Plane Vanilla #Mach 0.0 #IYsym IZsym Zsym 0 0 0.0 #Sref Cref Bref 9.0 0.9 10.0 #Xref Yref Zref 0.50 0.0 0.0 # # #==================================================================== SURFACE Wing #Nchordwise Cspace Nspanwise Sspace 8 1.0 12 1.0 # ANGLE 2.0 #------------------------------------------------------------- SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.2 -5.0 1.0 0.6 0.0 0 0 AFILE sd7037.dat #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 # CLAF 1.0 #------------------------------------------------------------- SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0. 0. 0. 1.0 0.0 0 0 AFILE sd7037.dat #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 CLAF 1.0 #------------------------------------------------------------- SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.2 5.0 1.0 0.6 0.0 0 0 AFILE sd7037.dat #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 # CLAF 1.0 #==================================================================== SURFACE H-stab #Nchordwise Cspace Nspanwise Sspace 6 1.0 6 1.0 # YDUPLICATE 0.0 # TRANSLATE 4.0 0.0 0.0 # #------------------------------------------------------------- SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.0 0.0 0.0 0.7 0. 0 0 #Cname Cgain Xhinge HingeVec SgnDup CONTROL elevator 1.0 0.7 0.0 1.0 0.0 1.0 #------------------------------------------------------------- SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.14 1.25 0.0 0.42 0. 0 0 #Cname Cgain Xhinge HingeVec SgnDup CONTROL elevator 1.0 0.7 0.0 1.0 0.0 1.0 # #==================================================================== SURFACE V-stab #Nchordwise Cspace Nspanwise Sspace 6 1.0 5 1.0 TRANSLATE 4.0 0.0 0.0 #------------------------------------------------------------- SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.0 0. 0.0 0.7 0. 0 0 #Cname Cgain Xhinge HingeVec SgnDup CONTROL rudder 1.0 0.5 0.0 0.0 1.0 1.0 #------------------------------------------------------------- SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.14 0. 1.0 0.42 0. 0 0 #Cname Cgain Xhinge HingeVec SgnDup CONTROL rudder 1.0 0.5 0.0 0.0 1.0 1.0 #-------------------------------------------------------------