// 0408221400 v1.0
// -{nnn}- is AIR file ref. Not many needed under fs9 and some values here are set to zero in the '*.air' file
[fltsim.0]
title=WhitleyVII
sim=WhitleyVII
model=
panel=
sound=
texture=
kb_checklists=whitley_check
kb_reference=whitley_ref
atc_id=YG-R
ui_manufacturer=Armstrong Whitworth
ui_type=AW38 "Whitley"
ui_variation=Mk VII
description=Coastal Command patrol aircraft.\nWith ASV. radar.
atc_id=Whitley
atc_airline=Air Force
atc_flight_number=YG-R
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 Rolls Royce Merlin X\n\nMaximum range\n1,2,300 nm with 1,000lb. bombload\n\nService ceiling\n20,000 ft\n\nFuel capacity\n1321 gal.US. 1100 gall.Imp.\n\nEmpty weight\n19,350 lb.\n\nMaximum gross weight\n33,950 lb. overload\n\nLength\n72.5 ft\n\nWingspan\n84 ft\n\nHeight\n15 ft.\n\nUseful load\n3,500 ~ 4,180lb."
[flight_tuning]
cruise_lift_scalar = 1.5
parasite_drag_scalar = 1.0
induced_drag_scalar = 2.2
elevator_effectiveness = 1.0
aileron_effectiveness = 0.5 // Reported as very heavy.
rudder_effectiveness = 1.0
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 = 33950 // (pounds)
empty_weight = 19350 // (pounds)
reference_datum_position = 0.00, 0, 0 // (feet) from FSim Ref. pos: (Chord/4,centerline, waterline)
empty_weight_CG_position = 0.86, 0, 0 // (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 = 80861 // -{no entries}-
empty_weight_roll_MOI = 77277
empty_weight_yaw_MOI = 154633
empty_weight_coupled_MOI = 0.0
[GeneralEngineData]
engine_type = 0 //0=Piston.
Engine.0 = 13.0, -9.48, 0.0 //(ft.) long, lat, vert. dist. from ref. datum
Engine.1 = 13.0, 9.48, 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= 137.42 //Cubic inches per cylinder
compression_ratio= 6.0
number_of_cylinders=12
max_rated_rpm= 3000
max_rated_hp= 1101 //Max rated HP ( Sound effect only )
fuel_metering_type= 1 // 1=Gravity Carburetor.
cooling_type= 1 // 1=Cooling type Liquid.
normalized_starter_torque= 0.06 //Starter torque factor
turbocharged= 1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 54 //Max design manifold pressure, (inHg)
min_design_mp= 1 //Min design manifold pressure, (inHg)
critical_altitude= 13000 //(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, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
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
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 ~ 2.05 actual
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 )
rotation= -1,-1
[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 = 4.0 //Degrees
wing_incidence = 8.5 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 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 = 56.0 //Knots True (KTAS)
full_flaps_stall_speed = 50.0 //Knots True (KTAS)
cruise_speed = 152.0 //Knots True (KTAS)
max_indicated_speed = 259.0 //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 = 7.0
static_cg_height = 8.0
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 = 28.55
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, 2.664, -39.438, 2.595, fx_navredm ,
light.1 = 3, 2.664, 39.453, 2.595, fx_navgrem ,
light.2 = 3, -50.500, 0.000, 1.054, fx_navwhi ,
light.3 = 4, 12.700, 0.000, 1.300, 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.)
LeftTip = 0.0, -11.0, 0.0, 219.0, 0.0 // == Main
RightTip= 0.0, 11.0, 0.0, 219.0, 0.0
LeftAux = 0.0, -4.8, 0.0, 114.0, 0.0
RightAux= 0.0, 4.8, 0.0, 114.0, 0.0
Center1 = 0.0, 0.0, 2.7, 186.0, 0.0
Center2 = 0.0, 0.0, -1.8, 469.0, 0.0 // Extra range tanks in bomb bay.
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 = 400.0 //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
