Dave Culp Aeromatic 2006-01-04 $Revision: 1.40 $ Models a Boeing 737. GPL (General Public License) http://www.gnu.org/licenses/gpl.html 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. 1171.00 94.70 12.31 348.00 48.04 297.00 44.50 625 0 24 80 -30 70 0 0 0 562000 1.473e+06 1.894e+06 0 8000 0 83000 639 0 -40 158 0 -84 0.80 0.50 0.02 90000 4000 8000 35 NONE 1 648 -100 -84 0.80 0.50 0.02 120000 10000 20000 0.0 LEFT 1 648 100 -84 0.80 0.50 0.02 120000 10000 20000 0.0 RIGHT 1 540 -193 -40 0 0 0 0 2 540 -193 -40 0 0 0 540 193 -40 0 0 0 1 2 540 193 -40 0 0 0 520 -80 -18 10200 10000 59.0 520 80 -18 10200 10000 480 0 -18 15000 4000 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum -0.3 0.3 fcs/elevator-pos-rad fcs/elevator-pos-rad -0.3 0.3 -1 1 fcs/elevator-pos-norm fcs/aileron-cmd-norm fcs/roll-trim-cmd-norm -1 1 fcs/roll-trim-sum -0.35 0.35 fcs/left-aileron-pos-rad -fcs/roll-trim-sum -0.35 0.35 fcs/right-aileron-pos-rad fcs/left-aileron-pos-rad -0.35 0.35 -1 1 fcs/left-aileron-pos-norm fcs/right-aileron-pos-rad -0.35 0.35 -1 1 fcs/right-aileron-pos-norm fcs/rudder-cmd-norm fcs/yaw-trim-cmd-norm -1 1 velocities/r-aero-rad_sec velocities/mach 0.00 0.0 0.10 0.0 0.11 1.0
fcs/yaw-damper velocities/mach 0.00 0.0 0.10 0.0 0.11 1.0
fcs/rudder-command-sum fcs/yaw-damper-final -1 1 fcs/rudder-sum -0.35 0.35 fcs/rudder-pos-rad fcs/rudder-pos-rad -0.35 0.35 -1 1 fcs/rudder-pos-norm fcs/flap-cmd-norm 0 0.125 0.25 0.375 0.5 0.625 0.75 0.875 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 fcs/spoiler-cmd-norm 0 1 fcs/spoiler-pos-norm Change_in_drag_due_to_ground_effect aero/h_b-mac-ft 0.0000 0.0480 0.1000 0.5150 0.1500 0.6290 0.2000 0.7090 0.3000 0.8150 0.4000 0.8820 0.5000 0.9280 0.6000 0.9620 0.7000 0.9880 0.8000 1.0000
Change_in_lift_due_to_ground_effect aero/h_b-mac-ft 0.0000 1.2030 0.1000 1.1270 0.1500 1.0900 0.2000 1.0730 0.3000 1.0460 0.4000 1.0550 0.5000 1.0190 0.6000 1.0130 0.7000 1.0080 0.8000 1.0060 0.9000 1.0030 1.0000 1.0020 1.1000 1.0000
Change_in_lift_due_to_speed_brake fcs/speedbrake-pos-norm 0.0000 1.0 0.1000 0.85
Change_in_lift_due_to_spoilers fcs/spoiler-pos-norm 0.0000 1.0 0.1000 0.6
Drag_at_zero_lift aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -1.57 1.5000 -0.26 0.0420 0.00 0.0210 0.26 0.0420 1.57 1.5000
Induced_drag aero/qbar-psf metrics/Sw-sqft aero/cl-squared aero/function/kCDge 0.043 Drag_due_to_mach aero/qbar-psf metrics/Sw-sqft velocities/mach 0.00 0.0000 0.79 0.0000 1.10 0.0230 1.80 0.0150
Drag_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-norm 0.059 Drag_due_to_gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.015 Drag_due_to_flight_spoilers aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.02 Drag_due_to_ground_spoilers aero/qbar-psf metrics/Sw-sqft fcs/spoiler-pos-norm 0.04 Drag_due_to_sideslip aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.57 1.2300 -0.26 0.0500 0.00 0.0000 0.26 0.0500 1.57 1.2300
Drag_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-norm 0.059 Side_force_due_to_beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1 Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/function/kCLge aero/function/kCLsb aero/function/kCLsp aero/alpha-rad -0.20 -0.68 0.00 0.20 0.23 1.20 0.46 0.20
Delta_Lift_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-norm aero/function/kCLge aero/function/kCLsb aero/function/kCLsp 0.9 Lift_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.2 Roll_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.09 Roll_moment_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec -0.4 Roll_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec 0.09 Roll_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad velocities/mach 0.0 0.100 2.0 0.033
Roll_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad 0.01 Pitch_moment_due_to_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -0.6 Pitch_moment_due_to_elevator aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad velocities/mach 0.0 -1.20 2.0 -0.30
Pitch_moment_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -27.0 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -16.0 Yaw_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.26 Yaw_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec -0.35 Yaw_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.20 aero/qbar-psf attitude/phi-rad position/h-sl-ft velocities/vc-kts fcs/throttle-cmd-norm fcs/elevator-pos-norm ON ON ON ON ON OFF OFF OFF ON