// Vickers Type 60 Vimy Commercial flight dynamics. // By Jens B. Kristensen september 2005 [fltsim.0] title=Vimy Commercial sim=Vimy Commercial model= panel= sound= texture= kb_checklists=vimy_commercial_check kb_reference=vimy_commercial_ref description=Vickers Vimy Commercial\n\nModel and Flight Dynamics by Jens B. Kristensen september 2005. Wing and tail textures based on the Vickers Vimy included with FS9. ui_manufacturer=Vickers ui_type=Vimy Commercial ui_variation=Instone Air Line atc_heavy=0 atc_id=G-EASI atc_airline=SPEED BIRD atc_flight_number=1920 [fltsim.1] title=Vimy Commercial Cargo sim=Vimy Commercial model=cargo panel=late sound= texture=cargo kb_checklists=vimy_commercial_check kb_reference=vimy_commercial_ref description=Vickers Vimy Commercial\n\nModel and Flight Dynamics by Jens B. Kristensen september 2005. Wing and tail textures based on the Vickers Vimy included with FS9. ui_manufacturer=Vickers ui_type=Vimy Commercial ui_variation=Instone Air Line cargo atc_heavy=0 atc_id=G-EASI atc_airline=SPEED BIRD atc_flight_number=1923 [General] atc_type=Vickers atc_model=Vimy performance=Maximum Speed\n98 mph\t87 kts\t157 km\/hr\n\nCruise Speed\n70-85 mph 60-75 kts 112-135 km\/hr\n\nEngine\nTwo 360-hp Rolls-Royce Eagle VIII\n\nPropellers\nFour-bladed, fixed pitch, wood\n\nMaximum Range\n450 mi\t720 km\n\nService Ceiling\n8,000 ft\t2,438 m\n\nFuel Capacity\n158 gal\t598 L\n\nEmpty Weight\n7,790 lb\t3,513 kg\n\nMaximum Gross Weight\n12,500 lb\t5,638 kg\n\nLength\n42 ft, 8 in\t13.01 m\n\nWingspan\n68 ft, 1 in\t20.75 m\n\nHeight\n15 ft, 7-½ in 4.76 m\n\nSeating\n2 crew, 10 passengers [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 12500 empty_weight = 7790 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 1 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 13 station_load.0 = 170, 4.5, 0.75, 2, Pilot station_load.1 = 170, 4.5, -0.75, 2, co-pilot station_load.2 = 2500, -2, 0, 0, Payload empty_weight_pitch_MOI = 12538 empty_weight_roll_MOI = 55185 empty_weight_yaw_MOI = 64616 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 0.5 elevator_trim_effectiveness = 3 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 hi_alpha_on_roll = 1 hi_alpha_on_yaw = 1 p_factor_on_yaw = 1 torque_on_roll = 1 gyro_precession_on_roll = 1 gyro_precession_on_yaw = 1 [GeneralEngineData] engine_type = 0 Engine.0 = 4.4, -8.4, 2.5 Engine.1 = 4.4, 8.4, 2.5 fuel_flow_scalar = 1 min_throttle_limit = 0 [piston_engine] power_scalar = 1 cylinder_displacement = 103.37 compression_ratio = 6 number_of_cylinders = 12 max_rated_rpm = 2200 max_rated_hp = 360 fuel_metering_type = 1 cooling_type = 1 normalized_starter_torque = 0.091 turbocharged = 0 max_design_mp = 29.9 min_design_mp = 9 critical_altitude = 3000 emergency_boost_type = 0 emergency_boost_mp_offset = 0 emergency_boost_gain_offset = 0 fuel_air_auto_mixture = 0 auto_ignition = 0 emergency_boost_duration = 0 max_rpm_mechanical_efficiency_scalar = 1 idle_rpm_mechanical_efficiency_scalar = 1 max_rpm_friction_scalar = 1 idle_rpm_friction_scalar = 1 [propeller] thrust_scalar = 1 propeller_type = 1 propeller_diameter = 10.5 propeller_blades = 4 propeller_moi = 48.1 beta_max = 34 beta_min = 14 min_gov_rpm = 300 prop_tc = 0.01 gear_reduction_ratio = 1.667 fixed_pitch_beta = 24 low_speed_theory_limit = 70.57 prop_sync_available = 1 prop_deice_available = 1 prop_feathering_available = 1 prop_auto_feathering_available = 1 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 prop_reverse_available = 0 minimum_on_ground_beta = 1 minimum_reverse_beta = -14 rotation = -1, -1 [contact_points] point.0= 1.000, -30.36, 0.00, -2.39, 1500, 0.000, 0.500, 20.000, 0.404, 2.500, 0.600, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, 0.900, -8.300, -6.550, 1600.000, 0.000, 1.600, 0.000, 0.404, 2.500, 0.686, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, 0.900, 8.300, -6.550, 1600.000, 0.000, 1.600, 0.000, 0.404, 2.500, 0.682, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, 8.100, 0.010, -3.200, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -4.000, -34.500, -1.000, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.5= 2.000, -4.000, 34.500, -1.000, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.6= 2.000, -4.000, -34.500, 9.400, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.7= 2.000, -4.000, 34.500, 9.400, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.8= 2.000, -34.000, 0.000, 5.000, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 static_pitch = 6.9965 //degrees (pitch when loaded on ground) static_cg_height=6.155 //feet, altitude of CG when at rest on the ground [Views] eyepoint = 5.72, 0.60, 3.69 [Flaps.0] type= 0 span-outboard= 0.125 extending-time= 5.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 25 max_generator_alternator_amps = 60 light_panel = 0, 0.3, 3 engine_generator_map= 1,1 [anemometers] anemometer.0 = 9.6, 0.0, -2.2 //Position from Datum [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, 6, 0.00, 3.65, fx_vclight, light.1 = 4, 0, 0.00, 1, fx_vclight, light.2 = 4, -6, 0.00, 1, fx_vclight, light.3 = 3, 2.2, -31.36, 8.23 , fx_navred light.4 = 3, 2.2, 31.36, 8.23, fx_navgre [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 0 Com.1 = 1, 0 Nav.1 = 0, 0, 0 Adf.1 = 0 Transponder.1 = 0 Marker.1 = 0 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 startup=fx_engstrt_jenny windshield_rain_effect_available = 0 //Do not draw rain on this windshield [autopilot] autopilot_available= 1 flight_director_available= 0 pitch_takeoff_ga=0.0 default_vertical_speed=500.000000 autothrottle_available=1 //only for testing autothrottle_arming_required=0 direction_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=15.000000 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 autothrottle_takeoff_ga=0 autothrottle_max_rpm=95.000000 autothrottle_available=0 [fuel] Center1 = 2, 0, 7.9, 8, 0 Center2 = 0, 0, -2, 150, 0 fuel_type = 1 number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 1330 wing_span = 68 wing_root_chord = 19.55 //both wings together wing_dihedral = 3 wing_incidence = 3 wing_twist = 0 oswald_efficiency_factor = 1.3 // artificially higher than 1 due to two wings 1.3 = 2*0.65 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 4.889 wing_pos_apex_vert = 1.0 htail_area = 120 htail_span = 23 //biplane tail combined htail_pos_lon = -27.3 htail_pos_vert = 0 htail_incidence = 6 htail_sweep = 0 vtail_area = 27 vtail_span = 5.6 vtail_sweep = 0 vtail_pos_lon = -27.3 vtail_pos_vert = 0 elevator_area = 63 aileron_area = 242 rudder_area = 21.6 elevator_up_limit = 30 elevator_down_limit = 20 aileron_up_limit = 15 aileron_down_limit = 15 rudder_limit = 30 elevator_trim_limit = 25 spoiler_limit = 0 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 39 full_flaps_stall_speed = 39 cruise_speed = 70 max_indicated_speed = 130 max_mach = 0.2628 [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 [brakes] parking_brake = 0 //Parking brake available toe_brakes_scale = 0.0 //Brake scalar [stall_warning] // 0 = None, 1 = Suction, 2 = Electric. type = 0 [hydraulic_system] electric_pumps = 0 engine_map = 1, 1, 0, 0 normal_pressure = 1000 [attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0 = 1, 0 [direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind direction_indicator.0 = 1, 0 [airspeed_indicators] airspeed_indicator.0 = 1, 0
