737-800 raised tail #Mach 0.78 #IYsym IZsym Zsym 0 0 0.0 #Sref Cref Bref 1260.0 11.0 113.0 #Xref Yref Zref 60.0 0.0 0.0 #-------------------------------------------------- SURFACE Wing !Nchordwise Cspace Nspanwise Sspace 12 1.0 26 -1.1 COMPONENT 1 YDUPLICATE 0.0 ANGLE 0.0 SCALE 1.0 1.0 0.07 TRANSLATE 50.0 0.0 0.0 !SECTION !#Xle Yle Zle Chord Ainc Nspanwise Sspace !-0.5 0.0 0.0 21.0 5.0 !AFILE !a1.dat !CONTROL !flap 1.0 0.81 0. 0. 0. +1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace -0.5 6.0 0.0 21.0 5.0 AFILE a1.dat CONTROL slat -1.0 -0.05 0. 0. 0. +1 CONTROL flap 1.0 0.81 0. 0. 0. +1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 2.167 10.0 6.0 18.333 0.0 AFILE a1.dat CONTROL slat -1.0 -0.05 0. 0. 0. +1 CONTROL flap 1.0 0.768 0. 0. 0. +1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 7.50 18.0 12.0 13.0 3.0 AFILE a1.dat CONTROL slat -1.0 -0.075 0. 0. 0. +1 CONTROL flap 1.0 0.685 0. 0. 0. +1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 16.0 34.0 28.0 9.0 1.0 AFILE a1.dat CONTROL slat -1.0 -0.11 0. 0. 0. +1 CONTROL flap 1.0 0.685 0. 0. 0. +1 CONTROL aileron -1.0 0.80 0. 0. 0. -1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 22.0 47.0 41.0 6.4 -0.5 AFILE a1.dat CONTROL slat -1.0 -0.17 0. 0. 0. +1 CONTROL aileron -1.0 0.80 0. 0. 0. -1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 25.1 54.0 48.0 4.9 -1.5 AFILE a1.dat CONTROL slat -1.0 -0.20 0. 0. 0. +1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 27.1 56.5 50.5 3.5 -2.0 AFILE a1.dat #-------------------------------------------------- SURFACE Stab #Nchordwise Cspace Nspanwise Sspace 6 1.0 15 -1.1 COMPONENT 1 YDUPLICATE 0.0 SCALE 1.0 1.0 0.17 TRANSLATE 110.0 0.0 6.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace -2.50 0.0 0.0 14.0 0. CONTROL elevator 1.0 0.60 0. 0. 0. 1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 2.00 6.0 6.0 11.5 0. 1 0. CONTROL elevator 1.0 0.64 0. 0. 0. 1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 10.7 18.0 18.0 6.8 0. CONTROL elevator 1.0 0.75 0. 0. 0. 1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 15.0 23.5 23.5 4.0 0. #-------------------------------------------------- SURFACE Fin #Nchordwise Cspace Nspanwise Sspace 7 1.0 11 1.0 COMPONENT 1 SCALE 1.0 1.0 1.0 TRANSLATE 95.0 0.0 6.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.0 0.0 0.0 26.5 0. CONTROL rudder 1.0 0.82 0. 0. 0. 1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 13.0 0.0 5.0 14.5 0. CONTROL rudder 1.0 0.70 0. 0. 0. 1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 28.0 0.0 25.0 4.0 0. CONTROL rudder 1.0 0.70 0. 0. 0. 1 #-------------------------------------------------- SURFACE Fuselage H #Nchordwise Cspace Nspanwise Sspace 24 1.0 COMPONENT 1 YDUPLICATE 0.0 SCALE 1.0 1.0 1.0 TRANSLATE 0.0 0.0 0.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.0 0.0 0.0 124.0 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.80 1.0 0.0 119.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 3.60 2.5 0.0 111.2 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 8.40 4.25 0.0 100.0 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 14.00 5.25 0.0 90.8 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 20.00 6.0 0.0 82.0 0. 1 0. #-------------------------------------------------- SURFACE Fuselage V Bottom #Nchordwise Cspace Nspanwise Sspace 24 1.0 NOWAKE COMPONENT 1 SCALE 1.0 1.0 1.0 TRANSLATE 0.0 0.0 0.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 12.00 0.0 -6.0 83.0 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 8.50 0.0 -5.25 91.0 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 5.00 0.0 -4.25 99.0 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 2.20 0.0 -2.5 110.0 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.50 0.0 -1.0 119.0 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.0 0.0 0.0 124.0 0. 1 0. #-------------------------------------------------- SURFACE Fuselage V Top #Nchordwise Cspace Nspanwise Sspace 24 1.0 COMPONENT 1 SCALE 1.0 1.0 1.0 TRANSLATE 0.0 0.0 0.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.0 0.0 0.0 124.0 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.50 0.0 1.0 123.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 2.20 0.0 2.5 121.8 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 5.00 0.0 4.25 119.0 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 8.50 0.0 5.25 115.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 12.00 0.0 6.0 112.0 0. 1 0. #-------------------------------------------------- SURFACE Nacelle #Nchordwise Cspace Nspanwise Sspace 6 1.0 12 0.0 COMPONENT 1 YDUPLICATE 0.0 SCALE 1.0 4.0 3.5 TRANSLATE 45.0 16.0 -4.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 0.0 1.0 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 0.5 0.866 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 0.866 0.5 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 1.0 0.0 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 0.866 -0.5 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 0.5 -0.866 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 0.0 -1.0 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 -0.5 -0.866 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 -0.866 -0.5 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 -1.0 0.0 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 -0.866 0.5 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 -0.5 0.866 12.5 0. 1 0. SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.00 0.0 1.0 12.5 0. 1 0.