Aeromatic v 0.8, DPC 2004-01-01 $Revision: 1.26 $ Models a Northrop T-38 This model was created using publicly available data, publicly available technical reports, textbooks, and guesses. It contains no proprietary or restricted data. If this model has been validated at all, it would be only to the extent that it seems to "fly right", and that it possibly complies with published, publicly known, performance data (maximum speed, endurance, etc.). Thus, this model is meant for educational and entertainment purposes only. This simulation model is not endorsed by the manufacturer. This model is not to be sold. 170 25.25 6.73 34 13 47 13 320 0 0 154 0 36 320 0 0 7806 36075 31319 7574 314 0 -10 73 0 -46 0.8 0.5 0.02 5000 500 5 NONE 1 335 -65 -46 0.8 0.5 0.02 37870 3787 0.0 LEFT 1 335 65 -46 0.8 0.5 0.02 37870 3787 0.0 RIGHT 1 -22 0 -4 0.80 0.50 5000.00 500.00 330 -157 -15 0.80 0.50 5000.00 500.00 330 157 -15 0.80 0.50 5000.00 500.00 178 0 54 0.80 0.50 5000.00 500.00 450 0 114 0.80 0.50 5000.00 500.00 525 0 5 0.80 0.50 5000.00 500.00 452 -20 0 0 0 0 0 551 -20 0 0.0 0.0 0.0 452 20 0 0.0 0 0 1 551 20 0 0.0 0.0 0.0 298 0 0 1953 1900 370 0 0 2029 2000 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pilot-pitch-sum velocities/mach 0.0000 1.0000 0.6000 1.0000 1.2000 0.7000
fcs/pitch-feel -1.0 0.583 fcs/elevator-pos-norm fcs/aileron-cmd-norm fcs/roll-trim-cmd-norm -1 1 fcs/pilot-roll-sum velocities/mach 0.0000 1.0000 0.6000 1.0000 1.2000 0.7000
fcs/roll-feel -1.00 0.75 fcs/left-aileron-pos-norm -fcs/roll-feel -1.00 0.65 fcs/right-aileron-pos-norm fcs/rudder-cmd-norm fcs/yaw-trim-cmd-norm -1 1 velocities/r-aero-rad_sec velocities/mach 0.0000 0.0000 0.1000 0.0000 0.1100 1.0000
aero/beta-rad velocities/mach 0.0000 0.0000 1.2000 0.0000
fcs/yaw-sas-rate fcs/yaw-sas-beta -0.1 0.1 fcs/rudder-command-sum fcs/yaw-sas-sum -1 1 fcs/rudder-sum -1.00 1.00 fcs/rudder-pos-norm fcs/throttle-cmd-norm 2 fcs/throttle-pos-norm fcs/throttle-cmd-norm[1] 2 fcs/throttle-pos-norm[1] fcs/flap-cmd-norm 0 24 40 fcs/flap-pos-deg fcs/flap-pos-deg 0 40 0 1 fcs/flap-pos-norm gear/gear-cmd-norm 0 1 gear/gear-pos-norm fcs/speedbrake-cmd-norm 0 1 fcs/speedbrake-pos-norm Drag_at_zero_lift aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -1.5700 1.5000 -0.2600 0.0320 0.0000 0.0160 0.2600 0.0320 1.5700 1.5000
Induced_drag aero/qbar-psf metrics/Sw-sqft aero/cl-squared 0.1000 Drag_due_to_mach aero/qbar-psf metrics/Sw-sqft velocities/mach 0.0000 0.0000 0.8100 0.0000 1.1000 0.0240 1.8000 0.0110
Drag_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.00225 Drag_due_to_gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.0150 Drag_due_to_speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.0250 Drag_due_to_sideslip aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.5700 1.2300 -0.2600 0.0500 0.0000 0.0000 0.2600 0.0500 1.5700 1.2300
Drag_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-norm 0.0300 Side_force_due_to_beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.0000 Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/alpha-radfcs/flap-pos-deg 0.0000 40.0000 -0.2000 -0.5710 0.1000 0.0000 0.0000 0.6000 0.2500 0.7160 1.3000 0.3300 0.9450 0.3000 0.6000 0.1740 0.0000
Lift_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-norm 0.0600 Roll_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad aero/alpha-rad 0.0000 -0.0500 0.5200 -0.1200
Roll_moment_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec -0.4000 Roll_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec 0.1200 Roll_moment_due_to_left_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-norm 0.0193 Roll_moment_due_to_right_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/right-aileron-pos-norm -0.0193 Roll_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-norm 0.0021 Pitch_moment_due_to_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -0.3000 Pitch_moment_due_to_elevator aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-norm -0.1950 Pitch_moment_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -18.0000 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -9.0000 Pitch_moment_due_to_flaps aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/flap-pos-deg -0.0025 Yaw_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.1000 Yaw_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec -0.1500 Yaw_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-norm -0.0070