[fltsim.0] title=AW P-51D sim=P51d model= panel= sound= texture= checklists=P51d_CHECK [WEIGHT_AND_BALANCE] empty_weight = 6840 // (pounds) reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170, -2.0, 0.0, 2.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 8185.0 empty_weight_roll_MOI = 4736.0 empty_weight_yaw_MOI = 10026.0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [piston_engine] power_scalar = 1.0 [propeller] thrust_scalar = 1.0 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [contact_points] //0 Class //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) point.0=1.0,-17.00, 0.00, -2.30, 3200, 0, 0.59,180.0, 0.40, 2.5, 0.80, 7.5, 5.00, 0, 0, 135 point.1=1.0, 1.80,-7.93, -7.10, 2200, 1, 0.59, 0.0, 0.50, 2.5, 0.83, 8.0, 8.00, 2, 0, 135 point.2=1.0, 1.80, 7.93, -7.10, 2200, 2, 0.59, 0.0, 0.50, 2.5, 0.83, 8.0, 8.00, 3, 0, 135 point.3=2.0, 0.00,-18.5, 0.00, 1200, 0, 0.00, 0.00, 0.00, 0.0, 0.00, 0.0, 0.00, 5 point.4=2.0, 0.00, 18.5, 0.00, 1200, 0, 0.00, 0.00, 0.00, 0.0, 0.00, 0.0, 0.00, 6 point.5=2.0,-20.51, 0.00, 0.00, 2400, 0, 0.00, 0.00, 0.00, 0.0, 0.00, 0.0, 0.00, 9 point.6=2.0, 12.24, 0.00, 0.00, 1200, 0, 0.00, 0.00, 0.00, 0.0, 0.00, 0.0, 0.00, 4 static_pitch= 15.0 //degrees (pitch when loaded on ground) static_cg_height=6.4 //(feet) altitude of CG when at rest (altitude when loaded on ground) [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.125 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=14 // degrees, KIAS flaps-position.2=28 // degrees, KIAS flaps-position.3=42 // degrees, KIAS flaps-position.4=55 // degrees, KIAS damaging-speed=175 // KIAS blowout-speed=265 // KIAS [Views] eyepoint=-2.70,0.00,2.53 [LIGHTS] panel=0.00, 0.50, -0.8, fx_vclight