diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/flight_model.cfg b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/flight_model.cfg new file mode 100644 index 0000000..1a8513c --- /dev/null +++ b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/flight_model.cfg @@ -0,0 +1,399 @@ +//TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.0_GE_F 15MAY25 + +[VERSION] +//KH Bump major +major = 4 +minor = 1 + +[WEIGHT_AND_BALANCE] +max_gross_weight = 630500 +empty_weight = 248567 +reference_datum_position = 0, 0, 0 +empty_weight_CG_position = -13.3, 0, 0 +CG_forward_limit = 0.12 +CG_aft_limit = 0.34 +empty_weight_pitch_MOI = 20897456 +empty_weight_roll_MOI = 6368555 +empty_weight_yaw_MOI = 40761191 +empty_weight_coupled_MOI = 0 +activate_mach_limit_based_on_cg = 0 +activate_cg_limit_based_on_mach = 0 +max_number_of_stations = 15 +//KH START Empty default +station_load.0=0, 82.0, -2.0, 4.0, Pilot, 1 +station_load.1=0, 82.0, 2.0, 4.0, First Officer, 2 +station_load.2=0, 80.0, 3.3, 4.0, Engineer, 0 +station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0 +station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0 +station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0 +station_load.6=0, 20.0, 5.0, 4.0, Upper zone 2 R, 0 +station_load.7=0, -20.0, -5.0, 4.0, Upper zone 3 L, 0 +station_load.8=0, -20.0, 5.0, 4.0, Upper zone 3 R, 0 +station_load.9=0, -50.0, -5.0, 4.0, Upper zone 4 L, 0 +station_load.10=0, -50.0, 5.0, 4.0, Upper zone 4 R, 0 +station_load.11=0, 30.0, 0.0, -4.5, Lower forward cargo, 0 +station_load.12=0, -30.0, 0.0, -4.5, Lower rear cargo, 0 +station_load.13=0, 5.0, -2.0, -4.5, Left aux tank, 0 +station_load.14=0, 5.0, 2.0, -4.5, Right aux tank, 0 +//KH END + +[CONTACT_POINTS] +static_pitch = 0 +static_cg_height = 16.4 +gear_system_type = 1 +tailwheel_lock = 0 +max_number_of_points = 16 +gear_locked_on_ground = 0 +gear_locked_above_speed = -1 +max_speed_full_steering = 25 +min_available_steering_angle_pct = 0.2 +max_speed_decreasing_steering = 45 +max_speed_full_steering_castering = 20 +max_speed_decreasing_steering_castering = 35 +emergency_extension_type = 2 +hyd_need_power_to_function= 0 +min_castering_angle = 0.05236 +max_castering_angle = 1.32645 +allow_stopped_steering = 1 +point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 +point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 +point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8 +point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8 +point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1 +point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1 +point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 + +[FUEL] +LeftMain = -20.00, -38.00, -1.0, 8938, 10.00 +RightMain = -20.00, 38.00, -1.0, 8938, 10.00 +Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00 +Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00 +Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00 +LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00 +RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 +External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 +//KH From 5.00, -2.00, -3.00, 0.00, 10.00 +LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 +//KH From 5.00, 2.00, -3.00, 0.00, 10.0 +RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00 +fuel_type = 2 +number_of_tank_selectors = 3 +electric_pump = 0 +engine_driven_pump = 1 +manual_transfer_pump = 0 +manual_pump = 0 +anemometer_pump = 0 +fuel_dump_rate = 0.02 +default_fuel_tank_selector.1 = 1 +default_fuel_tank_selector.2 = 1 +default_fuel_tank_selector.3 = 1 + +[AIRPLANE_GEOMETRY] +wing_area = 3648 +wing_span = 170.5 +wing_root_chord = 34.68 +wing_camber = 1 +wing_thickness_ratio = 0.04 +wing_dihedral = 2.2 +wing_incidence = 1.5 +wing_twist = -0.5 +oswald_efficiency_factor = 0.72 +wing_winglets_flag = 1 +wing_sweep = 38 +wing_pos_apex_lon = 1 +wing_pos_apex_vert = -2.75 +htail_area = 920 +htail_span = 59.5 +htail_pos_lon = -88 +htail_pos_vert = 5.0 +htail_incidence = 0.8 +htail_sweep = 36.5 +htail_thickness_ratio = 0.02 +vtail_area = 760 +vtail_span = 28.1 +vtail_sweep = 43 +vtail_pos_lon = -79.5 +vtail_pos_vert = 28 +vtail_thickness_ratio = 0.03 +fuselage_length = 202.16 +fuselage_diameter = 19.75 +fuselage_center_pos = 10, 0, 1.0 +elevator_area = 327.0 +aileron_area = 225.0 +rudder_area = 190.0 +elevator_up_limit = 25 +elevator_down_limit = 15 +aileron_up_limit = 25 +aileron_down_limit = 15 +rudder_limit = 23 +rudder_trim_limit = 20 +elevator_trim_limit = 30 +spoiler_limit = 60 +spoilerons_available = 1 +aileron_to_spoileron_gain = 3 +min_ailerons_for_spoilerons = 10 +min_flaps_for_spoilerons = 0 +spoiler_extension_time = 2.0 +spoiler_handle_available = 1 +auto_spoiler_available = 1 +auto_spoiler_auto_retracts = 0 +auto_spoiler_min_speed = 72 +positive_g_limit_flaps_up = 5.0 +positive_g_limit_flaps_down = 4.0 +negative_g_limit_flaps_up = -4.0 +negative_g_limit_flaps_down = -3.0 +load_safety_factor = 1.5 +elevator_trim_neutral = -1 +aileron_to_rudder_scale = 0 +flap_to_aileron_scale = 0 +fly_by_wire = 0 +elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5 +aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4 +rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7 +elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00 + +[AERODYNAMICS] +lift_coef_pitch_rate = -8.09375 +lift_coef_daoa = 2.68359 +lift_coef_delta_elevator = -0.28906 +lift_coef_horizontal_incidence = 0.91357 +lift_coef_flaps = 1 +lift_coef_spoilers = 0 +drag_coef_zero_lift = 0.02539 +drag_coef_flaps = 0.1889 +drag_coef_gear = 0.0549 +drag_coef_spoilers = 0.05207 +side_force_slip_angle = -0.77392 +side_force_roll_rate = 0.15478 +side_force_yaw_rate = 0 +side_force_delta_rudder = -0.14746 +pitch_moment_horizontal_incidence = 4.24755 +pitch_moment_delta_elevator = -2.37011 +pitch_moment_delta_trim = 0 +pitch_moment_pitch_damping = -214.1455 +pitch_moment_aoa_0 = 0.11621 +pitch_moment_daoa = 8.87255 +pitch_moment_flaps = 0.0105 +pitch_moment_gear = 0.0171 +pitch_moment_spoilers = 0 +pitch_moment_delta_elevator_propwash = -2.37011 +pitch_moment_pitch_propwash = -214.1455 +roll_moment_slip_angle = 0.26855 +roll_moment_roll_damping = -3.40869 +roll_moment_yaw_rate = -0.27197 +roll_moment_spoilers = 0.07 +roll_moment_delta_aileron = -0.34521 +roll_moment_delta_rudder = 0.01660 +roll_moment_delta_aileron_trim_scalar = -0.2 +yaw_moment_slip_angle = 0.18066 +yaw_moment_roll = 0.07470 +yaw_moment_yaw_damping = -2.49023 +yaw_moment_yaw_propwash = 0 +yaw_moment_delta_aileron = -0.00683 +yaw_moment_delta_rudder = 0.07128 +yaw_moment_delta_rudder_propwash = 0.075 +yaw_moment_delta_rudder_trim_scalar = -0.2 +compute_aero_center = 0 +aero_center_lift = -13.75 +lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0 +lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0 +lift_coef_mach_table = 0:1 +lift_coef_delta_elevator_mach_table = 0:0 +lift_coef_daoa_mach_table = 0:0 +lift_coef_pitch_rate_mach_table = 0:0 +lift_coef_horizontal_incidence_mach_table = 0:0 +drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337 +side_force_slip_angle_mach_table = 0:0 +side_force_delta_rudder_mach_table = 0:0 +side_force_yaw_rate_mach_table = 0:0 +side_force_roll_rate_mach_table = 0:0 +pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2 +pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1 +pitch_moment_horizontal_incidence_aoa_table = 0:1 +pitch_moment_daoa_aoa_table = 0:1 +pitch_moment_pitch_alpha_table = 0:1 +pitch_moment_delta_elevator_mach_table = 0:0 +pitch_moment_daoa_mach_table = 0:0 +pitch_moment_pitch_rate_mach_table = 0:0 +pitch_moment_horizontal_incidence_mach_table = 0:0 +pitch_moment_aoa_0_mach_table = 0:0 +roll_moment_aoa_table = 0:0 +roll_moment_slip_angle_aoa_table = 0:1 +roll_moment_roll_rate_aoa_table = 0:1 +roll_moment_delta_aileron_aoa_table = 0:1 +roll_moment_slip_angle_mach_table = 0:0 +roll_moment_delta_rudder_mach_table = 0:0 +roll_moment_delta_aileron_mach_table = 0:0 +roll_moment_yaw_rate_mach_table = 0:0 +roll_moment_roll_rate_mach_table = 0:0 +yaw_moment_aoa_table = 0:0 +yaw_moment_slip_angle_aoa_table = 0:1 +yaw_moment_yaw_rate_aoa_table = 0:1 +yaw_moment_delta_rudder_aoa_table = 0:1 +yaw_moment_slip_angle_mach_table = 0:0 +yaw_moment_delta_rudder_mach_table = 0:0 +yaw_moment_delta_aileron_mach_table = 0:0 +yaw_moment_yaw_rate_mach_table = 0:0 +yaw_moment_roll_rate_mach_table = 0:0 +elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1 +aileron_scaling_table = -0.785:1 ;0:1 +rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1 +elevator_lift_coef=3 +rudder_lift_coef=2 +aileron_load_factor_effectiveness_table = 0:1 +lift_coef_at_drag_zero = 0.1 +lift_coef_at_drag_zero_flaps = 0.1 + +[FLIGHT_TUNING] +modern_fm_only = 1 +cruise_lift_scalar = 1 +parasite_drag_scalar = 1 +induced_drag_scalar = 1 +flap_induced_drag_scalar = 1 +elevator_effectiveness = 1 +elevator_maxangle_scalar = 1 +aileron_effectiveness = 1 +rudder_effectiveness = 1 +rudder_maxangle_scalar = 1 +pitch_stability = 5 +roll_stability = 1 +yaw_stability = 1 +pitch_gyro_stability = 1 +roll_gyro_stability = 1 +yaw_gyro_stability = 1 +empty_CG_deviation_limit=0 +elevator_trim_effectiveness = 1.5 +aileron_trim_effectiveness = 1 +rudder_trim_effectiveness = 1 +hi_alpha_on_roll = 0 +hi_alpha_on_yaw = 0 +p_factor_on_yaw = 0 +torque_on_roll = 0 +gyro_precession_on_roll = 0 +gyro_precession_on_yaw = 0 +engine_wash_on_roll = 0 +wingflex_scalar = 2 +wingflex_offset = 0 +stall_coef_at_min_weight = 0.71 +ground_crosswind_effect_zero_speed=10 +ground_crosswind_effect_max_speed=150 +ground_high_speed_steeringwheel_static_friction_scalar=1.5 +ground_high_speed_otherwheel_static_friction_scalar=1.2 + +[REFERENCE SPEEDS] +full_flaps_stall_speed = 115 +flaps_up_stall_speed = 149 +cruise_speed = 345 +cruise_mach = 0.85 +crossover_speed = 330 +max_mach = 0.9 +max_indicated_speed = 395 +max_flaps_extended = 170 +normal_operating_speed = 325 +airspeed_indicator_max = 562.5 +rotation_speed_min = 145 +climb_speed = 250 +cruise_alt = 41000 +takeoff_speed = 165 +spawn_cruise_altitude = 5000 +spawn_descent_altitude = 500 +best_angle_climb_speed = 0 +approach_speed = 0 +best_glide = 0 +max_gear_extended = 200 + +[INTERACTIVE POINTS] +number_of_interactive_points = 2 +interactive_point.0 = 0.4, 75.65, -8.12, -0.567, 0, 0, 0, -75, 33, 2, 33, 2, 2, 33 +interactive_point.1 = 0.4, 33.3, 6.28, -7.18, 1, 0, 0, 90, 0, 0, 0, 0, 0, 0 + +[STALL PROTECTION] +stall_protection = 1 ; Alpha Protection +off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit) +off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit) +on_limit = 14 ; Alpha above which the Alpha Protection timer starts +on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered +timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered + +;===================== FLAPS ===================== + +[FLAPS.0] +type = 1 +system_type = 1 +span-outboard = 0.25 +extending-time = 22 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.1 +drag_scalar = 1.1 +pitch_scalar = 1 +max_on_ground_position = 7 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 0, -1, 0 +flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 +flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 +flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 +flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 +flaps-position.6 = 35, 160, 0.32, 1 +flaps-position.7 = 50, 150, 0.33, 1 + +[FLAPS.1] +type = 1 +system_type = 1 +span-outboard = 0.7 +extending-time = 23 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.1 +drag_scalar = 1.1 +pitch_scalar = 1 +max_on_ground_position = 7 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 0, -1, 0 +flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 +flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 +flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 +flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 +flaps-position.6 = 35, 160, 0.32, 1 +flaps-position.7 = 50, 150, 0.33, 1 + +[FLAPS.2] +type = 2 +system_type = 1 +span-outboard = 0.2 +extending-time = 8 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.5 +drag_scalar = 0.75 +pitch_scalar = 1 +max_on_ground_position = 1 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 20, 215, 0.5, 0.5 + +[FLAPS.3] +type = 2 +system_type = 1 +span-outboard = 0.7 +extending-time = 21 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.5 +drag_scalar = 0.75 +pitch_scalar = 1 +max_on_ground_position = 1 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 20, 215, 0.5, 0.5 diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/flight_model.cfg b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/flight_model.cfg new file mode 100644 index 0000000..2988df9 --- /dev/null +++ b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/flight_model.cfg @@ -0,0 +1,399 @@ +//TFDi Designs MD-11F (P&W PW4660) vRC1.7.0_PW_F 15MAY25 + +[VERSION] +//KH Bump major +major = 4 +minor = 1 + +[WEIGHT_AND_BALANCE] +max_gross_weight = 630500 +empty_weight = 248567 +reference_datum_position = 0, 0, 0 +empty_weight_CG_position = -13.3, 0, 0 +CG_forward_limit = 0.12 +CG_aft_limit = 0.34 +empty_weight_pitch_MOI = 20897456 +empty_weight_roll_MOI = 6368555 +empty_weight_yaw_MOI = 40761191 +empty_weight_coupled_MOI = 0 +activate_mach_limit_based_on_cg = 0 +activate_cg_limit_based_on_mach = 0 +max_number_of_stations = 15 +//KH START Empty default +station_load.0=0, 82.0, -2.0, 4.0, Pilot, 1 +station_load.1=0, 82.0, 2.0, 4.0, First Officer, 2 +station_load.2=0, 80.0, 3.3, 4.0, Engineer, 0 +station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0 +station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0 +station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0 +station_load.6=0, 20.0, 5.0, 4.0, Upper zone 2 R, 0 +station_load.7=0, -20.0, -5.0, 4.0, Upper zone 3 L, 0 +station_load.8=0, -20.0, 5.0, 4.0, Upper zone 3 R, 0 +station_load.9=0, -50.0, -5.0, 4.0, Upper zone 4 L, 0 +station_load.10=0, -50.0, 5.0, 4.0, Upper zone 4 R, 0 +station_load.11=0, 30.0, 0.0, -4.5, Lower forward cargo, 0 +station_load.12=0, -30.0, 0.0, -4.5, Lower rear cargo, 0 +station_load.13=0, 5.0, -2.0, -4.5, Left aux tank, 0 +station_load.14=0, 5.0, 2.0, -4.5, Right aux tank, 0 +//KH END + +[CONTACT_POINTS] +static_pitch = 0 +static_cg_height = 16.4 +gear_system_type = 1 +tailwheel_lock = 0 +max_number_of_points = 16 +gear_locked_on_ground = 0 +gear_locked_above_speed = -1 +max_speed_full_steering = 25 +min_available_steering_angle_pct = 0.2 +max_speed_decreasing_steering = 45 +max_speed_full_steering_castering = 20 +max_speed_decreasing_steering_castering = 35 +emergency_extension_type = 2 +hyd_need_power_to_function= 0 +min_castering_angle = 0.05236 +max_castering_angle = 1.32645 +allow_stopped_steering = 1 +point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 +point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 +point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8 +point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8 +point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1 +point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1 +point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 + +[FUEL] +LeftMain = -20.00, -38.00, -1.0, 8938, 10.00 +RightMain = -20.00, 38.00, -1.0, 8938, 10.00 +Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00 +Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00 +Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00 +LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00 +RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 +External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 +//KH From 5.00, -2.00, -3.00, 0.00, 10.00 +LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 +//KH From 5.00, 2.00, -3.00, 0.00, 10.0 +RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00 +fuel_type = 2 +number_of_tank_selectors = 3 +electric_pump = 0 +engine_driven_pump = 1 +manual_transfer_pump = 0 +manual_pump = 0 +anemometer_pump = 0 +fuel_dump_rate = 0.02 +default_fuel_tank_selector.1 = 1 +default_fuel_tank_selector.2 = 1 +default_fuel_tank_selector.3 = 1 + +[AIRPLANE_GEOMETRY] +wing_area = 3648 +wing_span = 170.5 +wing_root_chord = 34.68 +wing_camber = 1 +wing_thickness_ratio = 0.04 +wing_dihedral = 2.2 +wing_incidence = 1.5 +wing_twist = -0.5 +oswald_efficiency_factor = 0.72 +wing_winglets_flag = 1 +wing_sweep = 38 +wing_pos_apex_lon = 1 +wing_pos_apex_vert = -2.75 +htail_area = 920 +htail_span = 59.5 +htail_pos_lon = -88 +htail_pos_vert = 5.0 +htail_incidence = 0.8 +htail_sweep = 36.5 +htail_thickness_ratio = 0.02 +vtail_area = 760 +vtail_span = 28.1 +vtail_sweep = 43 +vtail_pos_lon = -79.5 +vtail_pos_vert = 28 +vtail_thickness_ratio = 0.03 +fuselage_length = 200.92 +fuselage_diameter = 19.75 +fuselage_center_pos = 10, 0, 1.0 +elevator_area = 327.0 +aileron_area = 225.0 +rudder_area = 190.0 +elevator_up_limit = 25 +elevator_down_limit = 15 +aileron_up_limit = 25 +aileron_down_limit = 15 +rudder_limit = 23 +rudder_trim_limit = 20 +elevator_trim_limit = 30 +spoiler_limit = 60 +spoilerons_available = 1 +aileron_to_spoileron_gain = 3 +min_ailerons_for_spoilerons = 10 +min_flaps_for_spoilerons = 0 +spoiler_extension_time = 2.0 +spoiler_handle_available = 1 +auto_spoiler_available = 1 +auto_spoiler_auto_retracts = 0 +auto_spoiler_min_speed = 72 +positive_g_limit_flaps_up = 5.0 +positive_g_limit_flaps_down = 4.0 +negative_g_limit_flaps_up = -4.0 +negative_g_limit_flaps_down = -3.0 +load_safety_factor = 1.5 +elevator_trim_neutral = -1 +aileron_to_rudder_scale = 0 +flap_to_aileron_scale = 0 +fly_by_wire = 0 +elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5 +aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4 +rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7 +elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00 + +[AERODYNAMICS] +lift_coef_pitch_rate = -8.09375 +lift_coef_daoa = 2.68359 +lift_coef_delta_elevator = -0.28906 +lift_coef_horizontal_incidence = 0.91357 +lift_coef_flaps = 1 +lift_coef_spoilers = 0 +drag_coef_zero_lift = 0.02539 +drag_coef_flaps = 0.1889 +drag_coef_gear = 0.0549 +drag_coef_spoilers = 0.05207 +side_force_slip_angle = -0.77392 +side_force_roll_rate = 0.15478 +side_force_yaw_rate = 0 +side_force_delta_rudder = -0.14746 +pitch_moment_horizontal_incidence = 4.24755 +pitch_moment_delta_elevator = -2.37011 +pitch_moment_delta_trim = 0 +pitch_moment_pitch_damping = -214.1455 +pitch_moment_aoa_0 = 0.11621 +pitch_moment_daoa = 8.87255 +pitch_moment_flaps = 0.0105 +pitch_moment_gear = 0.0171 +pitch_moment_spoilers = 0 +pitch_moment_delta_elevator_propwash = -2.37011 +pitch_moment_pitch_propwash = -214.1455 +roll_moment_slip_angle = 0.26855 +roll_moment_roll_damping = -3.40869 +roll_moment_yaw_rate = -0.27197 +roll_moment_spoilers = 0.07 +roll_moment_delta_aileron = -0.34521 +roll_moment_delta_rudder = 0.01660 +roll_moment_delta_aileron_trim_scalar = -0.2 +yaw_moment_slip_angle = 0.18066 +yaw_moment_roll = 0.07470 +yaw_moment_yaw_damping = -2.49023 +yaw_moment_yaw_propwash = 0 +yaw_moment_delta_aileron = -0.00683 +yaw_moment_delta_rudder = 0.07128 +yaw_moment_delta_rudder_propwash = 0.075 +yaw_moment_delta_rudder_trim_scalar = -0.2 +compute_aero_center = 0 +aero_center_lift = -13.75 +lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0 +lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0 +lift_coef_mach_table = 0:1 +lift_coef_delta_elevator_mach_table = 0:0 +lift_coef_daoa_mach_table = 0:0 +lift_coef_pitch_rate_mach_table = 0:0 +lift_coef_horizontal_incidence_mach_table = 0:0 +drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337 +side_force_slip_angle_mach_table = 0:0 +side_force_delta_rudder_mach_table = 0:0 +side_force_yaw_rate_mach_table = 0:0 +side_force_roll_rate_mach_table = 0:0 +pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2 +pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1 +pitch_moment_horizontal_incidence_aoa_table = 0:1 +pitch_moment_daoa_aoa_table = 0:1 +pitch_moment_pitch_alpha_table = 0:1 +pitch_moment_delta_elevator_mach_table = 0:0 +pitch_moment_daoa_mach_table = 0:0 +pitch_moment_pitch_rate_mach_table = 0:0 +pitch_moment_horizontal_incidence_mach_table = 0:0 +pitch_moment_aoa_0_mach_table = 0:0 +roll_moment_aoa_table = 0:0 +roll_moment_slip_angle_aoa_table = 0:1 +roll_moment_roll_rate_aoa_table = 0:1 +roll_moment_delta_aileron_aoa_table = 0:1 +roll_moment_slip_angle_mach_table = 0:0 +roll_moment_delta_rudder_mach_table = 0:0 +roll_moment_delta_aileron_mach_table = 0:0 +roll_moment_yaw_rate_mach_table = 0:0 +roll_moment_roll_rate_mach_table = 0:0 +yaw_moment_aoa_table = 0:0 +yaw_moment_slip_angle_aoa_table = 0:1 +yaw_moment_yaw_rate_aoa_table = 0:1 +yaw_moment_delta_rudder_aoa_table = 0:1 +yaw_moment_slip_angle_mach_table = 0:0 +yaw_moment_delta_rudder_mach_table = 0:0 +yaw_moment_delta_aileron_mach_table = 0:0 +yaw_moment_yaw_rate_mach_table = 0:0 +yaw_moment_roll_rate_mach_table = 0:0 +elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1 +aileron_scaling_table = -0.785:1 ;0:1 +rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1 +elevator_lift_coef=3 +rudder_lift_coef=2 +aileron_load_factor_effectiveness_table = 0:1 +lift_coef_at_drag_zero = 0.1 +lift_coef_at_drag_zero_flaps = 0.1 + +[FLIGHT_TUNING] +modern_fm_only = 1 +cruise_lift_scalar = 1 +parasite_drag_scalar = 1 +induced_drag_scalar = 1 +flap_induced_drag_scalar = 1 +elevator_effectiveness = 1 +elevator_maxangle_scalar = 1 +aileron_effectiveness = 1 +rudder_effectiveness = 1 +rudder_maxangle_scalar = 1 +pitch_stability = 5 +roll_stability = 1 +yaw_stability = 1 +pitch_gyro_stability = 1 +roll_gyro_stability = 1 +yaw_gyro_stability = 1 +empty_CG_deviation_limit=0 +elevator_trim_effectiveness = 1.5 +aileron_trim_effectiveness = 1 +rudder_trim_effectiveness = 1 +hi_alpha_on_roll = 0 +hi_alpha_on_yaw = 0 +p_factor_on_yaw = 0 +torque_on_roll = 0 +gyro_precession_on_roll = 0 +gyro_precession_on_yaw = 0 +engine_wash_on_roll = 0 +wingflex_scalar = 2 +wingflex_offset = 0 +stall_coef_at_min_weight = 0.71 +ground_crosswind_effect_zero_speed=10 +ground_crosswind_effect_max_speed=150 +ground_high_speed_steeringwheel_static_friction_scalar=1.5 +ground_high_speed_otherwheel_static_friction_scalar=1.2 + +[REFERENCE SPEEDS] +full_flaps_stall_speed = 115 +flaps_up_stall_speed = 149 +cruise_speed = 345 +cruise_mach = 0.85 +crossover_speed = 330 +max_mach = 0.9 +max_indicated_speed = 395 +max_flaps_extended = 170 +normal_operating_speed = 325 +airspeed_indicator_max = 562.5 +rotation_speed_min = 145 +climb_speed = 250 +cruise_alt = 41000 +takeoff_speed = 165 +spawn_cruise_altitude = 5000 +spawn_descent_altitude = 500 +best_angle_climb_speed = 0 +approach_speed = 0 +best_glide = 0 +max_gear_extended = 200 + +[INTERACTIVE POINTS] +number_of_interactive_points = 2 +interactive_point.0 = 0.4, 75.65, -8.12, -0.567, 0, 0, 0, -75, 33, 2, 33, 2, 2, 33 +interactive_point.1 = 0.4, 33.3, 6.28, -7.18, 1, 0, 0, 90, 0, 0, 0, 0, 0, 0 + +[STALL PROTECTION] +stall_protection = 1 ; Alpha Protection +off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit) +off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit) +on_limit = 14 ; Alpha above which the Alpha Protection timer starts +on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered +timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered + +;===================== FLAPS ===================== + +[FLAPS.0] +type = 1 +system_type = 1 +span-outboard = 0.25 +extending-time = 22 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.1 +drag_scalar = 1.1 +pitch_scalar = 1 +max_on_ground_position = 7 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 0, -1, 0 +flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 +flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 +flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 +flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 +flaps-position.6 = 35, 160, 0.32, 1 +flaps-position.7 = 50, 150, 0.33, 1 + +[FLAPS.1] +type = 1 +system_type = 1 +span-outboard = 0.7 +extending-time = 23 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.1 +drag_scalar = 1.1 +pitch_scalar = 1 +max_on_ground_position = 7 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 0, -1, 0 +flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 +flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 +flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 +flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 +flaps-position.6 = 35, 160, 0.32, 1 +flaps-position.7 = 50, 150, 0.33, 1 + +[FLAPS.2] +type = 2 +system_type = 1 +span-outboard = 0.2 +extending-time = 8 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.5 +drag_scalar = 0.75 +pitch_scalar = 1 +max_on_ground_position = 1 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 20, 215, 0.5, 0.5 + +[FLAPS.3] +type = 2 +system_type = 1 +span-outboard = 0.7 +extending-time = 21 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.5 +drag_scalar = 0.75 +pitch_scalar = 1 +max_on_ground_position = 1 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 20, 215, 0.5, 0.5 diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/flight_model.cfg b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/flight_model.cfg new file mode 100644 index 0000000..4132387 --- /dev/null +++ b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/flight_model.cfg @@ -0,0 +1,408 @@ +//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.0_GE 15MAY25 + +[VERSION] +//KH Bump major +major = 4 +minor = 1 + +[WEIGHT_AND_BALANCE] +max_gross_weight = 630500 +empty_weight = 283975 +reference_datum_position = 0, 0, 0 +empty_weight_CG_position = -13.3, 0, 0 +CG_forward_limit = 0.12 +CG_aft_limit = 0.34 +empty_weight_pitch_MOI = 20897456 +empty_weight_roll_MOI = 6368555 +empty_weight_yaw_MOI = 40761191 +empty_weight_coupled_MOI = 0 +activate_mach_limit_based_on_cg = 0 +activate_cg_limit_based_on_mach = 0 +max_number_of_stations = 21 +//KH START Empty default +station_load.0=0, 82.0, -2.0, 4.0, Pilot, 1 +station_load.1=0, 82.0, 2.0, 4.0, First Officer, 2 +station_load.2=0, 80.0, 3.3, 4.0, Engineer, 0 +station_load.3=0, 66.0, 0.0, 4.0, Cabin crew 1, 0 +station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 0 +station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 0 +station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 0 +station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 0 +station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 0 +station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 0 +station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 0 +station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 0 +station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 0 +station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 0 +station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 0 +station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 0 +station_load.16=0, -55.0, 0.0, 4.0, Cabin crew 2, 0 +station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 0 +station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 0 +station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0 +station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0 +//KH END + +[CONTACT_POINTS] +static_pitch = 0 +static_cg_height = 16.4 +gear_system_type = 1 +tailwheel_lock = 0 +max_number_of_points = 16 +gear_locked_on_ground = 0 +gear_locked_above_speed = -1 +max_speed_full_steering = 25 +min_available_steering_angle_pct = 0.2 +max_speed_decreasing_steering = 45 +max_speed_full_steering_castering = 20 +max_speed_decreasing_steering_castering = 35 +emergency_extension_type = 2 +hyd_need_power_to_function= 0 +min_castering_angle = 0.05236 +max_castering_angle = 1.32645 +allow_stopped_steering = 1 +point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 +point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 +point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8 +point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8 +point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1 +point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1 +point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 + +[FUEL] +LeftMain = -20.00, -38.00, -1.0, 8938, 10.00 +RightMain = -20.00, 38.00, -1.0, 8938, 10.00 +Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00 +Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00 +Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00 +LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00 +RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 +External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 +//KH From 5.00, -2.00, -3.00, 0.00, 10.00 +LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 +//KH From 5.00, 2.00, -3.00, 0.00, 10.0 +RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00 +fuel_type = 2 +number_of_tank_selectors = 3 +electric_pump = 0 +engine_driven_pump = 1 +manual_transfer_pump = 0 +manual_pump = 0 +anemometer_pump = 0 +fuel_dump_rate = 0.02 +default_fuel_tank_selector.1 = 1 +default_fuel_tank_selector.2 = 1 +default_fuel_tank_selector.3 = 1 + +[AIRPLANE_GEOMETRY] +wing_area = 3648 +wing_span = 170.5 +wing_root_chord = 34.68 +wing_camber = 1 +wing_thickness_ratio = 0.04 +wing_dihedral = 2.2 +wing_incidence = 1.5 +wing_twist = -0.5 +oswald_efficiency_factor = 0.72 +wing_winglets_flag = 1 +wing_sweep = 38 +wing_pos_apex_lon = 1 +wing_pos_apex_vert = -2.75 +htail_area = 920 +htail_span = 59.5 +htail_pos_lon = -88 +htail_pos_vert = 5.0 +htail_incidence = 0.8 +htail_sweep = 36.5 +htail_thickness_ratio = 0.02 +vtail_area = 760 +vtail_span = 28.1 +vtail_sweep = 43 +vtail_pos_lon = -79.5 +vtail_pos_vert = 28 +vtail_thickness_ratio = 0.03 +fuselage_length = 202.16 +fuselage_diameter = 19.75 +fuselage_center_pos = 10, 0, 1.0 +elevator_area = 327.0 +aileron_area = 225.0 +rudder_area = 190.0 +elevator_up_limit = 25 +elevator_down_limit = 15 +aileron_up_limit = 25 +aileron_down_limit = 15 +rudder_limit = 23 +rudder_trim_limit = 20 +elevator_trim_limit = 30 +spoiler_limit = 60 +spoilerons_available = 1 +aileron_to_spoileron_gain = 3 +min_ailerons_for_spoilerons = 10 +min_flaps_for_spoilerons = 0 +spoiler_extension_time = 2.0 +spoiler_handle_available = 1 +auto_spoiler_available = 1 +auto_spoiler_auto_retracts = 0 +auto_spoiler_min_speed = 72 +positive_g_limit_flaps_up = 5.0 +positive_g_limit_flaps_down = 4.0 +negative_g_limit_flaps_up = -4.0 +negative_g_limit_flaps_down = -3.0 +load_safety_factor = 1.5 +elevator_trim_neutral = -1 +aileron_to_rudder_scale = 0 +flap_to_aileron_scale = 0 +fly_by_wire = 0 +elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5 +aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4 +rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7 +elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00 + +[AERODYNAMICS] +lift_coef_pitch_rate = -8.09375 +lift_coef_daoa = 2.68359 +lift_coef_delta_elevator = -0.28906 +lift_coef_horizontal_incidence = 0.91357 +lift_coef_flaps = 1 +lift_coef_spoilers = 0 +drag_coef_zero_lift = 0.02539 +drag_coef_flaps = 0.1889 +drag_coef_gear = 0.0549 +drag_coef_spoilers = 0.05207 +side_force_slip_angle = -0.77392 +side_force_roll_rate = 0.15478 +side_force_yaw_rate = 0 +side_force_delta_rudder = -0.14746 +pitch_moment_horizontal_incidence = 4.24755 +pitch_moment_delta_elevator = -2.37011 +pitch_moment_delta_trim = 0 +pitch_moment_pitch_damping = -214.1455 +pitch_moment_aoa_0 = 0.11621 +pitch_moment_daoa = 8.87255 +pitch_moment_flaps = 0.0105 +pitch_moment_gear = 0.0171 +pitch_moment_spoilers = 0 +pitch_moment_delta_elevator_propwash = -2.37011 +pitch_moment_pitch_propwash = -214.1455 +roll_moment_slip_angle = 0.26855 +roll_moment_roll_damping = -3.40869 +roll_moment_yaw_rate = -0.27197 +roll_moment_spoilers = 0.07 +roll_moment_delta_aileron = -0.34521 +roll_moment_delta_rudder = 0.01660 +roll_moment_delta_aileron_trim_scalar = -0.2 +yaw_moment_slip_angle = 0.18066 +yaw_moment_roll = 0.07470 +yaw_moment_yaw_damping = -2.49023 +yaw_moment_yaw_propwash = 0 +yaw_moment_delta_aileron = -0.00683 +yaw_moment_delta_rudder = 0.07128 +yaw_moment_delta_rudder_propwash = 0.075 +yaw_moment_delta_rudder_trim_scalar = -0.2 +compute_aero_center = 0 +aero_center_lift = -13.75 +lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0 +lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0 +lift_coef_mach_table = 0:1 +lift_coef_delta_elevator_mach_table = 0:0 +lift_coef_daoa_mach_table = 0:0 +lift_coef_pitch_rate_mach_table = 0:0 +lift_coef_horizontal_incidence_mach_table = 0:0 +drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337 +side_force_slip_angle_mach_table = 0:0 +side_force_delta_rudder_mach_table = 0:0 +side_force_yaw_rate_mach_table = 0:0 +side_force_roll_rate_mach_table = 0:0 +pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2 +pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1 +pitch_moment_horizontal_incidence_aoa_table = 0:1 +pitch_moment_daoa_aoa_table = 0:1 +pitch_moment_pitch_alpha_table = 0:1 +pitch_moment_delta_elevator_mach_table = 0:0 +pitch_moment_daoa_mach_table = 0:0 +pitch_moment_pitch_rate_mach_table = 0:0 +pitch_moment_horizontal_incidence_mach_table = 0:0 +pitch_moment_aoa_0_mach_table = 0:0 +roll_moment_aoa_table = 0:0 +roll_moment_slip_angle_aoa_table = 0:1 +roll_moment_roll_rate_aoa_table = 0:1 +roll_moment_delta_aileron_aoa_table = 0:1 +roll_moment_slip_angle_mach_table = 0:0 +roll_moment_delta_rudder_mach_table = 0:0 +roll_moment_delta_aileron_mach_table = 0:0 +roll_moment_yaw_rate_mach_table = 0:0 +roll_moment_roll_rate_mach_table = 0:0 +yaw_moment_aoa_table = 0:0 +yaw_moment_slip_angle_aoa_table = 0:1 +yaw_moment_yaw_rate_aoa_table = 0:1 +yaw_moment_delta_rudder_aoa_table = 0:1 +yaw_moment_slip_angle_mach_table = 0:0 +yaw_moment_delta_rudder_mach_table = 0:0 +yaw_moment_delta_aileron_mach_table = 0:0 +yaw_moment_yaw_rate_mach_table = 0:0 +yaw_moment_roll_rate_mach_table = 0:0 +elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1 +aileron_scaling_table = -0.785:1 ;0:1 +rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1 +elevator_lift_coef=3 +rudder_lift_coef=2 +aileron_load_factor_effectiveness_table = 0:1 +lift_coef_at_drag_zero = 0.1 +lift_coef_at_drag_zero_flaps = 0.1 + +[FLIGHT_TUNING] +modern_fm_only = 1 +cruise_lift_scalar = 1 +parasite_drag_scalar = 1 +induced_drag_scalar = 1 +flap_induced_drag_scalar = 1 +elevator_effectiveness = 1 +elevator_maxangle_scalar = 1 +aileron_effectiveness = 1 +rudder_effectiveness = 1 +rudder_maxangle_scalar = 1 +pitch_stability = 5 +roll_stability = 1 +yaw_stability = 1 +pitch_gyro_stability = 1 +roll_gyro_stability = 1 +yaw_gyro_stability = 1 +empty_CG_deviation_limit=0 +elevator_trim_effectiveness = 1.5 +aileron_trim_effectiveness = 1 +rudder_trim_effectiveness = 1 +hi_alpha_on_roll = 0 +hi_alpha_on_yaw = 0 +p_factor_on_yaw = 0 +torque_on_roll = 0 +gyro_precession_on_roll = 0 +gyro_precession_on_yaw = 0 +engine_wash_on_roll = 0 +wingflex_scalar = 2 +wingflex_offset = 0 +stall_coef_at_min_weight = 0.71 +ground_crosswind_effect_zero_speed=10 +ground_crosswind_effect_max_speed=150 +ground_high_speed_steeringwheel_static_friction_scalar=1.5 +ground_high_speed_otherwheel_static_friction_scalar=1.2 + +[REFERENCE SPEEDS] +full_flaps_stall_speed = 115 +flaps_up_stall_speed = 149 +cruise_speed = 345 +cruise_mach = 0.85 +crossover_speed = 330 +max_mach = 0.9 +max_indicated_speed = 395 +max_flaps_extended = 170 +normal_operating_speed = 325 +airspeed_indicator_max = 562.5 +rotation_speed_min = 145 +climb_speed = 250 +cruise_alt = 41000 +takeoff_speed = 165 +spawn_cruise_altitude = 5000 +spawn_descent_altitude = 500 +best_angle_climb_speed = 0 +approach_speed = 0 +best_glide = 0 +max_gear_extended = 200 + +[INTERACTIVE POINTS] +number_of_interactive_points = 3 +interactive_point.0 = 0.4, 44.15, -10.05, -0.567, 0, 0, 0, -88, 35, 0, 35, 0, 2, 33 +interactive_point.1 = 0.4, 75.65, 7.92, -0.567, 0, 0, 0, 75, 33, 2, 33, 2, 2, 33 +interactive_point.2 = 0.4, 33.3, 6.28, -7.18, 1, 0, 0, 90, 0, 0, 0, 0, 0, 0 + +[STALL PROTECTION] +stall_protection = 1 ; Alpha Protection +off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit) +off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit) +on_limit = 14 ; Alpha above which the Alpha Protection timer starts +on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered +timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered + +;===================== FLAPS ===================== + +[FLAPS.0] +type = 1 +system_type = 1 +span-outboard = 0.25 +extending-time = 22 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.1 +drag_scalar = 1.1 +pitch_scalar = 1 +max_on_ground_position = 7 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 0, -1, 0 +flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 +flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 +flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 +flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 +flaps-position.6 = 35, 160, 0.32, 1 +flaps-position.7 = 50, 150, 0.33, 1 + + +[FLAPS.1] +type = 1 +system_type = 1 +span-outboard = 0.7 +extending-time = 23 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.1 +drag_scalar = 1.1 +pitch_scalar = 1 +max_on_ground_position = 7 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 0, -1, 0 +flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 +flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 +flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 +flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 +flaps-position.6 = 35, 160, 0.32, 1 +flaps-position.7 = 50, 150, 0.33, 1 + + +[FLAPS.2] +type = 2 +system_type = 1 +span-outboard = 0.2 +extending-time = 8 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.5 +drag_scalar = 0.75 +pitch_scalar = 1 +max_on_ground_position = 1 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 20, 215, 0.5, 0.5 + +[FLAPS.3] +type = 2 +system_type = 1 +span-outboard = 0.7 +extending-time = 21 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.5 +drag_scalar = 0.75 +pitch_scalar = 1 +max_on_ground_position = 1 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 20, 215, 0.5, 0.5 \ No newline at end of file diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_PW/flight_model.cfg b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_PW/flight_model.cfg new file mode 100644 index 0000000..bf5aa72 --- /dev/null +++ b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_PW/flight_model.cfg @@ -0,0 +1,406 @@ +//TFDi Designs MD-11 (PW4460) vRC1.7.0_PW 15MAY25 + +[VERSION] +//KH Bump major +major = 4 +minor = 1 + +[WEIGHT_AND_BALANCE] +max_gross_weight = 630500 +empty_weight = 283975 +reference_datum_position = 0, 0, 0 +empty_weight_CG_position = -13.3, 0, 0 +CG_forward_limit = 0.12 +CG_aft_limit = 0.34 +empty_weight_pitch_MOI = 20897456 +empty_weight_roll_MOI = 6368555 +empty_weight_yaw_MOI = 40761191 +empty_weight_coupled_MOI = 0 +activate_mach_limit_based_on_cg = 0 +activate_cg_limit_based_on_mach = 0 +max_number_of_stations = 21 +//KH START Empty default +station_load.0=0, 82.0, -2.0, 4.0, Pilot, 1 +station_load.1=0, 82.0, 2.0, 4.0, First Officer, 2 +station_load.2=0, 80.0, 3.3, 4.0, Engineer, 0 +station_load.3=0, 66.0, 0.0, 4.0, Cabin crew 1, 0 +station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 0 +station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 0 +station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 0 +station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 0 +station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 0 +station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 0 +station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 0 +station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 0 +station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 0 +station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 0 +station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 0 +station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 0 +station_load.16=0, -55.0, 0.0, 4.0, Cabin crew 2, 0 +station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 0 +station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 0 +station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0 +station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0 +//KH END + +[CONTACT_POINTS] +static_pitch = 0 +static_cg_height = 16.4 +gear_system_type = 1 +tailwheel_lock = 0 +max_number_of_points = 16 +gear_locked_on_ground = 0 +gear_locked_above_speed = -1 +max_speed_full_steering = 25 +min_available_steering_angle_pct = 0.2 +max_speed_decreasing_steering = 45 +max_speed_full_steering_castering = 20 +max_speed_decreasing_steering_castering = 35 +emergency_extension_type = 2 +hyd_need_power_to_function= 0 +min_castering_angle = 0.05236 +max_castering_angle = 1.32645 +allow_stopped_steering = 1 +point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 +point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 +point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8 +point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8 +point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1 +point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1 +point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 +point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1 +point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1 + +[FUEL] +LeftMain = -20.00, -38.00, -1.0, 8938, 10.00 +RightMain = -20.00, 38.00, -1.0, 8938, 10.00 +Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00 +Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00 +Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00 +LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00 +RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 +External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 +//KH From 5.00, -2.00, -3.00, 0.00, 10.00 +LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 +//KH From 5.00, 2.00, -3.00, 0.00, 10.0 +RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00 +fuel_type = 2 +number_of_tank_selectors = 3 +electric_pump = 0 +engine_driven_pump = 1 +manual_transfer_pump = 0 +manual_pump = 0 +anemometer_pump = 0 +fuel_dump_rate = 0.02 +default_fuel_tank_selector.1 = 1 +default_fuel_tank_selector.2 = 1 +default_fuel_tank_selector.3 = 1 + +[AIRPLANE_GEOMETRY] +wing_area = 3648 +wing_span = 170.5 +wing_root_chord = 34.68 +wing_camber = 1 +wing_thickness_ratio = 0.04 +wing_dihedral = 2.2 +wing_incidence = 1.5 +wing_twist = -0.5 +oswald_efficiency_factor = 0.72 +wing_winglets_flag = 1 +wing_sweep = 38 +wing_pos_apex_lon = 1 +wing_pos_apex_vert = -2.75 +htail_area = 920 +htail_span = 59.5 +htail_pos_lon = -88 +htail_pos_vert = 5.0 +htail_incidence = 0.8 +htail_sweep = 36.5 +htail_thickness_ratio = 0.02 +vtail_area = 760 +vtail_span = 28.1 +vtail_sweep = 43 +vtail_pos_lon = -79.5 +vtail_pos_vert = 28 +vtail_thickness_ratio = 0.03 +fuselage_length = 200.92 +fuselage_diameter = 19.75 +fuselage_center_pos = 10, 0, 1.0 +elevator_area = 327.0 +aileron_area = 225.0 +rudder_area = 190.0 +elevator_up_limit = 25 +elevator_down_limit = 15 +aileron_up_limit = 25 +aileron_down_limit = 15 +rudder_limit = 23 +rudder_trim_limit = 20 +elevator_trim_limit = 30 +spoiler_limit = 60 +spoilerons_available = 1 +aileron_to_spoileron_gain = 3 +min_ailerons_for_spoilerons = 10 +min_flaps_for_spoilerons = 0 +spoiler_extension_time = 2.0 +spoiler_handle_available = 1 +auto_spoiler_available = 1 +auto_spoiler_auto_retracts = 0 +auto_spoiler_min_speed = 72 +positive_g_limit_flaps_up = 5.0 +positive_g_limit_flaps_down = 4.0 +negative_g_limit_flaps_up = -4.0 +negative_g_limit_flaps_down = -3.0 +load_safety_factor = 1.5 +elevator_trim_neutral = -1 +aileron_to_rudder_scale = 0 +flap_to_aileron_scale = 0 +fly_by_wire = 0 +elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5 +aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4 +rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7 +elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00 + +[AERODYNAMICS] +lift_coef_pitch_rate = -8.09375 +lift_coef_daoa = 2.68359 +lift_coef_delta_elevator = -0.28906 +lift_coef_horizontal_incidence = 0.91357 +lift_coef_flaps = 1 +lift_coef_spoilers = 0 +drag_coef_zero_lift = 0.02539 +drag_coef_flaps = 0.1889 +drag_coef_gear = 0.0549 +drag_coef_spoilers = 0.05207 +side_force_slip_angle = -0.77392 +side_force_roll_rate = 0.15478 +side_force_yaw_rate = 0 +side_force_delta_rudder = -0.14746 +pitch_moment_horizontal_incidence = 4.24755 +pitch_moment_delta_elevator = -2.37011 +pitch_moment_delta_trim = 0 +pitch_moment_pitch_damping = -214.1455 +pitch_moment_aoa_0 = 0.11621 +pitch_moment_daoa = 8.87255 +pitch_moment_flaps = 0.0105 +pitch_moment_gear = 0.0171 +pitch_moment_spoilers = 0 +pitch_moment_delta_elevator_propwash = -2.37011 +pitch_moment_pitch_propwash = -214.1455 +roll_moment_slip_angle = 0.26855 +roll_moment_roll_damping = -3.40869 +roll_moment_yaw_rate = -0.27197 +roll_moment_spoilers = 0.07 +roll_moment_delta_aileron = -0.34521 +roll_moment_delta_rudder = 0.01660 +roll_moment_delta_aileron_trim_scalar = -0.2 +yaw_moment_slip_angle = 0.18066 +yaw_moment_roll = 0.07470 +yaw_moment_yaw_damping = -2.49023 +yaw_moment_yaw_propwash = 0 +yaw_moment_delta_aileron = -0.00683 +yaw_moment_delta_rudder = 0.07128 +yaw_moment_delta_rudder_propwash = 0.075 +yaw_moment_delta_rudder_trim_scalar = -0.2 +compute_aero_center = 0 +aero_center_lift = -13.75 +lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0 +lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0 +lift_coef_mach_table = 0:1 +lift_coef_delta_elevator_mach_table = 0:0 +lift_coef_daoa_mach_table = 0:0 +lift_coef_pitch_rate_mach_table = 0:0 +lift_coef_horizontal_incidence_mach_table = 0:0 +drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337 +side_force_slip_angle_mach_table = 0:0 +side_force_delta_rudder_mach_table = 0:0 +side_force_yaw_rate_mach_table = 0:0 +side_force_roll_rate_mach_table = 0:0 +pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2 +pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1 +pitch_moment_horizontal_incidence_aoa_table = 0:1 +pitch_moment_daoa_aoa_table = 0:1 +pitch_moment_pitch_alpha_table = 0:1 +pitch_moment_delta_elevator_mach_table = 0:0 +pitch_moment_daoa_mach_table = 0:0 +pitch_moment_pitch_rate_mach_table = 0:0 +pitch_moment_horizontal_incidence_mach_table = 0:0 +pitch_moment_aoa_0_mach_table = 0:0 +roll_moment_aoa_table = 0:0 +roll_moment_slip_angle_aoa_table = 0:1 +roll_moment_roll_rate_aoa_table = 0:1 +roll_moment_delta_aileron_aoa_table = 0:1 +roll_moment_slip_angle_mach_table = 0:0 +roll_moment_delta_rudder_mach_table = 0:0 +roll_moment_delta_aileron_mach_table = 0:0 +roll_moment_yaw_rate_mach_table = 0:0 +roll_moment_roll_rate_mach_table = 0:0 +yaw_moment_aoa_table = 0:0 +yaw_moment_slip_angle_aoa_table = 0:1 +yaw_moment_yaw_rate_aoa_table = 0:1 +yaw_moment_delta_rudder_aoa_table = 0:1 +yaw_moment_slip_angle_mach_table = 0:0 +yaw_moment_delta_rudder_mach_table = 0:0 +yaw_moment_delta_aileron_mach_table = 0:0 +yaw_moment_yaw_rate_mach_table = 0:0 +yaw_moment_roll_rate_mach_table = 0:0 +elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1 +aileron_scaling_table = -0.785:1 ;0:1 +rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1 +elevator_lift_coef=3 +rudder_lift_coef=2 +aileron_load_factor_effectiveness_table = 0:1 +lift_coef_at_drag_zero = 0.1 +lift_coef_at_drag_zero_flaps = 0.1 + +[FLIGHT_TUNING] +modern_fm_only = 1 +cruise_lift_scalar = 1 +parasite_drag_scalar = 1 +induced_drag_scalar = 1 +flap_induced_drag_scalar = 1 +elevator_effectiveness = 1 +elevator_maxangle_scalar = 1 +aileron_effectiveness = 1 +rudder_effectiveness = 1 +rudder_maxangle_scalar = 1 +pitch_stability = 5 +roll_stability = 1 +yaw_stability = 1 +pitch_gyro_stability = 1 +roll_gyro_stability = 1 +yaw_gyro_stability = 1 +empty_CG_deviation_limit=0 +elevator_trim_effectiveness = 1.5 +aileron_trim_effectiveness = 1 +rudder_trim_effectiveness = 1 +hi_alpha_on_roll = 0 +hi_alpha_on_yaw = 0 +p_factor_on_yaw = 0 +torque_on_roll = 0 +gyro_precession_on_roll = 0 +gyro_precession_on_yaw = 0 +engine_wash_on_roll = 0 +wingflex_scalar = 2 +wingflex_offset = 0 +stall_coef_at_min_weight = 0.71 +ground_crosswind_effect_zero_speed=10 +ground_crosswind_effect_max_speed=150 +ground_high_speed_steeringwheel_static_friction_scalar=1.5 +ground_high_speed_otherwheel_static_friction_scalar=1.2 + +[REFERENCE SPEEDS] +full_flaps_stall_speed = 115 +flaps_up_stall_speed = 149 +cruise_speed = 345 +cruise_mach = 0.85 +crossover_speed = 330 +max_mach = 0.9 +max_indicated_speed = 395 +max_flaps_extended = 170 +normal_operating_speed = 325 +airspeed_indicator_max = 562.5 +rotation_speed_min = 145 +climb_speed = 250 +cruise_alt = 41000 +takeoff_speed = 165 +spawn_cruise_altitude = 5000 +spawn_descent_altitude = 500 +best_angle_climb_speed = 0 +approach_speed = 0 +best_glide = 0 +max_gear_extended = 200 + +[INTERACTIVE POINTS] +number_of_interactive_points = 3 +interactive_point.0 = 0.4, 44.15, -10.05, -0.567, 0, 0, 0, -88, 35, 0, 35, 0, 2, 33 +interactive_point.1 = 0.4, 75.65, 7.92, -0.567, 0, 0, 0, 75, 33, 2, 33, 2, 2, 33 +interactive_point.2 = 0.4, 33.3, 6.28, -7.18, 1, 0, 0, 90, 0, 0, 0, 0, 0, 0 + +[STALL PROTECTION] +stall_protection = 1 ; Alpha Protection +off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit) +off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit) +on_limit = 14 ; Alpha above which the Alpha Protection timer starts +on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered +timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered + +;===================== FLAPS ===================== + +[FLAPS.0] +type = 1 +system_type = 1 +span-outboard = 0.25 +extending-time = 22 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.1 +drag_scalar = 1.1 +pitch_scalar = 1 +max_on_ground_position = 7 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 0, -1, 0 +flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 +flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 +flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 +flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 +flaps-position.6 = 35, 160, 0.32, 1 +flaps-position.7 = 50, 150, 0.33, 1 + +[FLAPS.1] +type = 1 +system_type = 1 +span-outboard = 0.7 +extending-time = 23 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.1 +drag_scalar = 1.1 +pitch_scalar = 1 +max_on_ground_position = 7 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 0, -1, 0 +flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 +flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 +flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 +flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 +flaps-position.6 = 35, 160, 0.32, 1 +flaps-position.7 = 50, 150, 0.33, 1 + +[FLAPS.2] +type = 2 +system_type = 1 +span-outboard = 0.2 +extending-time = 8 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.5 +drag_scalar = 0.75 +pitch_scalar = 1 +max_on_ground_position = 1 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 20, 215, 0.5, 0.5 + +[FLAPS.3] +type = 2 +system_type = 1 +span-outboard = 0.7 +extending-time = 21 +damaging-speed = 250 +blowout-speed = 300 +maneuvering_flaps = 0 +lift_scalar = 0.5 +drag_scalar = 0.75 +pitch_scalar = 1 +max_on_ground_position = 1 +flaps-position.0 = 0, -1, 0 +flaps-position.1 = 20, 215, 0.5, 0.5 \ No newline at end of file