Aeromatic v 0.95 2014-07-04 $Revision: 1.15 $ Models a F4F-3. 260.00 38.00 2.00 6.84 44.20 17.27 26.00 17.27 138.16 0.00 0.00 96.71 0.00 40.00 0 0 0 4326 4412 8083 5293 138.16 0.00 -8.63 2407 LBS + full (1070 LBS) fuel should bring model up to entered max weight 1203.5 138.16 0.00 -8.63 125.72 -68.40 -69.08 0.80 0.50 0.02 8769.98 4384.99 0 LEFT 1 125.72 68.40 -69.08 0.80 0.50 0.02 8769.98 4384.99 0 RIGHT 1 314.30 0.00 -20.72 0.80 0.50 0.02 8769.98 7015.98 5.00 NONE 1 138.16 -19.00 -8.63 1.00 1.00 8769.98 8769.98 138.16 19.00 -8.63 1.00 1.00 8769.98 8769.98 36.00 0.00 0.00 0.00 0.00 0.00 0 1 36.00 0.00 0.00 0.00 0.00 0.00 138.16 0.00 -8.63 534.97 267.48 138.16 0.00 -8.63 534.97 267.48 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum -0.35 0.35

fcs/elevator-pos-rad

fcs/elevator-pos-rad -0.35 0.35 -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 fcs/rudder-command-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 15 4 30 3

fcs/flap-pos-deg

fcs/flap-pos-deg 0 30 0 1

fcs/flap-pos-norm

gear/gear-cmd-norm 0 0 1 5

gear/gear-pos-norm

fcs/speedbrake-cmd-norm 0 0 1 1

fcs/speedbrake-pos-norm

Lift due to alpha aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -0.20 -0.730 0.00 0.170 0.23 1.200 0.60 0.582 Delta Lift due to flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.01000 Delta Lift due to speedbrake aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0 Lift due to Elevator Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.2 Drag at zero lift aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -1.57 1.500 -0.26 0.026 0.00 0.020 0.26 0.026 1.57 1.500 Induced drag aero/qbar-psf metrics/Sw-sqft aero/cl-squared 0.06 Drag due to mach aero/qbar-psf metrics/Sw-sqft velocities/mach 0.00 0.000 0.75 0.000 1.10 0.023 1.80 0.015 Drag due to flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.00133 Drag due to gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.03 Drag due to speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.02 Drag due to sideslip aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.57 1.230 -0.26 0.050 0.00 0.000 0.26 0.050 1.57 1.230 Drag due to Elevator Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-norm 0.04 Side force due to beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1 Roll moment due to beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.1 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 0.15 Roll moment due to aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0.18 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 -0.5 Pitch moment due to elevator aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad velocities/mach 0.0 -1.000 2.0 -0.250 Pitch moment due to pitch rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -15 Pitch moment due to alpha rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -7 Yaw moment due to beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.12 Yaw moment due to yaw rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec -0.15 Yaw moment due to rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.1 Adverse yaw aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad -0.003