[fltsim.0] title=CW-1 sim=CW-1 model= panel= sound= texture= kb_checklists= ui_manufacturer=Curtiss prop_anim_ratio=-1.76 atc_id_color=0000000000 visual_damage=0 description=The CW-1 was unique because it cost only $1500. It was easy to fly and very popular with its owners. Several hundreds were produced before the depression of the 1930's ruined the market. [General] atc_type=Curtiss atc_model=CW-1 editable=0 performance=Maximum Speed\t75 mph\nCruise Speed\t65 mph\nMaximum Range\t400 nm\nService Ceiling\t18,100 ft\nFuel Capacity\t8 U.S gal\nMax Gross Weight\t975 lb\nSeating\t\t2\nUseful Load\t420 lb\nPower Szekely SR-3-0 3 cylinder @45 hp\n [weight_and_balance] // ACM V2.3 max_gross_weight = 975 empty_weight = 555 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 313.8 empty_weight_roll_MOI = 313.9 empty_weight_yaw_MOI = 642.2 empty_weight_coupled_MOI = 0 max_number_of_stations = 3 station_load.0 = 250, 0.5, 0, 0 station_load.1 = station_load.2 = [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1.0 engine.0 = -0.01, 0, 0, [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 number_of_tank_selectors = 1 Center1 = 0.01, 0, -0.07, 8, 0 electric_pump=0 [contact_points] static_pitch = 9 static_cg_height = 3 max_number_of_points = 7 point.0 = 1, -13.8609, 0, -1.1661, 1200, 0, 0.238, 30, 0.3, 2.5, 0.2, 0, 0, 0, 0, 0 point.1 = 1, 0.2991, -2.5039, -3.50, 1600, 1, 0.728, 0, 0.54, 2.5, 0.65, 0, 0, 2, 0, 0 point.2 = 1, 0.3307, 2.5039, -3.50, 1600, 2, 0.728, 0, 0.54, 2.5, 0.65, 0, 0, 3, 0, 0 point.3 = 2, -1, -18.8148, 2.2952, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -1, 18.6905, 2.4191, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -14.4322, 0, -0.0736, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 4.9159, 0, -1.6837, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 [keyboard_response] elevator = 200, 1000 aileron = 200, 1000 rudder = 200, 1000 [forcefeedback] ground_bumps_magnitude1 = 2600 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5.0 ground_bumps_slope1 = 0.6 ground_bumps_magnitude2 = 1200 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.085 ground_bumps_slope2 = 0.65 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 3500000 [airplane_geometry] wing_area = 176 wing_span = 39.6 wing_root_chord = 4.8 wing_dihedral = 1.1 wing_incidence = 2.5 wing_twist = -1.0 oswald_efficiency_factor = 0.4 wing_winglets_flag = 0 wing_sweep = 0.0 wing_pos_apex_lon = 1.31 wing_pos_apex_vert = 2.1 htail_area = 18.2 htail_span = 9.6 htail_pos_lon = -13.4 htail_pos_vert = 1.3 htail_incidence = 0.2 htail_sweep = 30.0 vtail_area = 13.0 vtail_span = 4.44 vtail_sweep = 38.0 vtail_pos_lon = -13.5 vtail_pos_vert = 1.6 elevator_area = 10.64 aileron_area = 9.6 rudder_area = 6.55 elevator_up_limit = 22.0 elevator_down_limit = 22.0 aileron_up_limit = 20.0 aileron_down_limit = 20.0 rudder_limit = 22.0 elevator_trim_limit = 10.0 spoiler_limit = 0.0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 [electrical] max_battery_voltage = 0 generator_alternator_voltage = 0 max_generator_alternator_amps = 60 electric_always_available = 0 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 p_factor_on_yaw = 0.3 torque_on_roll = 0.3 gyro_precession_on_yaw = 0.3 gyro_precession_on_pitch = 0.3 [Flaps.0] type= 0 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=64 //Cubic inches per cylinder compression_ratio=7.5 //Compression ratio number_of_cylinders=3 //Number of cylinders max_rated_rpm=2600 //Max rated RPM max_rated_hp=45 //Max rated HP fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque=0.3 //Starter torque factor turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=0 //Max design manifold pressure, (inHg) min_design_mp=0 //Min design manifold pressure, (inHg) critical_altitude=0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost 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 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction [propeller] thrust_scalar=0.85 //Propeller thrust scalar propeller_type=1 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=6.25 //Propeller Diameter, (feet) propeller_blades=2 //Number of propeller blades propeller_moi=3.78 //Propeller moment of inertia beta_max=0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=0 //Miminum governed RPM prop_tc=0.1 //Prop time-constant gear_reduction_ratio=1.0 //Propeller gear reduction ratio fixed_pitch_beta=13.75 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=0 //Minimum RPM for prop feathering beta_feather=0 //Feathering pitch angle (degrees) power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller in feather defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees) //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 [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.5 //Brake scalar differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected [hydraulic_system] normal_pressure = 0.0 //PSI [Views] eyepoint=-1.684, -0.686, 1.241 [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 [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=0,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 0 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [Reference Speeds] flaps_up_stall_speed=33.0 //Knots True (KTAS) full_flaps_stall_speed=33.0 //Knots True (KTAS) cruise_speed=63.0 //Knots True (KTAS) max_indicated_speed = 106 //Red line (KIAS) [autopilot] autopilot_available=0 flight_director_available=0 [stall_warning] type=1