Examples

.gitignore

@@ -12,3 +12,4 @@ new*
 *COMPILED*
 *.out
 *.h5
+*.mat

app/OWENS_APP/src/data/NuMAD_Geom_SNL_5MW_D_Carbon_LCDT_ThickFoils_ThinSkin.csv

@@ -1,24 +1,24 @@
 SNL_5MW_D_Carbon_LCDT,,,,# Shear webs ->,1,# of stacks ->,7,Stack ID ->,1,2,3,4,5,6,7,Segment ID ->,1,2,3,4,5,6,7,8,9,10,11,12,DP Types,1,2,3,4,5,6,7,8,9,10,11,12,1,2,3,4,5,6,7,8,9,10,11,12,,
 ,,,,,,# of segments ->,12,Material ID ->,1,2,4,1,1,2,4,,,,,,,,,,,,,,,,,,,,,,,,,,,first entry in the CSV list is the exterior blade surface stack,,,,,,,,,,,,SW1,
 Sta.#,Blade span (m),Airfoil Shape File,TE Type,Twist (deg),Chord,xoffset,aero center,Section Label,LE,Panel_Face,Panel_Core,Spar,TE,SW_Face,SW_Core,-blank-,HP_TE,HP_Aft_Panel,HP_Aft_Spar,HP_Fore_Spar,HP_Fore_Panel,HP_LE,LP_LE,LP_Fore_Panel,LP_Aft_Spar,LP_Fore_Spar,LP_Aft_Panel,LP_TE,,,,,,,,,,,,,,HP_TE,HP_Aft_Panel,HP_Aft_Spar,HP_Fore_Spar,HP_Fore_Panel,HP_LE,LP_LE,LP_Fore_Panel,LP_Aft_Spar,LP_Fore_Spar,LP_Aft_Panel,LP_TE,stacks,dps
-1,0,TUD_42,sharp,0,6,0.3,0.2,,12,1,8,12,12,1,8,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-2,6.607,TUD_42,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-3,13.215,TUD_42,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-4,19.822,TUD_42,sharp,0,5.498,0.3,0.2,,11,1,8,12,11,1,8,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-5,26.43,TUD_42,sharp,0,4.431,0.3,0.2,,9,1,7,10,9,1,7,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-6,33.037,TUD_42,sharp,0,3.806,0.3,0.2,,8,1,6,8,8,1,6,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-7,39.645,TUD_42,sharp,0,3.435,0.3,0.2,,7,1,5,8,7,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-8,46.252,TUD_42,sharp,0,3.205,0.3,0.2,,6,1,5,7,6,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-9,52.859,TUD_42,sharp,0,3.068,0.3,0.2,,6,1,5,7,6,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-10,59.467,TUD_42,sharp,0,3.003,0.3,0.2,,6,1,4,7,6,1,4,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-11,66.074,TUD_42,sharp,0,3,0.3,0.2,,6,1,4,7,6,1,4,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-12,72.682,TUD_42,sharp,0,3.056,0.3,0.2,,6,1,4,7,6,1,4,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-13,79.289,TUD_42,sharp,0,3.176,0.3,0.2,,6,1,5,7,6,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-14,85.896,TUD_42,sharp,0,3.377,0.3,0.2,,7,1,5,8,7,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-15,92.504,TUD_42,sharp,0,3.688,0.3,0.2,,7,1,5,8,7,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-16,99.111,TUD_42,sharp,0,4.18,0.3,0.2,,8,1,6,9,8,1,6,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-17,105.719,TUD_42,sharp,0,4.924,0.3,0.2,,10,1,7,11,10,1,7,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-18,112.326,TUD_42,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-19,118.934,TUD_42,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-20,125.541,TUD_42,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
-21,132.148,TUD_42,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+1,0,NACA_0021,sharp,0,6,0.3,0.2,,12,1,8,12,12,1,8,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+2,6.607,NACA_0021,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+3,13.215,NACA_0021,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+4,19.822,NACA_0021,sharp,0,5.498,0.3,0.2,,11,1,8,12,11,1,8,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+5,26.43,NACA_0021,sharp,0,4.431,0.3,0.2,,9,1,7,10,9,1,7,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+6,33.037,NACA_0021,sharp,0,3.806,0.3,0.2,,8,1,6,8,8,1,6,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+7,39.645,NACA_0021,sharp,0,3.435,0.3,0.2,,7,1,5,8,7,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+8,46.252,NACA_0021,sharp,0,3.205,0.3,0.2,,6,1,5,7,6,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+9,52.859,NACA_0021,sharp,0,3.068,0.3,0.2,,6,1,5,7,6,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+10,59.467,NACA_0021,sharp,0,3.003,0.3,0.2,,6,1,4,7,6,1,4,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+11,66.074,NACA_0021,sharp,0,3,0.3,0.2,,6,1,4,7,6,1,4,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+12,72.682,NACA_0021,sharp,0,3.056,0.3,0.2,,6,1,4,7,6,1,4,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+13,79.289,NACA_0021,sharp,0,3.176,0.3,0.2,,6,1,5,7,6,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+14,85.896,NACA_0021,sharp,0,3.377,0.3,0.2,,7,1,5,8,7,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+15,92.504,NACA_0021,sharp,0,3.688,0.3,0.2,,7,1,5,8,7,1,5,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+16,99.111,NACA_0021,sharp,0,4.18,0.3,0.2,,8,1,6,9,8,1,6,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+17,105.719,NACA_0021,sharp,0,4.924,0.3,0.2,,10,1,7,11,10,1,7,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+18,112.326,NACA_0021,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+19,118.934,NACA_0021,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+20,125.541,NACA_0021,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"
+21,132.148,NACA_0021,sharp,0,6,0.3,0.2,,12,1,9,13,12,1,9,-1,-0.95,-0.5,-0.3,-0.1,-0.095,0,0.095,0.1,0.3,0.5,0.95,1,,,,,,,,,,,,,,"2,5,2","2,3,2","2,4,2","2,4,2","2,3,2","2,1,2","2,1,2","2,3,2","2,4,2","2,4,2","2,3,2","2,5,2","6,7,6","9,3,3,9"

docs/src/literate/C_customizablePreprocessing.jl

@@ -405,18 +405,25 @@ if !AD15On
     #########################################
     ### Set up aero forces
     #########################################
-    chord_spl = FLOWMath.akima(numadIn_bld.span./maximum(numadIn_bld.span), numadIn_bld.chord,LinRange(0,1,Nslices))
-
-    T1 = round(Int,(5.8/H)*Nslices)
-    T2 = round(Int,(11.1/H)*Nslices)
-    T3 = round(Int,(29.0/H)*Nslices)
-    T4 = round(Int,(34.7/H)*Nslices)
-    airfoils = fill("$(path)/airfoils/NACA_0021.dat",Nslices)
-    airfoils[T1:T4] .= "$(path)/airfoils/Sandia_001850.dat"
+    ### translate from blade span to blade height between the numad definition and the vertical slice positions
+    ### First get the angles from the overall geometry npoints and go to the numad npoints
+    delta_xs = shapeX[2:end] - shapeX[1:end-1]
+    delta_zs = shapeY[2:end] - shapeY[1:end-1]
+    delta3D = atan.(delta_xs./delta_zs)
+    delta3D_spl = FLOWMath.akima(shapeY[1:end-1]./maximum(shapeY[1:end-1]), delta3D,LinRange(0,1,length(numadIn_bld.span)-1))
 
-    chord = fill(1.22,Nslices) #TODO: link chord to numad and height as opposed to span
-    chord[T1:T4] .= 1.07
-    chord[T2:T3] .= 0.9191
+    bld_height_numad = cumsum(diff(numadIn_bld.span).*(1.0.-abs.(sin.(delta3D_spl)))) # now convert the numad span to a height
+
+    chord = FLOWMath.akima(bld_height_numad./maximum(bld_height_numad), numadIn_bld.chord,LinRange(0,1,Nslices)) # now we can use it to access the numad data 
+    airfoils = fill("nothing",Nslices)
+
+    for (iheight_numad,height_numad) in enumerate(bld_height_numad./maximum(bld_height_numad)) # Discretely assign the airfoils
+        for (iheight,height_slices) in enumerate(collect(LinRange(0,1,Nslices)))
+            if airfoils[iheight]=="nothing" && height_slices<=height_numad
+                airfoils[iheight] = "$(numadIn_bld.airfoil[iheight_numad]).dat"
+            end
+        end
+    end
 
     OWENSAero.setupTurb(shapeX,shapeY,B,chord,tsr,Vinf;AModel,DSModel,
     afname = airfoils, #TODO: map to the numad input
@@ -436,20 +443,28 @@ end
 nothing
 
 # Set up AeroDyn if used
-# Here we create AeroDyn the files, first by specifying the names, then by creating the files, TODO: hook up the direct sectionPropsArray_str
+# Here we create AeroDyn the files, first by specifying the names, then by creating the files
 # Then by initializing AeroDyn and grabbing the backend functionality with a function handle
 if AD15On
     ad_input_file="$path/ADInputFile_SingleTurbine2.dat"
     ifw_input_file="$path/IW2.dat"
     blade_filename="$path/blade2.dat"
     lower_strut_filename="$path/lower_arm2.dat"
     upper_strut_filename="$path/upper_arm2.dat"
-    airfoil_filenames = "$path/airfoils/NACA_0018_AllRe.dat"
     OLAF_filename = "$path/OLAF2.dat"
 
     NumADBldNds = NumADStrutNds = 10 
 
     bldchord_spl = FLOWMath.akima(numadIn_bld.span./maximum(numadIn_bld.span), numadIn_bld.chord,LinRange(0,1,NumADBldNds))
+
+    airfoil_filenames = fill("nothing",NumADBldNds) # Discretely assign the airfoils #TODO: separate out struts
+    for (ispan_numad,span_numad) in enumerate(numadIn_bld.span./maximum(numadIn_bld.span))
+        for (ispan,span_slices) in enumerate(collect(LinRange(0,1,NumADBldNds)))
+            if airfoil_filenames[ispan]=="nothing" && span_slices<=span_numad
+                airfoil_filenames[ispan] = "$(numadIn_bld.airfoil[ispan_numad]).dat"
+            end
+        end
+    end
 
     if meshtype == "ARCUS" 
         blade_filenames = [blade_filename for i=1:Nbld]
@@ -503,7 +518,7 @@ if AD15On
         BlCrvAng=zeros(blade_Nnodes[iADBody])
         BlTwist=zeros(blade_Nnodes[iADBody])
         BlChord=blade_chords[iADBody]
-        BlAFID=ones(Int,blade_Nnodes[iADBody])
+        BlAFID=collect(1:length(airfoil_filenames))
         OWENSOpenFASTWrappers.writeADbladeFile(filename;NumBlNds=blade_Nnodes[iADBody],BlSpn,BlCrvAC,BlSwpAC,BlCrvAng,BlTwist,BlChord,BlAFID)
     end