1.0 0.25 0.25 aero/alpha-rad aero/beta-rad aero/alpha-rad aero/beta-rad aero/alpha-rad aero/tmp/wy 2.0 aero/tmp/wz 2.0 0.5 0.0 aero/tmp/wx 57.29578 aero/envelope-aoa-mag-rad The current method of splitting L_env_aoa into LIFT and SIDE forces seems to have the wrong sign when alpha GT 90 and beta LT 0? Total_lift_force_from_envelope_due_to_aoa aero/qbar-psf aero/constants/volume-ft3_2_3 aero/envelope-lift-force-tweak-factor aero/envelope-aoa-mag-deg 0 0.000000 10 0.002911 20 0.007450 30 0.013047 45 0.016276 60 0.028917 75 0.028148 90 0.017636 105 -0.010199 120 -0.008625 135 -0.011184 150 -0.009168 165 -0.002132 180 0.000000 Same as for L_env_aoa. Total_moment_from_envelope_due_to_due_to_aoa aero/qbar-psf aero/constants/volume-ft3 aero/envelope-pitch-moment-tweak-factor aero/envelope-aoa-mag-deg 0 0.00000 10 0.26542 20 0.48736 30 0.66063 45 0.76844 60 0.65462 75 0.36527 90 -0.01611 105 -0.40902 120 -0.67203 135 -0.77532 150 -0.66775 165 -0.38522 180 0.00000 Drag_from_envelope_due_to_angle_of_attack aero/qbar-psf aero/constants/volume-ft3_2_3 aero/envelope-lift-force-tweak-factor aero/envelope-aoa-mag-deg 0 0.0059211 10 0.0084486 20 0.0088926 30 0.0178950 45 0.0325350 60 0.0506840 75 0.0766400 90 0.0999370 105 0.0866310 120 0.0561820 135 0.0342520 150 0.0154610 165 0.0042752 180 0.0018604 Drag_from_horizontal_fin_due_to_alpha aero/qbar-psf aero/constants/volume-ft3_2_3 aero/alpha-deg -180 0.0016346 -165 0.0135650 -150 0.0745610 -135 0.1331500 -120 0.1771500 -105 0.2169500 -90 0.1910000 -75 0.2154000 -60 0.17049 -45 0.14314 -30 0.072847 -20 0.027739 -10 0.0089855 0 0.0010200 10 0.0089855 20 0.027739 30 0.072847 45 0.14314 60 0.17049 75 0.2154000 90 0.1910000 105 0.2169500 120 0.1771500 135 0.1331500 150 0.0745610 165 0.0135650 180 0.0016346 Drag_due_to_elevator_deflection aero/qbar-psf aero/constants/volume-ft3_2_3 1.0 fcs/elevator-pos-deg -30 0.020407 0 0 30 0.020407 Drag_from_vertical_fin_due_to_beta aero/qbar-psf aero/constants/volume-ft3_2_3 1.0 aero/beta-deg -180 0.0016346 -165 0.0135650 -150 0.0745610 -135 0.1331500 -120 0.1771500 -105 0.2169500 -90 0.1910000 -75 0.2154000 -60 0.17049 -45 0.14314 -30 0.072847 -20 0.027739 -10 0.0089855 0 0.0010200 10 0.0089855 20 0.027739 30 0.072847 45 0.14314 60 0.17049 75 0.2154000 90 0.1910000 105 0.2169500 120 0.1771500 135 0.1331500 150 0.0745610 165 0.0135650 180 0.0016346 Drag_due_to_rudder_deflection aero/qbar-psf aero/constants/volume-ft3_2_3 1.0 fcs/rudder-pos-deg -30 0.020407 0 0 30 0.020407 Drag_from_car_and_rigging aero/qbar-psf aero/constants/volume-ft3_2_3 0.8 0.0059211 Side_force_from_envelope_due_to_beta -1.0 aero/force/L_env_aoa aero/tmp/wy 0.00001 aero/tmp/h_wy_wz Side_force_from_vertical_fin_due_to_beta aero/qbar-psf aero/constants/volume-ft3_2_3 -0.5 aero/beta-deg -180 0.00000 -165 0.05372 -150 0.12950 -135 0.13525 -120 0.10292 -105 0.05388 -90 -0.00000 -75 -0.05502 -60 -0.098868 -45 -0.14402 -30 -0.12832 -20 -0.082526 -10 -0.035474 0 0.000000 10 0.035474 20 0.082526 30 0.12832 45 0.14402 60 0.098868 75 0.05502 90 0.00000 105 -0.05388 120 -0.10292 135 -0.13525 150 -0.12950 165 -0.05372 180 0.00000 Side_force_due_to_rudder aero/qbar-psf aero/constants/volume-ft3_2_3 0.5 fcs/rudder-pos-deg -30 -0.066622 0 0 30 0.066622 Lift_from_envelope_due_to_alpha aero/force/L_env_aoa aero/tmp/wz 0.00001 aero/tmp/h_wy_wz Lift_from_horizontal_fin_due_to_alpha aero/qbar-psf aero/constants/volume-ft3_2_3 aero/alpha-deg -180 0.00000 -165 0.05372 -150 0.12950 -135 0.13525 -120 0.10292 -105 0.05388 -90 -0.00000 -75 -0.05502 -60 -0.098868 -45 -0.14402 -30 -0.12832 -20 -0.082526 -10 -0.035474 0 0.000000 10 0.035474 20 0.082526 30 0.12832 45 0.14402 60 0.098868 75 0.05502 90 0.00000 105 -0.05388 120 -0.10292 135 -0.13525 150 -0.12950 165 -0.05372 180 0.00000 Lift_due_to_elevator aero/qbar-psf aero/constants/volume-ft3_2_3 1.0 fcs/elevator-pos-deg -30 -0.066622 0 0 30 0.066622 Roll_moment_due_to_roll_rate_(damping) velocities/p-aero-rad_sec -75000.0 Pitch_moment_due_to_pitch_rate_(damping) velocities/q-aero-rad_sec -1500000.0 Pitch_moment_from_envelope_due_to_alpha aero/moment/M_env_aoa aero/tmp/wz 0.00001 aero/tmp/h_wy_wz Pitch_moment_from_horizontal_fin_due_to_alpha aero/qbar-psf aero/constants/volume-ft3 aero/alpha-deg -180 0.00000 -165 0.06884 -150 0.18569 -135 0.23584 -120 0.25459 -105 0.27774 -90 0.23735 -75 0.27625 -60 0.24490 -45 0.25233 -30 0.18336 -20 0.10816 -10 0.045351 0 0 10 -0.045351 20 -0.10816 30 -0.18336 45 -0.25233 60 -0.24490 75 -0.27625 90 -0.23735 105 -0.27774 120 -0.25459 135 -0.23584 150 -0.18569 165 -0.06884 180 0.00000 Pitch_moment_due_to_elevator aero/qbar-psf aero/constants/volume-ft3 1.0 fcs/elevator-pos-deg -30 0.082789 0 0 30 -0.082789 Yaw_moment_due_to_yaw_rate_(damping) velocities/r-aero-rad_sec -1500000.0 Yaw_moment_due_to_rudder aero/qbar-psf aero/constants/volume-ft3 2.5 fcs/rudder-pos-deg -30 0.082789 0 0 30 -0.082789 Yaw_moment_from_envelope_due_to_beta -1.0 aero/moment/M_env_aoa aero/tmp/wy 0.00001 aero/tmp/h_wy_wz Yaw_moment_from_vertical_fin_due_to_beta aero/qbar-psf aero/constants/volume-ft3 -1.0 aero/beta-deg -180 0.00000 -165 0.06884 -150 0.18569 -135 0.23584 -120 0.25459 -105 0.27774 -90 0.23735 -75 0.27625 -60 0.24490 -45 0.25233 -30 0.18336 -20 0.10816 -10 0.045351 0 0 10 -0.045351 20 -0.10816 30 -0.18336 45 -0.25233 60 -0.24490 75 -0.27625 90 -0.23735 105 -0.27774 120 -0.25459 135 -0.23584 150 -0.18569 165 -0.06884 180 0.00000