Supra 3.4m F3J 0.0 Mach 0 0 0.0 iYsym iZsym Zsym # 1034.0 7.60 133.86 Sref Cref Bref reference area, chord, span 3.750 0.0 1.5 Xref Yref Zref moment reference location 0.015 CDo # # # #============================================= SURFACE Inner Wing 7 1.0 8 -2.9 ! Nchord Cspace Nspan Sspace INDEX 1 ANGLE 1.0 twist angle bias for whole surface YDUPLICATE 0.0 SCALE 1.0 1.0 0.0437 ! 2.5 deg dihedral TRANSLATE 0.0 0.0 0.0 #--------------------------------------------- SECTION 0.0 0.0 0.0 9.75 0.0 1 0 AFIL 0.0 1.0 ag40d.dat CONTROL flap 1.0 0.75 0. 0. 0. 1. CONTROL aileron -1.00 0.75 0. 0. 0. -1. #--------------------- SECTION 0.25 31.5 31.5 8.75 0.0 1 0 AFIL 0.0 1.0 ag41d.dat CONTROL flap 1.0 0.75 0. 0. 0. 1. CONTROL aileron -1.00 0.75 0. 0. 0. -1. #============================================================== SURFACE Outer Wing 7 1.0 18 -2.0 ! Nchord Cspace Nspan Sspace INDEX 1 ANGLE 1.0 twist angle bias for whole surface YDUPLICATE 0.0 SCALE 1.0 1.0 0.13165 ! 7.5 deg dihedral TRANSLATE 0.25 31.5 1.37655 #--------------------------------------------- SECTION 0.0 0.0 0.0 8.75 0.0 1 0 AFIL 0.0 1.0 ag41d.dat CONTROL flap 1.0 0.75 0. 0. 0. 1. CONTROL aileron -1.0 0.75 0. 0. 0. -1. #--------------------- SECTION 1.0 23.5 23.5 6.25 -0.5 1 0 AFIL 0.0 1.0 ag42d.dat CONTROL flap 1.0 0.75 0. 0. 0. 1. CONTROL aileron -1.0 0.75 0. 0. 0. -1. DESIGN twist 1.0 #--------------------- SECTION 1.72 29.5 29.5 5.00 -0.5 1 0 AFIL 0.0 1.0 ag42d.dat CONTROL flap 1.0 0.75 0. 0. 0. 1. CONTROL aileron -1.0 0.75 0. 0. 0. -1. DESIGN twist 1.0 #--------------------- SECTION 2.75 34.0 34.0 3.40 -0.5 1 0 AFIL 0.0 1.0 ag43d.dat CONTROL flap 1.0 0.75 0. 0. 0. 1. CONTROL aileron -1.0 0.75 0. 0. 0. -1. DESIGN twist 1.0 #--------------------- SECTION 3.50 35.50 35.50 2.3 -0.5 1 0 AFIL 0.0 1.0 ag43d.dat CONTROL flap 1.0 0.75 0. 0. 0. 1. CONTROL aileron -1.0 0.75 0. 0. 0. -1. DESIGN twist 1.0 #============================================================== SURFACE Stab 5 1.0 12 -1.0 ! Nchord Cspace Nspan Sspace ANGLE 0.0 twist angle bias for whole surface YDUPLICATE 0.0 SCALE 1.0 1.0 1.0 TRANSLATE 37.5 0.0 2.1 #--------------------------------------------- SECTION 0.0 0.0 0. 4.40 0.000000 CONTROL elevator 1.0 0. 0. 0. 0. 1. #--------------------- SECTION 0.15385 2.0 0. 4.1154 0.000000 CONTROL elevator 1.0 0. 0. 0. 0. 1. #--------------------- SECTION 0.7692 10.0 0. 2.577 0.000000 CONTROL elevator 1.0 0. 0. 0. 0. 1. #--------------------- SECTION 1.173 12.0 0. 1.942 0.000000 CONTROL elevator 1.0 0. 0. 0. 0. 1. #--------------------- SECTION 1.50 12.7 0. 1.52 0.000000 CONTROL elevator 1.0 0. 0. 0. 0. 1. #--------------------- SECTION 2.00 13.0 0. 1.0 0.000000 CONTROL elevator 1.0 0. 0. 0. 0. 1. #============================================================== SURFACE Fin 10 1.0 12 -1.0 ! Nchord Cspace Nspan Sspace ANGLE 0.0 twist angle bias for whole surface SCALE 1.15 1.15 1.1 TRANSLATE 42.5 0.0 0.0 #--------------------------------------------- SECTION 0.0 0.0 0. 7.0 0.000000 CONTROL rudder 1.0 0.43 0. 0. 0. 1. #--------------------- SECTION 1.125 0.0 9.0 4.0 0.000000 CONTROL rudder 1.0 0.50 0. 0. 0. 1. #--------------------- SECTION 1.875 0.0 11.25 2.8333 0.000000 CONTROL rudder 1.0 0.50 0. 0. 0. 1. #--------------------- SECTION 2.5 0.0 12.0 2.0 0.000000 CONTROL rudder 1.0 0.50 0. 0. 0. 1.