[fltsim.0]
title=Republic P 47D-25 Thunderbolt 512th FS
sim=P47D4_25
model=P47D4_25

[General]
editable=0

[WEIGHT_AND_BALANCE]
max_gross_weight= 19400.000
empty_weight= 10291.1

reference_datum_position= 8.980, 0.000, 0.000
empty_weight_CG_position= -8.980, 0.000, 0.000

max_number_of_stations= 50
station_load.0= 180.000, -13.400, 0.000, 0.000

empty_weight_roll_MOI= 8253.000
empty_weight_pitch_MOI= 13454.000
empty_weight_yaw_MOI= 17273.000
empty_weight_coupled_MOI= 0.000

CG_forward_limit= 0.000
CG_aft_limit= 1.000


[fuel]
Center1= -8.350, 0.000, 0.000, 270.000, 0.000
Center2= -13.200, 0.000, 0.000, 100.000, 0.000
fuel_type= 1.000
number_of_tank_selectors= 1


[airplane_geometry]
wing_area= 300.000
wing_span= 40.780
wing_root_chord= 9.170
wing_dihedral= 6.000
wing_incidence= 1.000
wing_twist= 0.000
oswald_efficiency_factor= 0.65
wing_winglets_flag= 0
wing_sweep= 3.000
wing_pos_apex_lon= -6.690
wing_pos_apex_vert= -1.890
htail_area= 33.000
htail_span= 16.000
htail_pos_lon= -27.720
htail_pos_vert= 0.945
htail_incidence= 2.000
htail_sweep= 19.000
vtail_area= 26.000
vtail_span= 6.000
vtail_sweep= 30.000
vtail_pos_lon= -27.240
vtail_pos_vert= 1.890
elevator_area= 22.000
aileron_area= 26.300
rudder_area= 11.920
elevator_up_limit= 30.000
elevator_down_limit= 20.000
aileron_up_limit= 16.000
aileron_down_limit= 12.000
rudder_limit= 28.000
elevator_trim_limit= 7.000
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 3.00
system_type= 1
damaging-speed= 170.000
blowout-speed= 200.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000
flaps-position.1= 10.000
flaps-position.2= 20.000
flaps-position.3= 30.000
flaps-position.4= 40.000

[Reference Speeds]
flaps_up_stall_speed= 100.0
full_flaps_stall_speed= 87.000
cruise_speed= 202.000

[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= 1.000, -28.100, 0.000, -3.9, 2165.354, 0.000, 0.551, 180.000, 0.327, 2.500, 0.390, 3.000, 3.000, 0.000, 175.000, 180.000
point.1= 1.000, -7.480, -7.670, -8.0, 2165.354, 1.000, 1.400, 0.000, 0.547, 2.500, 0.891, 6.500, 7.500, 2.000, 175.000, 180.000
point.2= 1.000, -7.480, 7.670, -8.0, 2165.354, 2.000, 1.400, 0.000, 0.547, 2.500, 0.891, 9.500, 9.500, 3.000, 175.000, 180.000
point.3= 2.000, 0.0, 0.000, 0.00, 2100.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.4= 2.000, -6.480, 0.000, -4.0, 3000.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.5= 2.000, -8.980, -20.333, 0.000, 800.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.6= 2.000, -8.980, 20.333, 0.000, 800.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.7= 2.000, -30.913, 0.000, 6.95, 700.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.8= 2.000, 0.37, 0.000, -4.5, 750.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.9= 2.000, -31.0, 0.000, -0.5, 1200.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.10= 2.000, -8.980, -10.333, 0.000, 1000.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.11= 2.000, -8.980, 10.333, 0.000, 1000.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000

static_pitch= 11.66
static_cg_height= 6.93
tailwheel_lock = 1

[GeneralEngineData]
engine_type= 0
Engine.0= 0.37, 0.000, 0.000


[piston_engine]
cylinder_displacement= 155.780
compression_ratio= 6.650
number_of_cylinders= 18
max_rated_rpm= 2700.000
max_rated_hp= 2000.000
fuel_metering_type= 2
cooling_type= 0
normalized_starter_torque= 0.025
turbocharged= 1
max_design_mp= 52.000
min_design_mp= 1.000
critical_altitude= 30000.000
emergency_boost_type= 1
emergency_boost_mp_offset= 4.000
emergency_boost_gain_offset= 0.528
fuel_air_auto_mixture= 0
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= 1.000

[propeller]
propeller_type= 0
propeller_diameter= 13.0
propeller_blades= 4
propeller_moi= 77.000
beta_max= 65.000
beta_min= 18.500
min_gov_rpm= 1400.000
prop_tc= 0.010
gear_reduction_ratio= 2.000
fixed_pitch_beta= 20.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.000
beta_feather= 80.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
thrust_scalar=1.000

[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[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