DFSM updates

examples/01_aeroelasticse/OpenFAST_models/RM1/Airfoils/NACA6_0240_coords.txt

@@ -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

examples/01_aeroelasticse/OpenFAST_models/RM1/Airfoils/NACA6_0247_coords.txt

@@ -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