Simple Wing #Mach 0.0 #IYsym IZsym Zsym 0 0 0.0 #Sref Cref Bref 30.0 2.0 15.0 #Xref Yref Zref 0.50 0.0 0.0 # # #==================================================================== SURFACE Wing #Nchordwise Cspace Nspanwise Sspace 8 1.0 12 1.0 # YDUPLICATE 0.0 # ANGLE 2.0 #------------------------------------------------------------- SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0. 0. 0. 2.2 0.0 0 0 #Cname Cgain Xhinge HingeVec SgnDup CONTROL flap 1.0 0.75 0.0 0.0 0.0 1.0 CONTROL aileron -1.0 0.75 0.0 0.0 0.0 -1.0 #------------------------------------------------------------- SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.4 7.5 0.75 1.8 0.0 0 0 #Cname Cgain Xhinge HingeVec SgnDup CONTROL flap 1.0 0.75 0.0 0.0 0.0 1.0 CONTROL aileron -1.0 0.75 0.0 0.0 0.0 -1.0 #