[fltsim.0] title=Focke-Wulf Fw 190A-8 Lang sim=FW190AB_8 model=fw190aB_8 [General] editable=0 [WEIGHT_AND_BALANCE] max_gross_weight=10800.000000 empty_weight=7055.000000 reference_datum_position=7.720000,0.000000,0.000000 empty_weight_CG_position=-7.720000,0.000000,0.000000 max_number_of_stations=50 station_load.0=180.000000,-12.600000,0.000000,1.250000 empty_weight_roll_MOI=4210.000000 empty_weight_pitch_MOI=6919.000000 empty_weight_yaw_MOI=8844.000000 empty_weight_coupled_MOI=0.000000 CG_forward_limit=0.000000 CG_aft_limit=1.000000 [fuel] Center1=-9.440000,0.000000,0.000000,51.000000,0.000000 Center2=-11.000000,0.000000,0.000000,64.500000,0.000000 fuel_type= 1.000 number_of_tank_selectors= 1 [airplane_geometry] wing_area=197.000000 wing_span=34.500000 wing_root_chord=7.480000 wing_dihedral=5.000000 wing_incidence=1.500000 wing_twist=-0.500000 oswald_efficiency_factor=0.700000 wing_winglets_flag=0 wing_sweep=6.000000 wing_pos_apex_lon=-5.900000 wing_pos_apex_vert=-0.940000 htail_area=29.4 htail_span=12.250000 htail_pos_lon=-24.400000 htail_pos_vert=0.940000 htail_incidence=-0.700000 htail_sweep=4.000000 vtail_area=29.000000 vtail_span=6.140000 vtail_sweep=33.000000 vtail_pos_lon=-24.400000 vtail_pos_vert=1.700000 elevator_area=12.820000 aileron_area=20.7 rudder_area=8.230000 elevator_up_limit=28.000000 elevator_down_limit=21.000000 aileron_up_limit=17.000000 aileron_down_limit=17.000000 rudder_limit=20.000000 elevator_trim_limit=20.000000 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [Flaps.0] type=1 span-outboard=0.400000 extending-time=5.000000 system_type=0 damaging-speed=150.000000 blowout-speed=180.000000 lift_scalar=1.000000 drag_scalar=1.000000 pitch_scalar=1.000000 flaps-position.0=0.000000 flaps-position.1=12.000000 flaps-position.2=38.000000 flaps-position.3=75.000000 [Reference Speeds] flaps_up_stall_speed=95.000000 full_flaps_stall_speed=91.000000 cruise_speed=286.000000 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [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=1.000000,-26.600000,0.000000,-1.850000,1574.803000,0.000000,0.558000,180.000000,0.3,2.500000,0.970000,3.000000,3.000000,0.000000,140.000000,150.000000 point.1=1.000000,-5.73000,-6.58000,-6.95000,2165.354000,1.000000,0.558000,0.000000,0.4,2.500000,0.8000,7.500000,7.500000,2.000000,140.000000,150.000000 point.2=1.000000,-5.73000,6.580000,-6.95000,2165.354000,2.000000,0.558000,0.000000,0.4,2.500000,0.8000,6.500000,6.500000,3.000000,140.000000,150.000000 point.3=2.000000,0.00000,0.000000,0.00000,2100.0000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.4=2.000000,-12.600000,0.000000,-1.890000,3000.803000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.5=2.000000,-9.450000,-17.320000,0.450000,800.803000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.6=2.000000,-9.450000,17.320000,0.450000,800.803000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.7=2.000000,-27.00000,0.000000,5.000000,700.803000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.8=2.000000,-1.70000,0.000000,-4.90000,600.803000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.9=2.000000,-27.50000,0.000000,-0.20000,1574.803000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.10=2.000000,-9.450000,-9.0000,0.450000,1000.000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.11=2.000000,-9.450000,9.0000,0.450000,1000.000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 static_pitch=14.0 static_cg_height=5.86 tailwheel_lock = 1 [GeneralEngineData] engine_type=0 Engine.0=-1.7000,0.000000,0.000000 [piston_engine] cylinder_displacement=183.000000 compression_ratio=7.220000 number_of_cylinders=14 max_rated_rpm=2700.000000 max_rated_hp=1700.000000 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=41 min_design_mp=1.000000 critical_altitude=20600.000000 emergency_boost_type=2 emergency_boost_mp_offset=7.000000 emergency_boost_gain_offset=0.643000 emergency_boost_duration = 600 fuel_air_auto_mixture=1 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 power_scalar=1.000 fuel_flow_scalar=1.000000 [propeller] propeller_type=0 propeller_diameter=10.833000 propeller_blades=3 propeller_moi=33.0 beta_max=65.000000 beta_min=23.000000 min_gov_rpm=1800.000000 prop_tc=0.010000 gear_reduction_ratio=1.850000 fixed_pitch_beta=0.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 thrust_scalar=1.000 [keyboard_response] elevator= 300.000, 500.000 aileron= 450.000, 1000.000 rudder= 200.000, 1000.000 [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