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Merged
RyanDavies19 merged 4 commits into from
Jun 4, 2025
Merged

Add an Example Directory #311

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aa1842c
Add example folder from WPTO software demo days
RyanDavies19 May 23, 2025
8aa0208
Improve README, clean up for PR
RyanDavies19 Jun 3, 2025
3607452
Fix broken image reference
RyanDavies19 Jun 3, 2025
1fe3275
Add OpenFAST r-test license
RyanDavies19 Jun 3, 2025
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560 changes: 560 additions & 0 deletions example/MHK_RM1_Floating/Airfoils/NACA6_0240.dat
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47 changes: 47 additions & 0 deletions example/MHK_RM1_Floating/Airfoils/NACA6_0240_coords.txt
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Original file line number Diff line number Diff line change
@@ -0,0 +1,47 @@
40 NumCoords ! The number of coordinates in the airfoil shape file (including an extra coordinate for airfoil reference). Set to zero if coordinates not included.
! ......... x-y coordinates are next if NumCoords > 0 .............
! x-y coordinate of airfoil reference
! x/c y/c
0.25 0
! coordinates of airfoil shape
! NACA6_0240 Airfoil
! x/c y/c
0.000000 0.000000
0.001740 0.009990
0.009990 0.025540
0.026840 0.043840
0.085380 0.081830
0.126020 0.098890
0.173070 0.113700
0.225630 0.125450
0.343100 0.136890
0.405650 0.135010
0.469030 0.128320
0.532130 0.117850
0.653880 0.089820
0.711010 0.074320
0.764750 0.059150
0.814500 0.045100
0.899560 0.022380
0.933650 0.014140
0.961390 0.007980
0.982280 0.002440
0.982280 0.001830
0.961390 0.002090
0.933510 0.000850
0.859090 -0.008040
0.813820 -0.016050
0.764090 -0.026350
0.710600 -0.038510
0.594970 -0.065500
0.534160 -0.078430
0.472340 -0.089680
0.410300 -0.098140
0.289530 -0.102840
0.233070 -0.098960
0.180640 -0.091900
0.133180 -0.082080
0.056790 -0.055970
0.029750 -0.040380
0.011270 -0.024430
0.000000 0.000000
560 changes: 560 additions & 0 deletions example/MHK_RM1_Floating/Airfoils/NACA6_0247.dat
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47 changes: 47 additions & 0 deletions example/MHK_RM1_Floating/Airfoils/NACA6_0247_coords.txt
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Original file line number Diff line number Diff line change
@@ -0,0 +1,47 @@
40 NumCoords ! The number of coordinates in the airfoil shape file (including an extra coordinate for airfoil reference). Set to zero if coordinates not included.
! ......... x-y coordinates are next if NumCoords > 0 .............
! x-y coordinate of airfoil reference
! x/c y/c
0.25 0
! coordinates of airfoil shape
! NACA6_0247 Airfoil
! x/c y/c
0.000000 0.000000
0.006819 0.021573
0.027091 0.045571
0.060263 0.070519
0.105430 0.093593
0.161359 0.113695
0.226526 0.129332
0.299152 0.139084
0.377257 0.140958
0.458710 0.134375
0.541290 0.120926
0.622743 0.102688
0.700848 0.081979
0.773474 0.061268
0.838641 0.042604
0.894570 0.027238
0.939737 0.015604
0.972909 0.007552
0.993181 0.002511
1.000000 0.000000
0.993181 -0.000009
0.972909 0.000021
0.939737 -0.001786
0.894570 -0.006851
0.838641 -0.015998
0.773474 -0.029320
0.700848 -0.046093
0.622743 -0.064559
0.541290 -0.082348
0.458710 -0.096978
0.377257 -0.106009
0.299152 -0.107583
0.226526 -0.102345
0.161359 -0.091881
0.105430 -0.077436
0.060263 -0.059906
0.027091 -0.040088
0.006819 -0.019333
0.000000 0.000000
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