// 0409140100 v1.1
// -{nnn}- is AIR file ref. Not many used under fs9 and some values here are set to zero in the 'Whitley1.air' file
[fltsim.0]
title=Whitley1
sim=Whitley1
model=
panel=
sound=
texture=
kb_checklists=whitley1_check
kb_reference=whitley1_ref
atc_id_enable=0
atc_id=10-K
atc_airline=Air Force
atc_flight_number=10-K
ui_manufacturer=Armstrong Whitworth
ui_type=AW38 Whitley
ui_variation=Mk I
description=Light night bomber.
visual_damage=0
prop_anim_ratio=-1.76
[General]
atc_type=Armstrong Whitworth
atc_model=Whitley
editable=1
performance="Cruise speed\n190 mph 165 kts\n\nEngines\nTwo Armstrong Sidley Tiger XI engines\n\nMaximum range\n1,630 nm with 3,500lb. bombload\n\nService ceiling\n19,000 ft\n\nFuel capacity\n624 gal.US. 518 gall.Imp.\n\nEmpty weight\n19,000 lb.\n\nMaximum gross weight\n22,100 lb. \n\nLength\n72.5 ft\n\nWingspan\n84 ft.\n\nHeight\n15 ft.\n\nUseful load\n3,500 lb."
[flight_tuning]
cruise_lift_scalar = 1.6 // 1.5
parasite_drag_scalar = 1.5 // 1
induced_drag_scalar = 1.8 // 2.2
elevator_effectiveness = 0.7
aileron_effectiveness = 0.5 // 0.5 Reported as very heavy.
rudder_effectiveness = 0.7
pitch_stability = 1.0
roll_stability = 1.2
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
p_factor_on_yaw = 0.5
torque_on_roll = 1.0
gyro_precession_on_yaw = 1.0
gyro_precession_on_pitch = 1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 26500 // (pounds) [Mk III overload]
empty_weight = 16234 // (pounds) [Mk III]
reference_datum_position = 0.00, 0, 0 // (feet) from FSim Ref. pos: (Chord/4,centerline, waterline)
empty_weight_CG_position = 0.00, 0, 0 //0.86 (feet) from specified datum.
max_number_of_stations =10
station_load.0 = "0, 0, 0, 0," //Weight, Lat, Lon, Vert Position
;Moments of Inertia
empty_weight_pitch_MOI = 61984 // -{no entries}-
empty_weight_roll_MOI = 64833
empty_weight_yaw_MOI = 124481
empty_weight_coupled_MOI = 0.0
[GeneralEngineData]
engine_type = 0 //0=Piston.
Engine.0 = 15.0, -9.25, 0.0 //(ft.) long, lat, vert. dist. from ref. datum
Engine.1 = 15.0, 9.25, 0.0
fuel_flow_scalar= 1.0 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle.
max_contrail_temperature= -10 // A bit of fun.
[piston_engine] // -{no entry}-
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 100 //Cubic inches per cylinder [appx.]******
compression_ratio= 6.0
number_of_cylinders=14
max_rated_rpm= 3000
max_rated_hp= 935 //Max rated HP ( Sound effect only )
fuel_metering_type= 1 // 1=Gravity Carburetor.
cooling_type= 0 // 0=Cooling type Air.
normalized_starter_torque= 0.06 //Starter torque factor
turbocharged= 1 //Is it turbocharged? 1=TRUE
max_design_mp= 54 //Max design manifold pressure, (inHg)
min_design_mp= 1 //Min design manifold pressure, (inHg)
critical_altitude= 10000 //(ft.)Alt. to which the turbo. will give max. design MP.?? affects ceiling.
emergency_boost_type= 0 //0=None.
emergency_boost_mp_offset= 0
emergency_boost_gain_offset= 0
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE
max_rpm_mechanical_efficiency_scalar= 1.0
idle_rpm_mechanical_efficiency_scalar= 1.0
max_rpm_friction_scalar= 1.0
idle_rpm_friction_scalar= 0.4
[propeller] // -(no entry}-
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed
propeller_diameter= 12.7 //(feet)
propeller_blades= 3 // CCW
propeller_moi= 40.2 //Propeller moment of inertia
beta_max= 45.0 //(degrees)
beta_min= 15.0 //(degrees)
min_gov_rpm= 1400 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.95 //Propeller gear reduction ratio [a guess]
fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80.0 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 1 // 0=FALSE, 1=TRUE
prop_deice_available= 1 // 0=FALSE, 1=TRUE
prop_feathering_available= 1 // 0=FALSE, 1=TRUE ( Not implemented yet )
prop_auto_feathering_available= 0 // 0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering
beta_feather= 89.5 //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9 //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available= 0 // 0=FALSE, 1=TRUE
prop_reverse_available= 0 // 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees)
feathering_switches = 1 //Switches which invoke feathering ( Not implemented yet )
[airplane_geometry]
wing_area = 1232.0 //Square feet -{no entry}-
wing_span = 84.0 //Feet
wing_root_chord = 14.67 //Feet, NOT Root -- MAC
wing_dihedral = 2.0 //Degrees On thickness c/l
wing_incidence = 8.5 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.80 // 0.65 Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees,on Mean Average Chord (MAC)
wing_pos_apex_lon = 3.67 //Feet, long. dist. of MAC. LE. from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vert. dist. of MAC. LE. from reference point, positive going up
htail_area = 193.6 //Square feet -{no entry}-
htail_span = 31.44 //Feet
htail_pos_lon = -41.28 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 3.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.1 // +3.0 Degrees actual
htail_sweep = 5.0 //Degrees, on MAC
vtail_area = 38.0 //Square feet -{no entry}-
vtail_span = 8.58 //Feet, tip to body
vtail_sweep = 5.0 //Degrees, on MAC
vtail_pos_lon = -44.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 70.39 //Square feet -{320}-
aileron_area = 88.42 //Square feet
rudder_area = 56.0 //Square feet
elevator_up_limit = 17.0 //Degrees = 0.30 rad
elevator_down_limit = 15.0 //Degrees = 0.26 rad
aileron_up_limit = 20.0 //Degrees = 0.35 rad
aileron_down_limit = 15.0 //Degrees = 0.26 rad
rudder_limit = 30.0 //Degrees = 0.52 rad
elevator_trim_limit = 12.0 //Degrees = 0.21 rad
spoiler_limit = 0.0 //Degrees = 0.00 rad
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 85.0 //Knots True (KTAS)
full_flaps_stall_speed = 75.0 //Knots True (KTAS)
cruise_speed = 143.0 //Knots True (KTAS)
max_indicated_speed = 200.0 //Red line (KIAS)
//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
[contact_points]
// GEAR.
point.0=1, -37.38, 0.0, -3.4, 1200.0, 0, 0.6, 180.0, 0.42, 2.5, 0.87, 0.0, 0.0, 0, 0.0, 0.0
point.1=1, 2.70, -9.4, -8.4, 1600.0, 1, 2.1, 0.0, 0.50, 2.5, 0.85, 4.2, 5.2, 2, 152.0, 200.0
point.2=1, 2.70, 9.4, -8.4, 1600.0, 2, 2.1, 0.0, 0.50, 2.5, 0.85, 4.5, 5.8, 3, 152.0, 200.0
// SCRAPES.
point.3=2, 22.2, 0.0, -1.9, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0 // Nose.
point.4=2, -50.9, 0.0, 0.5, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0 // Tail.
point.5=2, 0.0, -42.0, 2.7, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0 // Left.
point.6=2, 0.0, 42.0, 2.7, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0 // Right.
point.7=2, 13.7, -9.3, -5.6, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0 // L.Prop.
point.8=2, 13.7, -9.3, -5.6, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0 // R.Prop.
point.9=2, -44.3, -7.5, 9.8, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 7, 0.0, 0.0 // L.Fin.
point.10=2,-44.3, 7.5, 9.8, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 8, 0.0, 0.0 // R.Fin.
static_pitch = 7.5
static_cg_height = 7.5
gear_system_type=1 //Hydraulic -{no entry}-
tailwheel_lock = 0
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 31.51 //Flap angle that activates warning at idle
flap_limit_power = 31.51 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.3 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[flaps.0] //Trailing Edge Flaps -{524}-
type = 1 // 1 - tail.
span-outboard = 0.46 // 0.0 .. 1.0
extending-time = 7 // seconds
flaps-position.0 = 0 // degrees = 0.00 rad
flaps-position.1 = 15 // degrees = 0.26 rad
flaps-position.2 = 30 // degrees = 0.52 rad
flaps-position.3 = 60 // degrees = 1.05 rad
damaging-speed = 152 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 1.0
drag_scalar = 1.5
pitch_scalar= 1.5
system_type = 1 // 1=Hydraulic.
[electrical]
max_battery_voltage = 25.2
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[Views]
eyepoint = 10.4, -0.9, 3.4 // z,x,y.
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 2.692, -39.438, 1.309, fx_navredm ,
light.1 = 3, 2.693, 39.453, 1.349, fx_navgrem ,
light.2 = 3, -48.698, 0.000, 1.051, fx_navwhi ,
light.3 = 4, 12.750, 0.000, 2.250, fx_vclight,
light.4 = 5, 2.069, -24.550, 1.306, fx_landing, // Beam done in FSDS.
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator =200, 1000
aileron =200, 1000
rudder =200, 1000
[fuel] //Long. Lat. Vertical (feet), Usable, Unusable (gallons US.)
LeftMain = 0.0, -15.0, 0.0, 219.0, 0.0
RightMain= 0.0, 15.0, 0.0, 219.0, 0.0
Center1 = 0.0, 0.0, 2.7, 186.0, 0.0
fuel_type = 1 // 1 = Avgas
number_of_tank_selectors = 2
electric_pump=1
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 0
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1 // Not authentic but Autopilot needs G/S
Nav.2 = 1, 1, 0
Adf.1 = 1
Adf.2 = 0
Transponder.1 = 1 // Not authentic but ATC needs this?
Marker.1 = 0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[hydraulic_system]
normal_pressure = 800.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
// Vacuum systems -{1512}- AIR file entry needed for vacuum selector and gauge.
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=1
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0
[stall_warning]
type=1
//=======================================================================================================
[autopilot] // -{ 1199 & 1203}- a/c MAY? have had a basic AP.
autopilot_available=1
flight_director_available=0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator =1
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain = 0.0
default_bank_mode=2 //Default to Heading Hold
[forcefeedback]
ground_bumps_magnitude1=2600 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000 ; in microseconds
