 | -130 0.850000000000000 1.22500000000000 0 131 | -125 0.760000000000000 1.35000000000000 0 132 | -120 0.670000000000000 1.46500000000000 0 133 | -115 0.575000000000000 1.55500000000000 0 134 | -110 0.450000000000000 1.63500000000000 0 135 | -105 0.320000000000000 1.70000000000000 0 136 | -100 0.185000000000000 1.75000000000000 0 137 | -95 0.0500000000000000 1.78000000000000 0 138 | -90 -0.0900000000000000 1.80000000000000 0 139 | -85 -0.230000000000000 1.80000000000000 0 140 | -80 -0.365000000000000 1.78000000000000 0 141 | -75 -0.500000000000000 1.73500000000000 0 142 | -70 -0.630000000000000 1.66500000000000 0 143 | -65 -0.760000000000000 1.57500000000000 0 144 | -60 -0.875000000000000 1.47000000000000 0 145 | -55 -0.955000000000000 1.34500000000000 0 146 | -50 -1.02000000000000 1.21500000000000 0 147 | -45 -1.05000000000000 1.07500000000000 0 148 | -40 -1.03500000000000 0.920000000000000 0 149 | -35 -0.980000000000000 0.745000000000000 0 150 | -30 -0.855000000000000 0.570000000000000 0 151 | -25 -0.579800000000000 0.405000000000000 0 152 | -22 -0.419800000000000 0.329000000000000 0 153 | -20 -0.315100000000000 0.282000000000000 0 154 | -18 -0.212000000000000 0.238000000000000 0 155 | -16 -0.111400000000000 0.196000000000000 0 156 | -14 -0.0172000000000000 0.158000000000000 0 157 | -12 0.0602000000000000 0.123000000000000 0 158 | -10 0.100300000000000 0.0630000000000000 0 159 | -9 0.0682000000000000 0.0396000000000000 0 160 | -8 -0.0214000000000000 0.0376000000000000 0 161 | -7 -0.116100000000000 0.0358000000000000 0 162 | -6 -0.158200000000000 0.0339000000000000 0 163 | -5 -0.178800000000000 0.0323000000000000 0 164 | -4 -0.178800000000000 0.0310000000000000 0 165 | -3 -0.155000000000000 0.0299000000000000 0 166 | -2 -0.113500000000000 0.0292000000000000 0 167 | -1 -0.0607000000000000 0.0288000000000000 0 168 | 0 0 0.0286000000000000 0 169 | 1 0.0607000000000000 0.0288000000000000 0 170 | 2 0.113500000000000 0.0292000000000000 0 171 | 3 0.155000000000000 0.0299000000000000 0 172 | 4 0.178800000000000 0.0310000000000000 0 173 | 5 0.178800000000000 0.0323000000000000 0 174 | 6 0.158200000000000 0.0339000000000000 0 175 | 7 0.116100000000000 0.0358000000000000 0 176 | 8 0.0214000000000000 0.0376000000000000 0 177 | 9 -0.0682000000000000 0.0396000000000000 0 178 | 10 -0.100300000000000 0.0630000000000000 0 179 | 12 -0.0602000000000000 0.123000000000000 0 180 | 14 0.0172000000000000 0.158000000000000 0 181 | 16 0.111400000000000 0.196000000000000 0 182 | 18 0.212000000000000 0.238000000000000 0 183 | 20 0.315100000000000 0.282000000000000 0 184 | 22 0.419800000000000 0.329000000000000 0 185 | 25 0.579800000000000 0.405000000000000 0 186 | 30 0.855000000000000 0.570000000000000 0 187 | 35 0.980000000000000 0.745000000000000 0 188 | 40 1.03500000000000 0.920000000000000 0 189 | 45 1.05000000000000 1.07500000000000 0 190 | 50 1.02000000000000 1.21500000000000 0 191 | 55 0.955000000000000 1.34500000000000 0 192 | 60 0.875000000000000 1.47000000000000 0 193 | 65 0.760000000000000 1.57500000000000 0 194 | 70 0.630000000000000 1.66500000000000 0 195 | 75 0.500000000000000 1.73500000000000 0 196 | 80 0.365000000000000 1.78000000000000 0 197 | 85 0.230000000000000 1.80000000000000 0 198 | 90 0.0900000000000000 1.80000000000000 0 199 | 95 -0.0500000000000000 1.78000000000000 0 200 | 100 -0.185000000000000 1.75000000000000 0 201 | 105 -0.320000000000000 1.70000000000000 0 202 | 110 -0.450000000000000 1.63500000000000 0 203 | 115 -0.575000000000000 1.55500000000000 0 204 | 120 -0.670000000000000 1.46500000000000 0 205 | 125 -0.760000000000000 1.35000000000000 0 206 | 130 -0.850000000000000 1.22500000000000 0 207 | 135 -0.930000000000000 1.08500000000000 0 208 | 140 -0.980000000000000 0.925000000000000 0 209 | 145 -0.900000000000000 0.755000000000000 0 210 | 150 -0.770000000000000 0.575000000000000 0 211 | 155 -0.670000000000000 0.420000000000000 0 212 | 160 -0.635000000000000 0.320000000000000 0 213 | 165 -0.680000000000000 0.230000000000000 0 214 | 170 -0.850000000000000 0.140000000000000 0 215 | 175 -0.660000000000000 0.0550000000000000 0 216 | 180 0 0.0250000000000000 0 217 | 218 | Reynolds Number: 4e4 219 | BV Dyn. Stall Model - Positive Stall AOA (deg): 4.0 220 | BV Dyn. Stall Model - Negative Stall AOA (deg): -4.0 221 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 5.363 222 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 0.7 223 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -0.7 224 | AOA (deg) CL CD Cm25 225 | -180 0 0.0250000000000000 0 226 | -175 0.660000000000000 0.0550000000000000 0 227 | -170 0.850000000000000 0.140000000000000 0 228 | -165 0.680000000000000 0.230000000000000 0 229 | -160 0.635000000000000 0.320000000000000 0 230 | -155 0.670000000000000 0.420000000000000 0 231 | -150 0.770000000000000 0.575000000000000 0 232 | -145 0.900000000000000 0.755000000000000 0 233 | -140 0.980000000000000 0.925000000000000 0 234 | -135 0.930000000000000 1.08500000000000 0 235 | -130 0.850000000000000 1.22500000000000 0 236 | -125 0.760000000000000 1.35000000000000 0 237 | -120 0.670000000000000 1.46500000000000 0 238 | -115 0.575000000000000 1.55500000000000 0 239 | -110 0.450000000000000 1.63500000000000 0 240 | -105 0.320000000000000 1.70000000000000 0 241 | -100 0.185000000000000 1.75000000000000 0 242 | -95 0.0500000000000000 1.78000000000000 0 243 | -90 -0.0900000000000000 1.80000000000000 0 244 | -85 -0.230000000000000 1.80000000000000 0 245 | -80 -0.365000000000000 1.78000000000000 0 246 | -75 -0.500000000000000 1.73500000000000 0 247 | -70 -0.630000000000000 1.66500000000000 0 248 | -65 -0.760000000000000 1.57500000000000 0 249 | -60 -0.875000000000000 1.47000000000000 0 250 | -55 -0.955000000000000 1.34500000000000 0 251 | -50 -1.02000000000000 1.21500000000000 0 252 | -45 -1.05000000000000 1.07500000000000 0 253 | -40 -1.03500000000000 0.920000000000000 0 254 | -35 -0.980000000000000 0.745000000000000 0 255 | -30 -0.855000000000000 0.570000000000000 0 256 | -25 -0.584000000000000 0.405000000000000 0 257 | -22 -0.426500000000000 0.329000000000000 0 258 | -20 -0.323600000000000 0.282000000000000 0 259 | -18 -0.222800000000000 0.238000000000000 0 260 | -16 -0.128700000000000 0.196000000000000 0 261 | -14 -0.0489000000000000 0.158000000000000 0 262 | -12 -0.0139000000000000 0.123000000000000 0 263 | -10 -0.210800000000000 0.0620000000000000 0 264 | -9 -0.354400000000000 0.0327000000000000 0 265 | -8 -0.442800000000000 0.0303000000000000 0 266 | -7 -0.475800000000000 0.0282000000000000 0 267 | -6 -0.457300000000000 0.0263000000000000 0 268 | -5 -0.411700000000000 0.0247000000000000 0 269 | -4 -0.349500000000000 0.0235000000000000 0 270 | -3 -0.268800000000000 0.0225000000000000 0 271 | -2 -0.183300000000000 0.0219000000000000 0 272 | -1 -0.0936000000000000 0.0215000000000000 0 273 | 0 0 0.0214000000000000 0 274 | 1 0.0936000000000000 0.0215000000000000 0 275 | 2 0.183300000000000 0.0219000000000000 0 276 | 3 0.268800000000000 0.0225000000000000 0 277 | 4 0.349500000000000 0.0235000000000000 0 278 | 5 0.411700000000000 0.0247000000000000 0 279 | 6 0.457300000000000 0.0263000000000000 0 280 | 7 0.475800000000000 0.0282000000000000 0 281 | 8 0.442800000000000 0.0303000000000000 0 282 | 9 0.354400000000000 0.0327000000000000 0 283 | 10 0.210800000000000 0.0620000000000000 0 284 | 12 0.0139000000000000 0.123000000000000 0 285 | 14 0.0489000000000000 0.158000000000000 0 286 | 16 0.128700000000000 0.196000000000000 0 287 | 18 0.222800000000000 0.238000000000000 0 288 | 20 0.323600000000000 0.282000000000000 0 289 | 22 0.426500000000000 0.329000000000000 0 290 | 25 0.584000000000000 0.405000000000000 0 291 | 30 0.855000000000000 0.570000000000000 0 292 | 35 0.980000000000000 0.745000000000000 0 293 | 40 1.03500000000000 0.920000000000000 0 294 | 45 1.05000000000000 1.07500000000000 0 295 | 50 1.02000000000000 1.21500000000000 0 296 | 55 0.955000000000000 1.34500000000000 0 297 | 60 0.875000000000000 1.47000000000000 0 298 | 65 0.760000000000000 1.57500000000000 0 299 | 70 0.630000000000000 1.66500000000000 0 300 | 75 0.500000000000000 1.73500000000000 0 301 | 80 0.365000000000000 1.78000000000000 0 302 | 85 0.230000000000000 1.80000000000000 0 303 | 90 0.0900000000000000 1.80000000000000 0 304 | 95 -0.0500000000000000 1.78000000000000 0 305 | 100 -0.185000000000000 1.75000000000000 0 306 | 105 -0.320000000000000 1.70000000000000 0 307 | 110 -0.450000000000000 1.63500000000000 0 308 | 115 -0.575000000000000 1.55500000000000 0 309 | 120 -0.670000000000000 1.46500000000000 0 310 | 125 -0.760000000000000 1.35000000000000 0 311 | 130 -0.850000000000000 1.22500000000000 0 312 | 135 -0.930000000000000 1.08500000000000 0 313 | 140 -0.980000000000000 0.925000000000000 0 314 | 145 -0.900000000000000 0.755000000000000 0 315 | 150 -0.770000000000000 0.575000000000000 0 316 | 155 -0.670000000000000 0.420000000000000 0 317 | 160 -0.635000000000000 0.320000000000000 0 318 | 165 -0.680000000000000 0.230000000000000 0 319 | 170 -0.850000000000000 0.140000000000000 0 320 | 175 -0.660000000000000 0.0550000000000000 0 321 | 180 0 0.0250000000000000 0 322 | 323 | Reynolds Number: 8e4 324 | BV Dyn. Stall Model - Positive Stall AOA (deg): 5.0 325 | BV Dyn. Stall Model - Negative Stall AOA (deg): -5.0 326 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 5.447 327 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 0.86 328 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -0.86 329 | AOA (deg) CL CD Cm25 330 | -180 0 0.0250000000000000 0 331 | -175 0.660000000000000 0.0550000000000000 0 332 | -170 0.850000000000000 0.140000000000000 0 333 | -165 0.680000000000000 0.230000000000000 0 334 | -160 0.635000000000000 0.320000000000000 0 335 | -155 0.670000000000000 0.420000000000000 0 336 | -150 0.770000000000000 0.575000000000000 0 337 | -145 0.900000000000000 0.755000000000000 0 338 | -140 0.980000000000000 0.925000000000000 0 339 | -135 0.930000000000000 1.08500000000000 0 340 | -130 0.850000000000000 1.22500000000000 0 341 | -125 0.760000000000000 1.35000000000000 0 342 | -120 0.670000000000000 1.46500000000000 0 343 | -115 0.575000000000000 1.55500000000000 0 344 | -110 0.450000000000000 1.63500000000000 0 345 | -105 0.320000000000000 1.70000000000000 0 346 | -100 0.185000000000000 1.75000000000000 0 347 | -95 0.0500000000000000 1.78000000000000 0 348 | -90 -0.0900000000000000 1.80000000000000 0 349 | -85 -0.230000000000000 1.80000000000000 0 350 | -80 -0.365000000000000 1.78000000000000 0 351 | -75 -0.500000000000000 1.73500000000000 0 352 | -70 -0.630000000000000 1.66500000000000 0 353 | -65 -0.760000000000000 1.57500000000000 0 354 | -60 -0.875000000000000 1.47000000000000 0 355 | -55 -0.955000000000000 1.34500000000000 0 356 | -50 -1.02000000000000 1.21500000000000 0 357 | -45 -1.05000000000000 1.07500000000000 0 358 | -40 -1.03500000000000 0.920000000000000 0 359 | -35 -0.980000000000000 0.745000000000000 0 360 | -30 -0.855000000000000 0.570000000000000 0 361 | -25 -0.596300000000000 0.405000000000000 0 362 | -22 -0.443000000000000 0.329000000000000 0 363 | -20 -0.347200000000000 0.282000000000000 0 364 | -18 -0.260300000000000 0.238000000000000 0 365 | -16 -0.202700000000000 0.196000000000000 0 366 | -14 -0.225600000000000 0.158000000000000 0 367 | -12 -0.440800000000000 0.0800000000000000 0 368 | -11 -0.553100000000000 0.0315000000000000 0 369 | -10 -0.624800000000000 0.0288000000000000 0 370 | -9 -0.660600000000000 0.0264000000000000 0 371 | -8 -0.658900000000000 0.0242000000000000 0 372 | -7 -0.622400000000000 0.0223000000000000 0 373 | -6 -0.561500000000000 0.0206000000000000 0 374 | -5 -0.475300000000000 0.0192000000000000 0 375 | -4 -0.388000000000000 0.0181000000000000 0 376 | -3 -0.292400000000000 0.0172000000000000 0 377 | -2 -0.193500000000000 0.0167000000000000 0 378 | -1 -0.0889000000000000 0.0163000000000000 0 379 | 0 0 0.0162000000000000 0 380 | 1 0.0889000000000000 0.0163000000000000 0 381 | 2 0.193500000000000 0.0167000000000000 0 382 | 3 0.292400000000000 0.0172000000000000 0 383 | 4 0.388000000000000 0.0181000000000000 0 384 | 5 0.475300000000000 0.0192000000000000 0 385 | 6 0.561500000000000 0.0206000000000000 0 386 | 7 0.622400000000000 0.0223000000000000 0 387 | 8 0.658900000000000 0.0242000000000000 0 388 | 9 0.660600000000000 0.0264000000000000 0 389 | 10 0.624800000000000 0.0288000000000000 0 390 | 11 0.553100000000000 0.0315000000000000 0 391 | 12 0.440800000000000 0.0800000000000000 0 392 | 14 0.225600000000000 0.158000000000000 0 393 | 16 0.202700000000000 0.196000000000000 0 394 | 18 0.260300000000000 0.238000000000000 0 395 | 20 0.347200000000000 0.282000000000000 0 396 | 22 0.443000000000000 0.329000000000000 0 397 | 25 0.596300000000000 0.405000000000000 0 398 | 30 0.855000000000000 0.570000000000000 0 399 | 35 0.980000000000000 0.745000000000000 0 400 | 40 1.03500000000000 0.920000000000000 0 401 | 45 1.05000000000000 1.07500000000000 0 402 | 50 1.02000000000000 1.21500000000000 0 403 | 55 0.955000000000000 1.34500000000000 0 404 | 60 0.875000000000000 1.47000000000000 0 405 | 65 0.760000000000000 1.57500000000000 0 406 | 70 0.630000000000000 1.66500000000000 0 407 | 75 0.500000000000000 1.73500000000000 0 408 | 80 0.365000000000000 1.78000000000000 0 409 | 85 0.230000000000000 1.80000000000000 0 410 | 90 0.0900000000000000 1.80000000000000 0 411 | 95 -0.0500000000000000 1.78000000000000 0 412 | 100 -0.185000000000000 1.75000000000000 0 413 | 105 -0.320000000000000 1.70000000000000 0 414 | 110 -0.450000000000000 1.63500000000000 0 415 | 115 -0.575000000000000 1.55500000000000 0 416 | 120 -0.670000000000000 1.46500000000000 0 417 | 125 -0.760000000000000 1.35000000000000 0 418 | 130 -0.850000000000000 1.22500000000000 0 419 | 135 -0.930000000000000 1.08500000000000 0 420 | 140 -0.980000000000000 0.925000000000000 0 421 | 145 -0.900000000000000 0.755000000000000 0 422 | 150 -0.770000000000000 0.575000000000000 0 423 | 155 -0.670000000000000 0.420000000000000 0 424 | 160 -0.635000000000000 0.320000000000000 0 425 | 165 -0.680000000000000 0.230000000000000 0 426 | 170 -0.850000000000000 0.140000000000000 0 427 | 175 -0.660000000000000 0.0550000000000000 0 428 | 180 0 0.0250000000000000 0 429 | 430 | Reynolds Number: 1.6e5 431 | BV Dyn. Stall Model - Positive Stall AOA (deg): 5.0 432 | BV Dyn. Stall Model - Negative Stall AOA (deg): -5.0 433 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 434 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.1 435 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.1 436 | AOA (deg) CL CD Cm25 437 | -180 0 0.0250000000000000 0 438 | -175 0.660000000000000 0.0550000000000000 0 439 | -170 0.850000000000000 0.140000000000000 0 440 | -165 0.680000000000000 0.230000000000000 0 441 | -160 0.635000000000000 0.320000000000000 0 442 | -155 0.670000000000000 0.420000000000000 0 443 | -150 0.770000000000000 0.575000000000000 0 444 | -145 0.900000000000000 0.755000000000000 0 445 | -140 0.980000000000000 0.925000000000000 0 446 | -135 0.930000000000000 1.08500000000000 0 447 | -130 0.850000000000000 1.22500000000000 0 448 | -125 0.760000000000000 1.35000000000000 0 449 | -120 0.670000000000000 1.46500000000000 0 450 | -115 0.575000000000000 1.55500000000000 0 451 | -110 0.450000000000000 1.63500000000000 0 452 | -105 0.320000000000000 1.70000000000000 0 453 | -100 0.185000000000000 1.75000000000000 0 454 | -95 0.0500000000000000 1.78000000000000 0 455 | -90 -0.0900000000000000 1.80000000000000 0 456 | -85 -0.230000000000000 1.80000000000000 0 457 | -80 -0.365000000000000 1.78000000000000 0 458 | -75 -0.500000000000000 1.73500000000000 0 459 | -70 -0.630000000000000 1.66500000000000 0 460 | -65 -0.760000000000000 1.57500000000000 0 461 | -60 -0.875000000000000 1.47000000000000 0 462 | -55 -0.955000000000000 1.34500000000000 0 463 | -50 -1.02000000000000 1.21500000000000 0 464 | -45 -1.05000000000000 1.07500000000000 0 465 | -40 -1.03500000000000 0.920000000000000 0 466 | -35 -0.980000000000000 0.745000000000000 0 467 | -30 -0.855000000000000 0.570000000000000 0 468 | -25 -0.632100000000000 0.405000000000000 0 469 | -22 -0.502600000000000 0.329000000000000 0 470 | -20 -0.438200000000000 0.282000000000000 0 471 | -18 -0.420200000000000 0.238000000000000 0 472 | -16 -0.489600000000000 0.196000000000000 0 473 | -14 -0.623700000000000 0.158000000000000 0 474 | -13 -0.692300000000000 0.0770000000000000 0 475 | -12 -0.748800000000000 0.0288000000000000 0 476 | -11 -0.785200000000000 0.0262000000000000 0 477 | -10 -0.794900000000000 0.0238000000000000 0 478 | -9 -0.778100000000000 0.0217000000000000 0 479 | -8 -0.737300000000000 0.0198000000000000 0 480 | -7 -0.672400000000000 0.0181000000000000 0 481 | -6 -0.596000000000000 0.0166000000000000 0 482 | -5 -0.506800000000000 0.0153000000000000 0 483 | -4 -0.411400000000000 0.0144000000000000 0 484 | -3 -0.308800000000000 0.0137000000000000 0 485 | -2 -0.220000000000000 0.0131000000000000 0 486 | -1 -0.110000000000000 0.0129000000000000 0 487 | 0 0 0.0128000000000000 0 488 | 1 0.110000000000000 0.0129000000000000 0 489 | 2 0.220000000000000 0.0131000000000000 0 490 | 3 0.308800000000000 0.0137000000000000 0 491 | 4 0.411400000000000 0.0144000000000000 0 492 | 5 0.506800000000000 0.0153000000000000 0 493 | 6 0.596000000000000 0.0166000000000000 0 494 | 7 0.672400000000000 0.0181000000000000 0 495 | 8 0.737300000000000 0.0198000000000000 0 496 | 9 0.778100000000000 0.0217000000000000 0 497 | 10 0.794900000000000 0.0238000000000000 0 498 | 11 0.785200000000000 0.0262000000000000 0 499 | 12 0.748800000000000 0.0288000000000000 0 500 | 13 0.692300000000000 0.0770000000000000 0 501 | 14 0.623700000000000 0.158000000000000 0 502 | 16 0.489600000000000 0.196000000000000 0 503 | 18 0.420200000000000 0.238000000000000 0 504 | 20 0.438200000000000 0.282000000000000 0 505 | 22 0.502600000000000 0.329000000000000 0 506 | 25 0.632100000000000 0.405000000000000 0 507 | 30 0.855000000000000 0.570000000000000 0 508 | 35 0.980000000000000 0.745000000000000 0 509 | 40 1.03500000000000 0.920000000000000 0 510 | 45 1.05000000000000 1.07500000000000 0 511 | 50 1.02000000000000 1.21500000000000 0 512 | 55 0.955000000000000 1.34500000000000 0 513 | 60 0.875000000000000 1.47000000000000 0 514 | 65 0.760000000000000 1.57500000000000 0 515 | 70 0.630000000000000 1.66500000000000 0 516 | 75 0.500000000000000 1.73500000000000 0 517 | 80 0.365000000000000 1.78000000000000 0 518 | 85 0.230000000000000 1.80000000000000 0 519 | 90 0.0900000000000000 1.80000000000000 0 520 | 95 -0.0500000000000000 1.78000000000000 0 521 | 100 -0.185000000000000 1.75000000000000 0 522 | 105 -0.320000000000000 1.70000000000000 0 523 | 110 -0.450000000000000 1.63500000000000 0 524 | 115 -0.575000000000000 1.55500000000000 0 525 | 120 -0.670000000000000 1.46500000000000 0 526 | 125 -0.760000000000000 1.35000000000000 0 527 | 130 -0.850000000000000 1.22500000000000 0 528 | 135 -0.930000000000000 1.08500000000000 0 529 | 140 -0.980000000000000 0.925000000000000 0 530 | 145 -0.900000000000000 0.755000000000000 0 531 | 150 -0.770000000000000 0.575000000000000 0 532 | 155 -0.670000000000000 0.420000000000000 0 533 | 160 -0.635000000000000 0.320000000000000 0 534 | 165 -0.680000000000000 0.230000000000000 0 535 | 170 -0.850000000000000 0.140000000000000 0 536 | 175 -0.660000000000000 0.0550000000000000 0 537 | 180 0 0.0250000000000000 0 538 | 539 | Reynolds Number: 3.6e5 540 | BV Dyn. Stall Model - Positive Stall AOA (deg): 4.0 541 | BV Dyn. Stall Model - Negative Stall AOA (deg): -4.0 542 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 543 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.32 544 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.32 545 | AOA (deg) CL CD Cm25 546 | -180 0 0.0250000000000000 0 547 | -175 0.660000000000000 0.0550000000000000 0 548 | -170 0.850000000000000 0.140000000000000 0 549 | -165 0.680000000000000 0.230000000000000 0 550 | -160 0.635000000000000 0.320000000000000 0 551 | -155 0.670000000000000 0.420000000000000 0 552 | -150 0.770000000000000 0.575000000000000 0 553 | -145 0.900000000000000 0.755000000000000 0 554 | -140 0.980000000000000 0.925000000000000 0 555 | -135 0.930000000000000 1.08500000000000 0 556 | -130 0.850000000000000 1.22500000000000 0 557 | -125 0.760000000000000 1.35000000000000 0 558 | -120 0.670000000000000 1.46500000000000 0 559 | -115 0.575000000000000 1.55500000000000 0 560 | -110 0.450000000000000 1.63500000000000 0 561 | -105 0.320000000000000 1.70000000000000 0 562 | -100 0.185000000000000 1.75000000000000 0 563 | -95 0.0500000000000000 1.78000000000000 0 564 | -90 -0.0900000000000000 1.80000000000000 0 565 | -85 -0.230000000000000 1.80000000000000 0 566 | -80 -0.365000000000000 1.78000000000000 0 567 | -75 -0.500000000000000 1.73500000000000 0 568 | -70 -0.630000000000000 1.66500000000000 0 569 | -65 -0.760000000000000 1.57500000000000 0 570 | -60 -0.875000000000000 1.47000000000000 0 571 | -55 -0.955000000000000 1.34500000000000 0 572 | -50 -1.02000000000000 1.21500000000000 0 573 | -45 -1.05000000000000 1.07500000000000 0 574 | -40 -1.03500000000000 0.920000000000000 0 575 | -35 -0.980000000000000 0.745000000000000 0 576 | -30 -0.855000000000000 0.570000000000000 0 577 | -25 -0.772400000000000 0.405000000000000 0 578 | -22 -0.705000000000000 0.329000000000000 0 579 | -20 -0.699700000000000 0.282000000000000 0 580 | -18 -0.731900000000000 0.238000000000000 0 581 | -16 -0.800700000000000 0.196000000000000 0 582 | -14 -0.880300000000000 0.0940000000000000 0 583 | -13 -0.910400000000000 0.0259000000000000 0 584 | -12 -0.927900000000000 0.0235000000000000 0 585 | -11 -0.924900000000000 0.0213000000000000 0 586 | -10 -0.898300000000000 0.0194000000000000 0 587 | -9 -0.852600000000000 0.0176000000000000 0 588 | -8 -0.787900000000000 0.0159000000000000 0 589 | -7 -0.710000000000000 0.0145000000000000 0 590 | -6 -0.622800000000000 0.0132000000000000 0 591 | -5 -0.524000000000000 0.0121000000000000 0 592 | -4 -0.440000000000000 0.0112000000000000 0 593 | -3 -0.330000000000000 0.0107000000000000 0 594 | -2 -0.220000000000000 0.0104000000000000 0 595 | -1 -0.110000000000000 0.0102000000000000 0 596 | 0 0 0.0101000000000000 0 597 | 1 0.110000000000000 0.0102000000000000 0 598 | 2 0.220000000000000 0.0104000000000000 0 599 | 3 0.330000000000000 0.0107000000000000 0 600 | 4 0.440000000000000 0.0112000000000000 0 601 | 5 0.524000000000000 0.0121000000000000 0 602 | 6 0.622800000000000 0.0132000000000000 0 603 | 7 0.710000000000000 0.0145000000000000 0 604 | 8 0.787900000000000 0.0159000000000000 0 605 | 9 0.852600000000000 0.0176000000000000 0 606 | 10 0.898300000000000 0.0194000000000000 0 607 | 11 0.924900000000000 0.0213000000000000 0 608 | 12 0.927900000000000 0.0235000000000000 0 609 | 13 0.910400000000000 0.0259000000000000 0 610 | 14 0.880300000000000 0.0940000000000000 0 611 | 16 0.800700000000000 0.196000000000000 0 612 | 18 0.731900000000000 0.238000000000000 0 613 | 20 0.699700000000000 0.282000000000000 0 614 | 22 0.705000000000000 0.329000000000000 0 615 | 25 0.772400000000000 0.405000000000000 0 616 | 30 0.855000000000000 0.570000000000000 0 617 | 35 0.980000000000000 0.745000000000000 0 618 | 40 1.03500000000000 0.920000000000000 0 619 | 45 1.05000000000000 1.07500000000000 0 620 | 50 1.02000000000000 1.21500000000000 0 621 | 55 0.955000000000000 1.34500000000000 0 622 | 60 0.875000000000000 1.47000000000000 0 623 | 65 0.760000000000000 1.57500000000000 0 624 | 70 0.630000000000000 1.66500000000000 0 625 | 75 0.500000000000000 1.73500000000000 0 626 | 80 0.365000000000000 1.78000000000000 0 627 | 85 0.230000000000000 1.80000000000000 0 628 | 90 0.0900000000000000 1.80000000000000 0 629 | 95 -0.0500000000000000 1.78000000000000 0 630 | 100 -0.185000000000000 1.75000000000000 0 631 | 105 -0.320000000000000 1.70000000000000 0 632 | 110 -0.450000000000000 1.63500000000000 0 633 | 115 -0.575000000000000 1.55500000000000 0 634 | 120 -0.670000000000000 1.46500000000000 0 635 | 125 -0.760000000000000 1.35000000000000 0 636 | 130 -0.850000000000000 1.22500000000000 0 637 | 135 -0.930000000000000 1.08500000000000 0 638 | 140 -0.980000000000000 0.925000000000000 0 639 | 145 -0.900000000000000 0.755000000000000 0 640 | 150 -0.770000000000000 0.575000000000000 0 641 | 155 -0.670000000000000 0.420000000000000 0 642 | 160 -0.635000000000000 0.320000000000000 0 643 | 165 -0.680000000000000 0.230000000000000 0 644 | 170 -0.850000000000000 0.140000000000000 0 645 | 175 -0.660000000000000 0.0550000000000000 0 646 | 180 0 0.0250000000000000 0 647 | 648 | Reynolds Number: 7e5 649 | BV Dyn. Stall Model - Positive Stall AOA (deg): 5.0 650 | BV Dyn. Stall Model - Negative Stall AOA (deg): -5.0 651 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 652 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.43 653 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.43 654 | AOA (deg) CL CD Cm25 655 | -180 0 0.0250000000000000 0 656 | -175 0.660000000000000 0.0550000000000000 0 657 | -170 0.850000000000000 0.140000000000000 0 658 | -165 0.680000000000000 0.230000000000000 0 659 | -160 0.635000000000000 0.320000000000000 0 660 | -155 0.670000000000000 0.420000000000000 0 661 | -150 0.770000000000000 0.575000000000000 0 662 | -145 0.900000000000000 0.755000000000000 0 663 | -140 0.980000000000000 0.925000000000000 0 664 | -135 0.930000000000000 1.08500000000000 0 665 | -130 0.850000000000000 1.22500000000000 0 666 | -125 0.760000000000000 1.35000000000000 0 667 | -120 0.670000000000000 1.46500000000000 0 668 | -115 0.575000000000000 1.55500000000000 0 669 | -110 0.450000000000000 1.63500000000000 0 670 | -105 0.320000000000000 1.70000000000000 0 671 | -100 0.185000000000000 1.75000000000000 0 672 | -95 0.0500000000000000 1.78000000000000 0 673 | -90 -0.0900000000000000 1.80000000000000 0 674 | -85 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0.0202000000000000 0 695 | -11 -0.997300000000000 0.0183000000000000 0 696 | -10 -0.954100000000000 0.0166000000000000 0 697 | -9 -0.890400000000000 0.0150000000000000 0 698 | -8 -0.815600000000000 0.0136000000000000 0 699 | -7 -0.729100000000000 0.0123000000000000 0 700 | -6 -0.632800000000000 0.0112000000000000 0 701 | -5 -0.550000000000000 0.0102000000000000 0 702 | -4 -0.440000000000000 0.00960000000000000 0 703 | -3 -0.330000000000000 0.00910000000000000 0 704 | -2 -0.220000000000000 0.00880000000000000 0 705 | -1 -0.110000000000000 0.00870000000000000 0 706 | 0 0 0.00850000000000000 0 707 | 1 0.110000000000000 0.00870000000000000 0 708 | 2 0.220000000000000 0.00880000000000000 0 709 | 3 0.330000000000000 0.00910000000000000 0 710 | 4 0.440000000000000 0.00960000000000000 0 711 | 5 0.550000000000000 0.0102000000000000 0 712 | 6 0.632800000000000 0.0112000000000000 0 713 | 7 0.729100000000000 0.0123000000000000 0 714 | 8 0.815600000000000 0.0136000000000000 0 715 | 9 0.890400000000000 0.0150000000000000 0 716 | 10 0.954100000000000 0.0166000000000000 0 717 | 11 0.997300000000000 0.0183000000000000 0 718 | 12 1.02450000000000 0.0202000000000000 0 719 | 13 1.02890000000000 0.0223000000000000 0 720 | 14 1.01750000000000 0.0245000000000000 0 721 | 15 0.993800000000000 0.102000000000000 0 722 | 16 0.964800000000000 0.196000000000000 0 723 | 18 0.915000000000000 0.238000000000000 0 724 | 20 0.887700000000000 0.282000000000000 0 725 | 22 0.886700000000000 0.329000000000000 0 726 | 25 0.932600000000000 0.405000000000000 0 727 | 30 0.855000000000000 0.570000000000000 0 728 | 35 0.980000000000000 0.745000000000000 0 729 | 40 1.03500000000000 0.920000000000000 0 730 | 45 1.05000000000000 1.07500000000000 0 731 | 50 1.02000000000000 1.21500000000000 0 732 | 55 0.955000000000000 1.34500000000000 0 733 | 60 0.875000000000000 1.47000000000000 0 734 | 65 0.760000000000000 1.57500000000000 0 735 | 70 0.630000000000000 1.66500000000000 0 736 | 75 0.500000000000000 1.73500000000000 0 737 | 80 0.365000000000000 1.78000000000000 0 738 | 85 0.230000000000000 1.80000000000000 0 739 | 90 0.0900000000000000 1.80000000000000 0 740 | 95 -0.0500000000000000 1.78000000000000 0 741 | 100 -0.185000000000000 1.75000000000000 0 742 | 105 -0.320000000000000 1.70000000000000 0 743 | 110 -0.450000000000000 1.63500000000000 0 744 | 115 -0.575000000000000 1.55500000000000 0 745 | 120 -0.670000000000000 1.46500000000000 0 746 | 125 -0.760000000000000 1.35000000000000 0 747 | 130 -0.850000000000000 1.22500000000000 0 748 | 135 -0.930000000000000 1.08500000000000 0 749 | 140 -0.980000000000000 0.925000000000000 0 750 | 145 -0.900000000000000 0.755000000000000 0 751 | 150 -0.770000000000000 0.575000000000000 0 752 | 155 -0.670000000000000 0.420000000000000 0 753 | 160 -0.635000000000000 0.320000000000000 0 754 | 165 -0.680000000000000 0.230000000000000 0 755 | 170 -0.850000000000000 0.140000000000000 0 756 | 175 -0.660000000000000 0.0550000000000000 0 757 | 180 0 0.0250000000000000 0 758 | 759 | Reynolds Number: 1e6 760 | BV Dyn. Stall Model - Positive Stall AOA (deg): 6.0 761 | BV Dyn. Stall Model - Negative Stall AOA (deg): -6.0 762 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 763 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.43 764 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.43 765 | AOA (deg) CL CD Cm25 766 | -180 0 0.0250000000000000 0 767 | -175 0.660000000000000 0.0550000000000000 0 768 | -170 0.850000000000000 0.140000000000000 0 769 | -165 0.680000000000000 0.230000000000000 0 770 | -160 0.635000000000000 0.320000000000000 0 771 | -155 0.670000000000000 0.420000000000000 0 772 | -150 0.770000000000000 0.575000000000000 0 773 | -145 0.900000000000000 0.755000000000000 0 774 | -140 0.980000000000000 0.925000000000000 0 775 | -135 0.930000000000000 1.08500000000000 0 776 | -130 0.850000000000000 1.22500000000000 0 777 | -125 0.760000000000000 1.35000000000000 0 778 | -120 0.670000000000000 1.46500000000000 0 779 | -115 0.575000000000000 1.55500000000000 0 780 | -110 0.450000000000000 1.63500000000000 0 781 | -105 0.320000000000000 1.70000000000000 0 782 | -100 0.185000000000000 1.75000000000000 0 783 | -95 0.0500000000000000 1.78000000000000 0 784 | -90 -0.0900000000000000 1.80000000000000 0 785 | -85 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0.0187000000000000 0 806 | -11 -1.02840000000000 0.0170000000000000 0 807 | -10 -0.975100000000000 0.0154000000000000 0 808 | -9 -0.906700000000000 0.0139000000000000 0 809 | -8 -0.825600000000000 0.0126000000000000 0 810 | -7 -0.736200000000000 0.0115000000000000 0 811 | -6 -0.660000000000000 0.0102000000000000 0 812 | -5 -0.550000000000000 0.00950000000000000 0 813 | -4 -0.440000000000000 0.00890000000000000 0 814 | -3 -0.330000000000000 0.00860000000000000 0 815 | -2 -0.220000000000000 0.00830000000000000 0 816 | -1 -0.110000000000000 0.00820000000000000 0 817 | 0 0 0.00820000000000000 0 818 | 1 0.110000000000000 0.00820000000000000 0 819 | 2 0.220000000000000 0.00830000000000000 0 820 | 3 0.330000000000000 0.00860000000000000 0 821 | 4 0.440000000000000 0.00890000000000000 0 822 | 5 0.550000000000000 0.00950000000000000 0 823 | 6 0.660000000000000 0.0102000000000000 0 824 | 7 0.736200000000000 0.0115000000000000 0 825 | 8 0.825600000000000 0.0126000000000000 0 826 | 9 0.906700000000000 0.0139000000000000 0 827 | 10 0.975100000000000 0.0154000000000000 0 828 | 11 1.02840000000000 0.0170000000000000 0 829 | 12 1.06640000000000 0.0187000000000000 0 830 | 13 1.08040000000000 0.0206000000000000 0 831 | 14 1.07930000000000 0.0227000000000000 0 832 | 15 1.06240000000000 0.0251000000000000 0 833 | 16 1.04020000000000 0.108000000000000 0 834 | 18 0.995900000000000 0.238000000000000 0 835 | 20 0.970700000000000 0.282000000000000 0 836 | 22 0.969600000000000 0.329000000000000 0 837 | 25 1.01070000000000 0.405000000000000 0 838 | 30 0.855000000000000 0.570000000000000 0 839 | 35 0.980000000000000 0.745000000000000 0 840 | 40 1.03500000000000 0.920000000000000 0 841 | 45 1.05000000000000 1.07500000000000 0 842 | 50 1.02000000000000 1.21500000000000 0 843 | 55 0.955000000000000 1.34500000000000 0 844 | 60 0.875000000000000 1.47000000000000 0 845 | 65 0.760000000000000 1.57500000000000 0 846 | 70 0.630000000000000 1.66500000000000 0 847 | 75 0.500000000000000 1.73500000000000 0 848 | 80 0.365000000000000 1.78000000000000 0 849 | 85 0.230000000000000 1.80000000000000 0 850 | 90 0.0900000000000000 1.80000000000000 0 851 | 95 -0.0500000000000000 1.78000000000000 0 852 | 100 -0.185000000000000 1.75000000000000 0 853 | 105 -0.320000000000000 1.70000000000000 0 854 | 110 -0.450000000000000 1.63500000000000 0 855 | 115 -0.575000000000000 1.55500000000000 0 856 | 120 -0.670000000000000 1.46500000000000 0 857 | 125 -0.760000000000000 1.35000000000000 0 858 | 130 -0.850000000000000 1.22500000000000 0 859 | 135 -0.930000000000000 1.08500000000000 0 860 | 140 -0.980000000000000 0.925000000000000 0 861 | 145 -0.900000000000000 0.755000000000000 0 862 | 150 -0.770000000000000 0.575000000000000 0 863 | 155 -0.670000000000000 0.420000000000000 0 864 | 160 -0.635000000000000 0.320000000000000 0 865 | 165 -0.680000000000000 0.230000000000000 0 866 | 170 -0.850000000000000 0.140000000000000 0 867 | 175 -0.660000000000000 0.0550000000000000 0 868 | 180 0 0.0250000000000000 0 869 | 870 | Reynolds Number: 2e6 871 | BV Dyn. Stall Model - Positive Stall AOA (deg): 6.0 872 | BV Dyn. Stall Model - Negative Stall AOA (deg): -6.0 873 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 874 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.54 875 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.54 876 | AOA (deg) CL CD Cm25 877 | -180 0 0.0250000000000000 0 878 | -175 0.660000000000000 0.0550000000000000 0 879 | -170 0.850000000000000 0.140000000000000 0 880 | -165 0.680000000000000 0.230000000000000 0 881 | -160 0.635000000000000 0.320000000000000 0 882 | -155 0.670000000000000 0.420000000000000 0 883 | -150 0.770000000000000 0.575000000000000 0 884 | -145 0.900000000000000 0.755000000000000 0 885 | -140 0.980000000000000 0.925000000000000 0 886 | -135 0.930000000000000 1.08500000000000 0 887 | -130 0.850000000000000 1.22500000000000 0 888 | -125 0.760000000000000 1.35000000000000 0 889 | -120 0.670000000000000 1.46500000000000 0 890 | -115 0.575000000000000 1.55500000000000 0 891 | -110 0.450000000000000 1.63500000000000 0 892 | -105 0.320000000000000 1.70000000000000 0 893 | -100 0.185000000000000 1.75000000000000 0 894 | -95 0.0500000000000000 1.78000000000000 0 895 | -90 -0.0900000000000000 1.80000000000000 0 896 | -85 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0 917 | -12 -1.12960000000000 0.0163000000000000 0 918 | -11 -1.07720000000000 0.0148000000000000 0 919 | -10 -1.01110000000000 0.0134000000000000 0 920 | -9 -0.931400000000000 0.0122000000000000 0 921 | -8 -0.843900000000000 0.0111000000000000 0 922 | -7 -0.744900000000000 0.0101000000000000 0 923 | -6 -0.660000000000000 0.00930000000000000 0 924 | -5 -0.550000000000000 0.00870000000000000 0 925 | -4 -0.440000000000000 0.00840000000000000 0 926 | -3 -0.330000000000000 0.00800000000000000 0 927 | -2 -0.220000000000000 0.00780000000000000 0 928 | -1 -0.110000000000000 0.00770000000000000 0 929 | 0 0 0.00770000000000000 0 930 | 1 0.110000000000000 0.00770000000000000 0 931 | 2 0.220000000000000 0.00780000000000000 0 932 | 3 0.330000000000000 0.00800000000000000 0 933 | 4 0.440000000000000 0.00840000000000000 0 934 | 5 0.550000000000000 0.00870000000000000 0 935 | 6 0.660000000000000 0.00930000000000000 0 936 | 7 0.744900000000000 0.0101000000000000 0 937 | 8 0.843900000000000 0.0111000000000000 0 938 | 9 0.931400000000000 0.0122000000000000 0 939 | 10 1.01110000000000 0.0134000000000000 0 940 | 11 1.07720000000000 0.0148000000000000 0 941 | 12 1.12960000000000 0.0163000000000000 0 942 | 13 1.16620000000000 0.0179000000000000 0 943 | 14 1.18130000000000 0.0197000000000000 0 944 | 15 1.18130000000000 0.0218000000000000 0 945 | 16 1.16950000000000 0.0240000000000000 0 946 | 17 1.15500000000000 0.120000000000000 0 947 | 18 1.13830000000000 0.238000000000000 0 948 | 20 1.11720000000000 0.282000000000000 0 949 | 22 1.11270000000000 0.329000000000000 0 950 | 25 1.14680000000000 0.405000000000000 0 951 | 30 0.855000000000000 0.570000000000000 0 952 | 35 0.980000000000000 0.745000000000000 0 953 | 40 1.03500000000000 0.920000000000000 0 954 | 45 1.05000000000000 1.07500000000000 0 955 | 50 1.02000000000000 1.21500000000000 0 956 | 55 0.955000000000000 1.34500000000000 0 957 | 60 0.875000000000000 1.47000000000000 0 958 | 65 0.760000000000000 1.57500000000000 0 959 | 70 0.630000000000000 1.66500000000000 0 960 | 75 0.500000000000000 1.73500000000000 0 961 | 80 0.365000000000000 1.78000000000000 0 962 | 85 0.230000000000000 1.80000000000000 0 963 | 90 0.0900000000000000 1.80000000000000 0 964 | 95 -0.0500000000000000 1.78000000000000 0 965 | 100 -0.185000000000000 1.75000000000000 0 966 | 105 -0.320000000000000 1.70000000000000 0 967 | 110 -0.450000000000000 1.63500000000000 0 968 | 115 -0.575000000000000 1.55500000000000 0 969 | 120 -0.670000000000000 1.46500000000000 0 970 | 125 -0.760000000000000 1.35000000000000 0 971 | 130 -0.850000000000000 1.22500000000000 0 972 | 135 -0.930000000000000 1.08500000000000 0 973 | 140 -0.980000000000000 0.925000000000000 0 974 | 145 -0.900000000000000 0.755000000000000 0 975 | 150 -0.770000000000000 0.575000000000000 0 976 | 155 -0.670000000000000 0.420000000000000 0 977 | 160 -0.635000000000000 0.320000000000000 0 978 | 165 -0.680000000000000 0.230000000000000 0 979 | 170 -0.850000000000000 0.140000000000000 0 980 | 175 -0.660000000000000 0.0550000000000000 0 981 | 180 0 0.0250000000000000 0 982 | 983 | Reynolds Number: 5e6 984 | BV Dyn. Stall Model - Positive Stall AOA (deg): 7.0 985 | BV Dyn. Stall Model - Negative Stall AOA (deg): -7.0 986 | LB Dyn. Stall Model - Lift Coeff. Slope at Zero Lift AOA (per radian): 6.303 987 | LB Dyn. Stall Model - Positive Critical Lift Coeff.: 1.65 988 | LB Dyn. Stall Model - Negative Critical Lift Coeff.: -1.65 989 | AOA (deg) CL CD Cm25 990 | -180 0 0.0250000000000000 0 991 | -175 0.660000000000000 0.0550000000000000 0 992 | -170 0.850000000000000 0.140000000000000 0 993 | -165 0.680000000000000 0.230000000000000 0 994 | -160 0.635000000000000 0.320000000000000 0 995 | -155 0.670000000000000 0.420000000000000 0 996 | -150 0.770000000000000 0.575000000000000 0 997 | -145 0.900000000000000 0.755000000000000 0 998 | -140 0.980000000000000 0.925000000000000 0 999 | -135 0.930000000000000 1.08500000000000 0 1000 | -130 0.850000000000000 1.22500000000000 0 1001 | -125 0.760000000000000 1.35000000000000 0 1002 | -120 0.670000000000000 1.46500000000000 0 1003 | -115 0.575000000000000 1.55500000000000 0 1004 | -110 0.450000000000000 1.63500000000000 0 1005 | -105 0.320000000000000 1.70000000000000 0 1006 | -100 0.185000000000000 1.75000000000000 0 1007 | -95 0.0500000000000000 1.78000000000000 0 1008 | -90 -0.0900000000000000 1.80000000000000 0 1009 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1.02000000000000 1.21500000000000 0 1071 | 55 0.955000000000000 1.34500000000000 0 1072 | 60 0.875000000000000 1.47000000000000 0 1073 | 65 0.760000000000000 1.57500000000000 0 1074 | 70 0.630000000000000 1.66500000000000 0 1075 | 75 0.500000000000000 1.73500000000000 0 1076 | 80 0.365000000000000 1.78000000000000 0 1077 | 85 0.230000000000000 1.80000000000000 0 1078 | 90 0.0900000000000000 1.80000000000000 0 1079 | 95 -0.0500000000000000 1.78000000000000 0 1080 | 100 -0.185000000000000 1.75000000000000 0 1081 | 105 -0.320000000000000 1.70000000000000 0 1082 | 110 -0.450000000000000 1.63500000000000 0 1083 | 115 -0.575000000000000 1.55500000000000 0 1084 | 120 -0.670000000000000 1.46500000000000 0 1085 | 125 -0.760000000000000 1.35000000000000 0 1086 | 130 -0.850000000000000 1.22500000000000 0 1087 | 135 -0.930000000000000 1.08500000000000 0 1088 | 140 -0.980000000000000 0.925000000000000 0 1089 | 145 -0.900000000000000 0.755000000000000 0 1090 | 150 -0.770000000000000 0.575000000000000 0 1091 | 155 -0.670000000000000 0.420000000000000 0 1092 | 160 -0.635000000000000 0.320000000000000 0 1093 | 165 -0.680000000000000 0.230000000000000 0 1094 | 170 -0.850000000000000 0.140000000000000 0 1095 | 175 -0.660000000000000 0.0550000000000000 0 1096 | 180 0 0.0250000000000000 0 1097 | -------------------------------------------------------------------------------- /airfoilData/naca0012_free_format.c81: -------------------------------------------------------------------------------- 1 | # FREE FORMAT 2 | PROFILO NACA 0012 ; 11 39 11 65 9 47 3 | 0 0.2 0.3 0.4 0.5 0.6 0.7 0.75 0.8 0.9 1 4 | -180 0 0 0 0 0 0 0 0 0 0 0 5 | -172.5 0.78 0.78 0.78 0.78 0.78 0.78 0.78 0.78 0.78 0.78 0.78 6 | -161 0.62 0.62 0.62 0.62 0.62 0.62 0.62 0.62 0.62 0.62 0.62 7 | -147 1 1 1 1 1 1 1 1 1 1 1 8 | -129 1 1 1 1 1 1 1 1 1 1 1 9 | -49 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 10 | -39 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 -1.18 11 | -21 -0.8 -0.8 -0.81 -0.83 -0.85 -0.85 -0.85 -0.71 -0.68 -0.64 -0.64 12 | -16.5 -1.007 -1.007 -0.944 -0.96 -0.965 -0.965 -0.965 -0.795 -0.76 -0.7 -0.7 13 | -15 -1.19 -1.19 -1.09 -1.055 -0.99 -0.98 -0.98 -0.83 -0.79 -0.72 -0.72 14 | -14 -1.333 -1.333 -1.22 -1.096 -1 -0.97 -0.97 -0.84 -0.805 -0.73 -0.73 15 | -13 -1.334 -1.334 -1.28 -1.12 -1 -0.96 -0.96 -0.85 -0.815 -0.735 -0.735 16 | -12 -1.255 -1.255 -1.26 -1.13 -1 -0.947 -0.94 -0.85 -0.82 -0.74 -0.74 17 | -11 -1.161 -1.161 -1.19 -1.12 -0.994 -0.93 -0.923 -0.85 -0.81 -0.74 -0.74 18 | -10 -1.055 -1.055 -1.01 -1.082 -0.985 -0.91 -0.9 -0.845 -0.805 -0.73 -0.73 19 | -8 -0.844 -0.844 -0.88 -0.907 -0.922 -0.87 -0.84 -0.82 -0.77 -0.695 -0.695 20 | -6 -0.633 -0.633 -0.66 -0.684 -0.741 -0.77 -0.75 -0.77 -0.72 -0.593 -0.593 21 | -4 -0.422 -0.422 -0.44 -0.456 -0.494 -0.544 -0.578 -0.627 -0.603 -0.396 -0.396 22 | -2 -0.211 -0.211 -0.22 -0.228 -0.247 -0.272 -0.313 -0.35 -0.395 -0.2 -0.2 23 | 0 0 0 0 0 0 0 0 0 0 0 0 24 | 2 0.211 0.211 0.22 0.228 0.247 0.272 0.313 0.35 0.395 0.2 0.2 25 | 4 0.422 0.422 0.44 0.456 0.494 0.544 0.578 0.627 0.603 0.396 0.396 26 | 6 0.633 0.633 0.66 0.684 0.741 0.77 0.75 0.77 0.72 0.593 0.593 27 | 8 0.844 0.844 0.88 0.907 0.922 0.87 0.84 0.82 0.77 0.695 0.695 28 | 10 1.055 1.055 1.1 1.082 0.985 0.91 0.9 0.845 0.805 0.73 0.73 29 | 11 1.161 1.161 1.19 1.12 0.994 0.93 0.923 0.85 0.81 0.74 0.74 30 | 12 1.255 1.255 1.26 1.13 1 0.947 0.94 0.85 0.82 0.74 0.74 31 | 13 1.334 1.334 1.28 1.12 1 0.96 0.96 0.85 0.815 0.735 0.735 32 | 14 1.333 1.333 1.22 1.096 1 0.97 0.97 0.84 0.805 0.73 0.73 33 | 15 1.19 1.19 1.09 1.055 0.99 0.98 0.98 0.83 0.79 0.73 0.73 34 | 16.5 1.007 1.007 0.944 0.96 0.965 0.965 0.965 0.795 0.76 0.7 0.7 35 | 21 0.8 0.8 0.81 0.83 0.85 0.85 0.85 0.71 0.68 0.64 0.64 36 | 39 1.18 1.18 1.18 1.18 1.18 1.18 1.18 1.18 1.18 1.18 1.18 37 | 49 1.18 1.18 1.18 1.18 1.18 1.18 1.18 1.18 1.18 1.18 1.18 38 | 129 -1 -1 -1 -1 -1 -1 -1 -1 -1 -1 -1 39 | 147 -1 -1 -1 -1 -1 -1 -1 -1 -1 -1 -1 40 | 161 -0.62 -0.62 -0.62 -0.62 -0.62 -0.62 -0.62 -0.62 -0.62 -0.62 -0.62 41 | 172.5 -0.78 -0.78 -0.78 -0.78 -0.78 -0.78 -0.78 -0.78 -0.78 -0.78 -0.78 42 | 180 0 0 0 0 0 0 0 0 0 0 0 43 | 0 0.2 0.3 0.4 0.5 0.6 0.7 0.75 0.8 0.9 1 44 | -180 0.022 0.022 0.022 0.022 0.022 0.022 0.022 0.022 0.022 0.022 0.022 45 | -175 0.062 0.062 0.062 0.062 0.062 0.062 0.062 0.062 0.062 0.062 0.062 46 | -170 0.132 0.132 0.132 0.132 0.132 0.132 0.132 0.132 0.132 0.132 0.132 47 | -165 0.242 0.242 0.242 0.242 0.242 0.242 0.242 0.242 0.242 0.242 0.242 48 | -160 0.302 0.302 0.302 0.302 0.302 0.302 0.302 0.302 0.302 0.302 0.302 49 | -140 1.042 1.042 1.042 1.042 1.042 1.042 1.042 1.042 1.042 1.042 1.042 50 | -120 1.652 1.652 1.652 1.652 1.652 1.652 1.652 1.652 1.652 1.652 1.652 51 | -110 1.852 1.852 1.852 1.852 1.852 1.852 1.852 1.852 1.852 1.852 1.852 52 | -100 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 53 | -90 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 54 | -80 1.962 1.962 1.962 1.962 1.962 1.962 1.962 1.962 1.962 1.962 1.962 55 | -70 1.842 1.842 1.842 1.842 1.842 1.842 1.842 1.842 1.842 1.842 1.842 56 | -60 1.662 1.662 1.662 1.662 1.662 1.662 1.662 1.662 1.662 1.662 1.662 57 | -50 1.392 1.392 1.392 1.392 1.392 1.399 1.392 1.392 1.392 1.392 1.392 58 | -30 0.562 0.562 0.562 0.562 0.562 0.562 0.562 0.562 0.562 0.562 0.562 59 | -21 0.332 0.332 0.332 0.332 0.332 0.332 0.332 0.332 0.332 0.332 0.332 60 | -16 0.155 0.155 0.181 0.207 0.235 0.257 0.274 0.292 0.305 0.342 0.342 61 | -15 0.102 0.102 0.148 0.181 0.209 0.233 0.252 0.271 0.282 0.298 0.298 62 | -14 0.038 0.038 0.099 0.146 0.18 0.212 0.233 0.249 0.26 0.293 0.293 63 | -13 0.0264 0.0264 0.0455 0.094 0.148 0.191 0.216 0.231 0.239 0.272 0.292 64 | -12 0.022 0.022 0.03 0.06 0.111 0.164 0.198 0.211 0.22 0.252 0.291 65 | -11 0.0196 0.0196 0.0232 0.038 0.078 0.135 0.17 0.192 0.202 0.232 0.275 66 | -10 0.0174 0.0174 0.0189 0.0259 0.053 0.105 0.145 0.176 0.186 0.213 0.254 67 | -9 0.0154 0.0154 0.0159 0.0187 0.0351 0.077 0.122 0.159 0.172 0.199 0.232 68 | -8 0.0138 0.0138 0.0138 0.0147 0.022 0.053 0.101 0.14 0.155 0.183 0.214 69 | -7 0.0122 0.0122 0.0122 0.0123 0.0141 0.035 0.082 0.111 0.139 0.169 0.192 70 | -6 0.011 0.011 0.011 0.011 0.011 0.0212 0.0615 0.082 0.12 0.14 0.17 71 | -5 0.01 0.01 0.01 0.01 0.01 0.0132 0.038 0.054 0.048 0.111 0.14 72 | -4 0.0093 0.0093 0.0093 0.0093 0.0093 0.01 0.0167 0.03 0.0575 0.095 0.112 73 | -3 0.0088 0.0088 0.0088 0.0088 0.0088 0.009 0.0102 0.0175 0.0355 0.086 0.102 74 | -2 0.0085 0.0085 0.0085 0.0085 0.0085 0.0085 0.0086 0.0117 0.024 0.081 0.098 75 | -1 0.0083 0.0083 0.0083 0.0083 0.0083 0.0083 0.0083 0.0091 0.0175 0.078 0.096 76 | 0 0.008 0.008 0.008 0.008 0.008 0.008 0.008 0.008 0.0137 0.078 0.095 77 | 1 0.0083 0.0083 0.0083 0.0083 0.0083 0.0083 0.0083 0.0091 0.0175 0.078 0.096 78 | 2 0.0085 0.0085 0.0085 0.0085 0.0085 0.0085 0.0086 0.0117 0.024 0.081 0.098 79 | 3 0.0088 0.0088 0.0088 0.0088 0.0088 0.009 0.0102 0.0175 0.0355 0.086 0.102 80 | 4 0.0093 0.0093 0.0093 0.0093 0.0093 0.01 0.0167 0.03 0.0575 0.095 0.112 81 | 5 0.01 0.01 0.01 0.01 0.01 0.0132 0.038 0.054 0.048 0.111 0.14 82 | 6 0.011 0.011 0.011 0.011 0.011 0.0212 0.0615 0.082 0.12 0.14 0.17 83 | 7 0.0122 0.0122 0.0122 0.0123 0.0141 0.035 0.082 0.111 0.139 0.169 0.192 84 | 8 0.0138 0.0138 0.0138 0.0147 0.022 0.053 0.101 0.14 0.155 0.183 0.214 85 | 9 0.0154 0.0154 0.0159 0.0187 0.0351 0.077 0.122 0.159 0.172 0.199 0.232 86 | 10 0.0174 0.0174 0.0189 0.0259 0.053 0.105 0.145 0.176 0.186 0.213 0.254 87 | 11 0.0196 0.0196 0.0232 0.038 0.078 0.135 0.17 0.192 0.202 0.232 0.275 88 | 12 0.022 0.022 0.03 0.06 0.111 0.164 0.198 0.211 0.22 0.252 0.291 89 | 13 0.0264 0.0264 0.0455 0.094 0.148 0.191 0.216 0.231 0.239 0.272 0.292 90 | 14 0.038 0.038 0.099 0.146 0.18 0.212 0.233 0.249 0.26 0.293 0.293 91 | 15 0.102 0.102 0.148 0.181 0.209 0.233 0.252 0.271 0.282 0.298 0.298 92 | 16 0.155 0.155 0.181 0.207 0.235 0.257 0.274 0.292 0.305 0.342 0.342 93 | 21 0.332 0.332 0.332 0.332 0.332 0.332 0.332 0.332 0.332 0.332 0.332 94 | 30 0.562 0.562 0.562 0.562 0.562 0.562 0.562 0.562 0.562 0.562 0.562 95 | 50 1.392 1.392 1.392 1.392 1.392 1.392 1.392 1.392 1.392 1.392 1.392 96 | 60 1.662 1.662 1.662 1.662 1.662 1.662 1.662 1.662 1.662 1.662 1.662 97 | 70 1.842 1.842 1.842 1.842 1.842 1.842 1.842 1.842 1.842 1.842 1.842 98 | 80 1.962 1.962 1.962 1.962 1.962 1.962 1.962 1.962 1.962 1.962 1.962 99 | 90 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 100 | 100 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 2.022 101 | 110 1.852 1.852 1.852 1.852 1.852 1.852 1.852 1.852 1.852 1.852 1.852 102 | 120 1.652 1.652 1.652 1.652 1.652 1.652 1.652 1.652 1.652 1.652 1.652 103 | 140 1.042 1.042 1.042 1.042 1.042 1.042 1.042 1.042 1.042 1.042 1.042 104 | 160 0.302 0.302 0.302 0.302 0.302 0.302 0.302 0.302 0.302 0.302 0.302 105 | 165 0.242 0.242 0.242 0.242 0.242 0.242 0.242 0.242 0.242 0.242 0.242 106 | 170 0.132 0.132 0.132 0.132 0.132 0.132 0.132 0.132 0.132 0.132 0.132 107 | 175 0.062 0.062 0.062 0.062 0.062 0.062 0.062 0.062 0.062 0.062 0.062 108 | 180 0.022 0.022 0.022 0.022 0.022 0.022 0.022 0.022 0.022 0.022 0.022 109 | 0.2 0.3 0.4 0.5 0.6 0.7 0.75 0.8 0.9 110 | -180 0 0 0 0 0 0 0 0 0 111 | -170 0.4 0.4 0.4 0.4 0.4 0.4 0.4 0.4 0.4 112 | -165 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 113 | -160 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 114 | -135 0.5 0.5 0.5 0.5 0.5 0.5 0.5 0.5 0.5 115 | -90 0.5 0.5 0.5 0.5 0.5 0.5 0.5 0.5 0.5 116 | -30 0.174 0.184 0.196 0.214 0.235 0.25 0.264 0.277 0.298 117 | -23 0.112 0.118 0.128 0.144 0.157 0.171 0.183 0.206 0.232 118 | -16 0.073 0.078 0.086 0.097 0.108 0.117 0.137 0.176 0.2 119 | -15 0.054 0.065 0.073 0.084 0.097 0.111 0.133 0.173 0.195 120 | -14 0 0.027 0.054 0.068 0.086 0.103 0.127 0.167 0.189 121 | -13 0 0.0015 0.025 0.05 0.074 0.093 0.122 0.163 0.184 122 | -12 0 0 0.002 0.03 0.06 0.083 0.116 0.157 0.176 123 | -11 0 0 -0.003 0.014 0.046 0.074 0.108 0.149 0.17 124 | -10 0 0 -0.0015 0.002 0.032 0.065 0.1 0.142 0.163 125 | -9 0 0 0 -0.003 0.016 0.054 0.089 0.132 0.154 126 | -8 0 0 0 -0.004 0.005 0.041 0.082 0.123 0.145 127 | -7 0 0 0 0 -0.004 0.0275 0.072 0.1125 0.136 128 | -6 0 0 0 0 -0.003 0.016 0.0625 0.1 0.125 129 | -4 0 0 0 0 0 0.005 0.04 0.076 0.102 130 | -3 0 0 0 0 0 -0.0025 0.026 0.0665 0.087 131 | -2 0 0 0 0 0 0 0.013 0.053 0.07 132 | -1 0 0 0 0 0 0 0.0035 0.033 0.045 133 | 0 0 0 0 0 0 0 0 0 0 134 | 1 0 0 0 0 0 0 -0.0035 -0.033 -0.045 135 | 2 0 0 0 0 0 0 -0.013 -0.053 -0.07 136 | 3 0 0 0 0 0 0.0025 -0.026 -0.0665 -0.087 137 | 4 0 0 0 0 0 -0.005 -0.04 -0.076 -0.102 138 | 6 0 0 0 0 0.003 -0.016 -0.0625 -0.1 -0.125 139 | 7 0 0 0 0 0.004 -0.0275 -0.072 -0.1125 -0.136 140 | 8 0 0 0 0.004 -0.005 -0.041 -0.082 -0.123 -0.145 141 | 9 0 0 0 0.003 -0.016 -0.054 -0.089 -0.132 -0.154 142 | 10 0 0 0.0015 -0.002 -0.032 -0.065 -0.1 -0.142 -0.163 143 | 11 0 0 0.003 -0.014 -0.046 -0.074 -0.108 -0.149 -0.17 144 | 12 0 0 -0.002 -0.03 -0.06 -0.083 -0.116 -0.157 -0.176 145 | 13 0 -0.0015 -0.025 -0.05 -0.074 -0.093 -0.122 -0.163 -0.184 146 | 14 0 -0.027 -0.054 -0.068 -0.086 -0.103 -0.127 -0.167 -0.189 147 | 15 -0.054 -0.065 -0.073 -0.084 -0.097 -0.111 -0.133 -0.173 -0.195 148 | 16 -0.073 -0.078 -0.086 -0.097 -0.108 -0.117 -0.137 -0.176 -0.2 149 | 23 -0.112 -0.118 -0.128 -0.144 -0.157 -0.171 -0.183 -0.206 -0.232 150 | 30 -0.174 -0.184 -0.196 -0.214 -0.235 -0.25 -0.264 -0.277 -0.298 151 | 90 -0.5 -0.5 -0.5 -0.5 -0.5 -0.5 -0.5 -0.5 -0.5 152 | 135 -0.5 -0.5 -0.5 -0.5 -0.5 -0.5 -0.5 -0.5 -0.5 153 | 160 -0.3 -0.3 -0.3 -0.3 -0.3 -0.3 -0.3 -0.3 -0.3 154 | 165 -0.3 -0.3 -0.3 -0.3 -0.3 -0.3 -0.3 -0.3 -0.3 155 | 170 -0.4 -0.4 -0.4 -0.4 -0.4 -0.4 -0.4 -0.4 -0.4 156 | 180 0 0 0 0 0 0 0 0 0 157 | -------------------------------------------------------------------------------- /airfoilData/sandiaImport/NACA_0012_Re1e6.dat: -------------------------------------------------------------------------------- 1 | Reynolds Number: 1e6 NACA 0012 SECTION DATA. EPPLER MODEL, CL. CD. DEC78, data from Sandia report, ocr by Louis Gagnon from "Aerodynamic characteristics of seven symmetrical airfoil sections through 180-degree angle of attack for use in aerodynamic analysis of vertical axis wind turbines" Sheldahl, R E ; Klimas, P C 2 | 0.0000 0.0000 .0065 3 | 1.0000 .1100 .0066 4 | 2.0000 .2200 .0068 5 | 3.0000 .3300 .0071 6 | 4.0000 .4400 .0078 7 | 5.0000 .5500 .0091 8 | 6.0000 .5500 .0101 9 | 7.0000 .7700 .0110 10 | 8.0000 .8800 .0119 11 | 9.0000 .9661 .0134 12 | 10.0000 1.0512 .0147 13 | 11.0000 1.1097 .0162 14 | 12.0000 1.1212 .0180 15 | 13.0000 1.0487 .0200 16 | 14.0000 .8846 .0222 17 | 15.0000 .7108 .0245 18 | 16.0000 .6060 .1280 19 | 17.0000 .5906 .2310 20 | 18.0000 .6030 .2520 21 | 19.0000 .6334 .2740 22 | 20.0000 .6716 .2970 23 | 21.0000 .7162 .3200 24 | 22.0000 .7613 .3440 25 | 23.0000 .8097 .3690 26 | 24.0000 .8589 .3940 27 | 25.0000 .9093 .4200 28 | 26.0000 .9618 .4460 29 | 27.0000 1.0144 .4730 30 | 30.0000 .9150 .5700 31 | 35.0000 1.0200 .7450 32 | 40.0000 1.0750 .9200 33 | 45.0000 1.0850 1.0750 34 | 50.0000 1.0400 1.2150 35 | 55.0000 .9650 1.3450 36 | 60.0000 .8750 1.4700 37 | 65.0000 .7650 1.5750 38 | 70.0000 .6500 1.6650 39 | 75.0000 .5150 1.7350 40 | 80.0000 .3700 1.7800 41 | 85.0000 .2200 1.8000 42 | 90.0000 .0700 1.8000 43 | 95.0000 -.0700 1.7800 44 | 100.0000 -.2200 1.7500 45 | 105.0000 -.3700 1.7000 46 | 110.0000 -.5100 1.6350 47 | 115.0000 -.6250 1.5550 48 | 120.0000 -.7350 1.4650 49 | 125.0000 -.8400 1.3500 50 | 130.0000 -.9100 1.2250 51 | 135.0000 -.9450 1.0850 52 | 140.0000 -.9450 .9250 53 | 145.0000 -.9100 .7550 54 | 150.0000 -.8500 .5750 55 | 155.0000 -.7400 .4200 56 | 160.0000 -.6600 .3200 57 | 165.0000 -.6750 .2300 58 | 170.0000 -.8500 .1400 59 | 175.0000 -.6900 .0550 60 | 180.0000 0.0000 .0250 61 | -------------------------------------------------------------------------------- /airfoilData/sandiaImport/NACA_0012_Re1e7.dat: -------------------------------------------------------------------------------- 1 | Reynolds Number: 1e7 NACA 0012 SECTION DATA. EPPLER MODEL, CL. CD. DEC78, data from Sandia report, ocr by Louis Gagnon from "Aerodynamic characteristics of seven symmetrical airfoil sections through 180-degree angle of attack for use in aerodynamic analysis of vertical axis wind turbines" Sheldahl, R E ; Klimas, P C 2 | 0.0000 0.0000 .0064 3 | 1.0000 .1100 .0064 4 | 2.0000 .2200 .0066 5 | 3.0000 .3300 .0068 6 | 4.0000 .4400 .0071 7 | 5.0000 .5500 .0074 8 | 6.0000 .6600 .0078 9 | 7.0000 .7700 .0082 10 | 8.0000 .8800 .0086 11 | 9.0000 .9900 .0091 12 | 10.0000 1.1000 .0097 13 | 11.0000 1.2100 .0104 14 | 12.0000 1.2906 .0116 15 | 13.0000 1.3687 .0127 16 | 14.0000 1.4171 .0141 17 | 15.0000 1.4214 .0157 18 | 16.0000 1.2941 .0182 19 | 17.0000 1.1200 .0210 20 | 18.0000 .9795 .0241 21 | 19.0000 .8983 .1610 22 | 20.0000 .8668 .2970 23 | 21.0000 .8665 .3200 24 | 22.0000 .8859 .3440 25 | 23.0000 .9151 .3690 26 | 24.0000 .9492 .3940 27 | 25.0000 .9927 .4200 28 | 26.0000 1.0371 .4460 29 | 27.0000 1.0833 .4730 30 | 30.0000 .9150 .5700 31 | 35.0000 1.0200 .7450 32 | 40.0000 1.0750 .9200 33 | 45.0000 1.0850 1.0750 34 | 50.0000 1.0400 1.2150 35 | 55.0000 .9650 1.3450 36 | 60.0000 .8750 1.4700 37 | 65.0000 .7650 1.5750 38 | 70.0000 .6500 1.6650 39 | 75.0000 .5150 1.7350 40 | 80.0000 .3700 1.7800 41 | 85.0000 .2200 1.8000 42 | 90.0000 .0700 1.8000 43 | 95.0000 -.0700 1.7800 44 | 100.0000 -.2200 1.7500 45 | 105.0000 -.3700 1.7000 46 | 110.0000 -.5100 1.6350 47 | 115.0000 -.6250 1.5550 48 | 120.0000 -.7350 1.4650 49 | 125.0000 -.8400 1.3500 50 | 130.0000 -.9100 1.2250 51 | 135.0000 -.9450 1.0850 52 | 140.0000 -.9450 .9250 53 | 145.0000 -.9100 .7550 54 | 150.0000 -.8500 .5750 55 | 155.0000 -.7400 .4200 56 | 160.0000 -.6600 .3200 57 | 165.0000 -.6750 .2300 58 | 170.0000 -.8500 .1400 59 | 175.0000 -.6900 .0550 60 | 180.0000 0.0000 .0250 61 | -------------------------------------------------------------------------------- /airfoilData/testNACA.blend: -------------------------------------------------------------------------------- https://raw.githubusercontent.com/fossasia/Codeheat/25eeca8d18eaf08c8a1b65618ca5777c752e37f8/airfoilData/testNACA.blend -------------------------------------------------------------------------------- /manualImages/README.md: -------------------------------------------------------------------------------- 1 | # mbdyn-manualImages 2 | 3 | Task description for the creation of new images for the MBDyn manual and/or website. 4 | 5 | 6 | 1. Consult the latest version of the manual, taken from the private CVS and uploaded here: input.pdf, to see how cardano.256.png, inline.256.png, revHinge.256.png, and spherHinge.256.png were included in the manual (p.225, 240, 248, and 255) 7 | 8 | 2. find an element for which an image would be beneficial; chose a common filename root for your new element (ie: cardano, revHinge, ...); for the instructions here we'll use "yourFile" 9 | 10 | 3. starting from the revolute.blend Blender file, of which the layers are explained in revolute.txt, create your own element image making sure you respect the element description given in the manual; save the modified Blender file with a new name (yourFile.blend) 11 | 12 | 4. render the element in png, regenerate the color palette to use 256 colors (GIMP recommended [Menu: Image->Mode->Indexed]), trim the image to remove any white borders (GIMP recommended [Menu: Image->Autotrim]) 13 | 14 | 5. convert the modified generated png into an eps3 file using the following command: `convert yourFile.png eps3:yourFile.eps` 15 | 16 | 6. submit the generated files: yourFile.blend, yourFile.png, and yourFile.eps; the eps and png files should not exceed 100k each 17 | -------------------------------------------------------------------------------- /manualImages/cardano.256.png: -------------------------------------------------------------------------------- https://raw.githubusercontent.com/fossasia/Codeheat/25eeca8d18eaf08c8a1b65618ca5777c752e37f8/manualImages/cardano.256.png -------------------------------------------------------------------------------- /manualImages/inline.256.png: -------------------------------------------------------------------------------- https://raw.githubusercontent.com/fossasia/Codeheat/25eeca8d18eaf08c8a1b65618ca5777c752e37f8/manualImages/inline.256.png -------------------------------------------------------------------------------- /manualImages/input.pdf: -------------------------------------------------------------------------------- https://raw.githubusercontent.com/fossasia/Codeheat/25eeca8d18eaf08c8a1b65618ca5777c752e37f8/manualImages/input.pdf -------------------------------------------------------------------------------- /manualImages/revHinge.256.png: -------------------------------------------------------------------------------- https://raw.githubusercontent.com/fossasia/Codeheat/25eeca8d18eaf08c8a1b65618ca5777c752e37f8/manualImages/revHinge.256.png -------------------------------------------------------------------------------- /manualImages/revolute.blend: -------------------------------------------------------------------------------- https://raw.githubusercontent.com/fossasia/Codeheat/25eeca8d18eaf08c8a1b65618ca5777c752e37f8/manualImages/revolute.blend -------------------------------------------------------------------------------- /manualImages/revolute.txt: -------------------------------------------------------------------------------- 1 | Layers 1 & 2: revolute hinge 2 | Layers 3 & 4: sperical hinge 3 | Layers 5 & 6: cardano hinge 4 | Layers 7 & 8: in line joint 5 | Layer 11: camera and light 6 | Layer 12: spare parts 7 | 8 | -------------------------------------------------------------------------------- /manualImages/spherHinge.256.png: -------------------------------------------------------------------------------- https://raw.githubusercontent.com/fossasia/Codeheat/25eeca8d18eaf08c8a1b65618ca5777c752e37f8/manualImages/spherHinge.256.png --------------------------------------------------------------------------------