[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