D8.1 Model #Mach 0.15 #IYsym IZsym Zsym 0 0 0.0 #Sref Cref Bref 525.0 6.0 90.0 #Xref Yref Zref 38.0 0.0 0.0 #-------------------------------------------------- SURFACE Wing #Nchordwise Cspace Nspanwise Sspace 8 1.0 26 -1.5 INDEX 1 YDUPLICATE 0.0 ANGLE 0.0 ! low-incidence wing position !3.0 ! high-incidence wing position SCALE 1.0 1.0 1.0 TRANSLATE 34.0 0.0 -1.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.0 5.4 0.0 9.0 2.0 AFILE da00.dat CONTROL flap 1.0 0.75 0. 0. 0. +1 CONTROL slat 1.0 -.111 0. 0. 0. +1 CLAF 1.05 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.947 11.0 0.291 7.951 2.0 AFILE da02.dat CONTROL flap 1.0 0.75 0. 0. 0. +1 CONTROL slat 1.0 -.117 0. 0. 0. +1 CLAF 1.05 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 3.070 24.0 0.945 5.599 1.5 AFILE da03.dat CONTROL flap 1.0 0.75 0. 0. 0. +1 CONTROL slat 1.0 -.136 0. 0. 0. +1 CONTROL aileron -1.0 0.80 0. 0. 0. -1 CLAF 1.04 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 5.030 36.0 1.548 3.428 0.8 AFILE da04.dat CONTROL flap 1.0 0.75 0. 0. 0. +1 CONTROL slat 1.0 -.178 0. 0. 0. +1 CONTROL aileron -1.0 0.80 0. 0. 0. -1 CLAF 1.03 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 6.50 45.0 2.0 1.8 0.5 AFILE da05.dat CONTROL slat 1.0 -.278 0. 0. 0. +1 CONTROL aileron -1.0 0.80 0. 0. 0. -1 CLAF 1.01 DESIGN a5 #-------------------------------------------------- SURFACE Stab #Nchordwise Cspace Nspanwise Sspace 6 1.0 14 -2.0 INDEX 1 YDUPLICATE 0.0 ANGLE 0.0 SCALE 1.0 1.0 1.0 TRANSLATE 65.0 0.0 8.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.0 0.0 0.0 4.0 0. CONTROL elevator 1.0 0.0 0. 0. 0. 1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.0 5.0 0.0 4.0 0. CONTROL elevator 1.0 0.0 0. 0. 0. 1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 1.075 12.0 0.0 2.345 0. CONTROL elevator 1.0 0.0 0. 0. 0. 1 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 1.69 16.0 0.0 1.40 0. CONTROL elevator 1.0 0.0 0. 0. 0. 1 #-------------------------------------------------- SURFACE Fin #Nchordwise Cspace Nspanewise Sspace 9 1.0 11 0.75 INDEX 1 YDUPLICATE 0.0 ANGLE 0.0 SCALE 1.0 1.0 1.0 TRANSLATE 0.0 0.0 0.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 56.5 5.4 -1.0 8.0 0. CONTROL rudder 1.0 0.77 0. 0. 0. 0.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 60.0 5.3 1.5 5.0 0. CONTROL rudder 1.0 0.65 0. 0. 0. 0.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 65.0 5.0 8.0 2.4 0. CONTROL rudder 1.0 0.65 0. 0. 0. 0.0 #-------------------------------------------------- SURFACE Fuselage #Nchordwise Cspace Nspanwise Sspace 32 0.6 INDEX 1 YDUPLICATE 0.0 SCALE 1.0 1.0 1.0 TRANSLATE 0.0 0.0 -1.0 SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.0 0.0 0.0 63.9 0. 1 0. AFILE d8f0c.dat SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 0.78 1.2 0.0 63.18 0. 1 0. AFILE d8f1c.dat SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 3.36 2.85 0.0 60.60 0. 1 0. AFILE d8f2c.dat SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 8.04 4.29 0.0 56.01 0. 1 0. AFILE d8f3c.dat SECTION #Xle Yle Zle Chord Ainc Nspanwise Sspace 14.40 5.4 0.0 49.80 0. 1 0.