update to 1.1.14
This commit is contained in:
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818277edcf
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3b003f3363
@ -1,15 +1,15 @@
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//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.1_GE 24JAN26
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//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.8.0_GE 04FEB26
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[VERSION]
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[VERSION]
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//KH Bump major
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//KH Bump major
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major = 4
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major = 4
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minor = 2
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minor = 8
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[WEIGHT_AND_BALANCE]
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[WEIGHT_AND_BALANCE]
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max_gross_weight = 630500
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max_gross_weight = 630500
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empty_weight = 283975
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empty_weight = 283975
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reference_datum_position = 0, 0, 0
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reference_datum_position = 0, 0, 0
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empty_weight_CG_position = -13.3, 0, 0
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empty_weight_CG_position = -10.0, 0, 0
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CG_forward_limit = 0.12
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CG_forward_limit = 0.12
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CG_aft_limit = 0.34
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CG_aft_limit = 0.34
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empty_weight_pitch_MOI = 20897456
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empty_weight_pitch_MOI = 20897456
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@ -59,7 +59,7 @@ max_speed_decreasing_steering_castering = 35
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emergency_extension_type = 2
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emergency_extension_type = 2
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hyd_need_power_to_function= 0
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hyd_need_power_to_function= 0
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min_castering_angle = 0.05236
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min_castering_angle = 0.05236
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max_castering_angle = 1.32645
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max_castering_angle = 3.142
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allow_stopped_steering = 1
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allow_stopped_steering = 1
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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
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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
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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
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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
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@ -88,9 +88,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
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RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
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RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
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External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
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External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
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//KH From 5.00, -2.00, -3.00, 0.00, 10.00
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//KH From 5.00, -2.00, -3.00, 0.00, 10.00
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LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00
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LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
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//KH From 5.00, 2.00, -3.00, 0.00, 10.0
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//KH From 5.00, 2.00, -3.00, 0.00, 10.0
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RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
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RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
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fuel_type = 2
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fuel_type = 2
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number_of_tank_selectors = 3
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number_of_tank_selectors = 3
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electric_pump = 0
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electric_pump = 0
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@ -175,7 +175,7 @@ lift_coef_horizontal_incidence = 0.91357
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lift_coef_flaps = 1
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lift_coef_flaps = 1
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lift_coef_spoilers = 0
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lift_coef_spoilers = 0
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drag_coef_zero_lift = 0.02539
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drag_coef_zero_lift = 0.02539
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drag_coef_flaps = 0.0789
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drag_coef_flaps = 0.1339
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drag_coef_gear = 0.0549
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drag_coef_gear = 0.0549
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drag_coef_spoilers = 0.05207
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drag_coef_spoilers = 0.05207
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side_force_slip_angle = -0.77392
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side_force_slip_angle = -0.77392
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@ -265,7 +265,7 @@ cruise_lift_scalar = 1
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parasite_drag_scalar = 1
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parasite_drag_scalar = 1
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induced_drag_scalar = 1
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induced_drag_scalar = 1
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flap_induced_drag_scalar = 1
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flap_induced_drag_scalar = 1
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elevator_effectiveness = 1
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elevator_effectiveness = 1.1
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elevator_maxangle_scalar = 1
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elevator_maxangle_scalar = 1
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aileron_effectiveness = 1
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aileron_effectiveness = 1
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rudder_effectiveness = 1
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rudder_effectiveness = 1
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@ -362,7 +362,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.7 = 50, 155, 0.54, 1
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flaps-position.7 = 50, 155, 0.43, 1
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[FLAPS.1]
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[FLAPS.1]
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@ -384,7 +384,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.7 = 50, 155, 0.54, 1
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flaps-position.7 = 50, 155, 0.43, 1
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[FLAPS.2]
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[FLAPS.2]
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@ -1,15 +1,15 @@
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//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.1_GE 24JAN26
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//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.8.0_GE 04FEB26
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[VERSION]
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[VERSION]
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//KH Bump major
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//KH Bump major
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major = 4
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major = 4
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minor = 2
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minor = 8
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[WEIGHT_AND_BALANCE]
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[WEIGHT_AND_BALANCE]
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max_gross_weight = 630500
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max_gross_weight = 630500
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empty_weight = 283975
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empty_weight = 283975
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reference_datum_position = 0, 0, 0
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reference_datum_position = 0, 0, 0
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empty_weight_CG_position = -13.3, 0, 0
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empty_weight_CG_position = -10.0, 0, 0
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CG_forward_limit = 0.12
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CG_forward_limit = 0.12
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CG_aft_limit = 0.34
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CG_aft_limit = 0.34
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empty_weight_pitch_MOI = 20897456
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empty_weight_pitch_MOI = 20897456
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@ -59,7 +59,7 @@ max_speed_decreasing_steering_castering = 35
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emergency_extension_type = 2
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emergency_extension_type = 2
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hyd_need_power_to_function= 0
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hyd_need_power_to_function= 0
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min_castering_angle = 0.05236
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min_castering_angle = 0.05236
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max_castering_angle = 1.32645
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max_castering_angle = 3.142
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allow_stopped_steering = 1
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allow_stopped_steering = 1
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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
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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
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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
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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
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@ -88,9 +88,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
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RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
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RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
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External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
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External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
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//KH From 5.00, -2.00, -3.00, 0.00, 10.00
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//KH From 5.00, -2.00, -3.00, 0.00, 10.00
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LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00
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LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
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//KH From 5.00, 2.00, -3.00, 0.00, 10.0
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//KH From 5.00, 2.00, -3.00, 0.00, 10.0
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RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
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RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
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fuel_type = 2
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fuel_type = 2
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number_of_tank_selectors = 3
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number_of_tank_selectors = 3
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electric_pump = 0
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electric_pump = 0
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@ -175,7 +175,7 @@ lift_coef_horizontal_incidence = 0.91357
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lift_coef_flaps = 1
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lift_coef_flaps = 1
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lift_coef_spoilers = 0
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lift_coef_spoilers = 0
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drag_coef_zero_lift = 0.02539
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drag_coef_zero_lift = 0.02539
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drag_coef_flaps = 0.0789
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drag_coef_flaps = 0.1339
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drag_coef_gear = 0.0549
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drag_coef_gear = 0.0549
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drag_coef_spoilers = 0.05207
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drag_coef_spoilers = 0.05207
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side_force_slip_angle = -0.77392
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side_force_slip_angle = -0.77392
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@ -265,7 +265,7 @@ cruise_lift_scalar = 1
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parasite_drag_scalar = 1
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parasite_drag_scalar = 1
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induced_drag_scalar = 1
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induced_drag_scalar = 1
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flap_induced_drag_scalar = 1
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flap_induced_drag_scalar = 1
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elevator_effectiveness = 1
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elevator_effectiveness = 1.1
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elevator_maxangle_scalar = 1
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elevator_maxangle_scalar = 1
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aileron_effectiveness = 1
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aileron_effectiveness = 1
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rudder_effectiveness = 1
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rudder_effectiveness = 1
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@ -362,7 +362,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.7 = 50, 155, 0.54, 1
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flaps-position.7 = 50, 155, 0.43, 1
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[FLAPS.1]
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[FLAPS.1]
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@ -384,7 +384,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.7 = 50, 155, 0.54, 1
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flaps-position.7 = 50, 155, 0.43, 1
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[FLAPS.2]
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[FLAPS.2]
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@ -1,4 +1,4 @@
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; TFDi Designs MD-11 (PW4462) vRC1.7.1_PW 24JAN26
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; TFDi Designs MD-11 (PW4462) vRC1.8.0_PW 04FEB26
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[MODULAR_MERGE]
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[MODULAR_MERGE]
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auto = true
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auto = true
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@ -6,13 +6,13 @@ auto = true
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[VERSION]
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[VERSION]
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//KH Bump major
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//KH Bump major
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major = 4
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major = 4
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minor = 2
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minor = 8
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[WEIGHT_AND_BALANCE]
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[WEIGHT_AND_BALANCE]
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max_gross_weight = 630500
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max_gross_weight = 630500
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empty_weight = 283975
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empty_weight = 283975
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reference_datum_position = 0, 0, 0
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reference_datum_position = 0, 0, 0
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empty_weight_CG_position = -13.3, 0, 0
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empty_weight_CG_position = -10.0, 0, 0
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CG_forward_limit = 0.12
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CG_forward_limit = 0.12
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CG_aft_limit = 0.34
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CG_aft_limit = 0.34
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empty_weight_pitch_MOI = 20897456
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empty_weight_pitch_MOI = 20897456
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@ -62,7 +62,7 @@ max_speed_decreasing_steering_castering = 35
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emergency_extension_type = 2
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emergency_extension_type = 2
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hyd_need_power_to_function= 0
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hyd_need_power_to_function= 0
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min_castering_angle = 0.05236
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min_castering_angle = 0.05236
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max_castering_angle = 1.32645
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max_castering_angle = 3.142
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allow_stopped_steering = 1
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allow_stopped_steering = 1
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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
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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
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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
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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
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@ -90,10 +90,8 @@ Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
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LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
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LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
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RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
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RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
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External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
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External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
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//KH From 5.00, -2.00, -3.00, 0.00, 10.00
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LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
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LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00
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RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
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//KH From 5.00, 2.00, -3.00, 0.00, 10.0
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RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
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fuel_type = 2
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fuel_type = 2
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number_of_tank_selectors = 3
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number_of_tank_selectors = 3
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electric_pump = 0
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electric_pump = 0
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@ -178,7 +176,7 @@ lift_coef_horizontal_incidence = 0.91357
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lift_coef_flaps = 1
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lift_coef_flaps = 1
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lift_coef_spoilers = 0
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lift_coef_spoilers = 0
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drag_coef_zero_lift = 0.02539
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drag_coef_zero_lift = 0.02539
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drag_coef_flaps = 0.0789
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drag_coef_flaps = 0.1339
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drag_coef_gear = 0.0549
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drag_coef_gear = 0.0549
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drag_coef_spoilers = 0.05207
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drag_coef_spoilers = 0.05207
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side_force_slip_angle = -0.77392
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side_force_slip_angle = -0.77392
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@ -268,7 +266,7 @@ cruise_lift_scalar = 1
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parasite_drag_scalar = 1
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parasite_drag_scalar = 1
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induced_drag_scalar = 1
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induced_drag_scalar = 1
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flap_induced_drag_scalar = 1
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flap_induced_drag_scalar = 1
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elevator_effectiveness = 1
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elevator_effectiveness = 1.1
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elevator_maxangle_scalar = 1
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elevator_maxangle_scalar = 1
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aileron_effectiveness = 1
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aileron_effectiveness = 1
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rudder_effectiveness = 1
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rudder_effectiveness = 1
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@ -365,7 +363,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.7 = 50, 155, 0.54, 1
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flaps-position.7 = 50, 155, 0.43, 1
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[FLAPS.1]
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[FLAPS.1]
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type = 1
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type = 1
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@ -386,7 +384,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.7 = 50, 155, 0.54, 1
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flaps-position.7 = 50, 155, 0.43, 1
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[FLAPS.2]
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[FLAPS.2]
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type = 2
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type = 2
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@ -1,4 +1,4 @@
|
|||||||
; TFDi Designs MD-11 (PW4462) vRC1.7.1_PW 24JAN26
|
; TFDi Designs MD-11 (PW4462) vRC1.8.0_PW 04FEB26
|
||||||
|
|
||||||
[MODULAR_MERGE]
|
[MODULAR_MERGE]
|
||||||
auto = true
|
auto = true
|
||||||
@ -6,13 +6,13 @@ auto = true
|
|||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 2
|
minor = 8
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
empty_weight = 283975
|
empty_weight = 283975
|
||||||
reference_datum_position = 0, 0, 0
|
reference_datum_position = 0, 0, 0
|
||||||
empty_weight_CG_position = -13.3, 0, 0
|
empty_weight_CG_position = -10.0, 0, 0
|
||||||
CG_forward_limit = 0.12
|
CG_forward_limit = 0.12
|
||||||
CG_aft_limit = 0.34
|
CG_aft_limit = 0.34
|
||||||
empty_weight_pitch_MOI = 20897456
|
empty_weight_pitch_MOI = 20897456
|
||||||
@ -62,7 +62,7 @@ max_speed_decreasing_steering_castering = 35
|
|||||||
emergency_extension_type = 2
|
emergency_extension_type = 2
|
||||||
hyd_need_power_to_function= 0
|
hyd_need_power_to_function= 0
|
||||||
min_castering_angle = 0.05236
|
min_castering_angle = 0.05236
|
||||||
max_castering_angle = 1.32645
|
max_castering_angle = 3.142
|
||||||
allow_stopped_steering = 1
|
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.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.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
|
||||||
@ -91,9 +91,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
|||||||
RightTip = -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
|
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||||
//KH From 5.00, -2.00, -3.00, 0.00, 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
|
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||||
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
|
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||||
fuel_type = 2
|
fuel_type = 2
|
||||||
number_of_tank_selectors = 3
|
number_of_tank_selectors = 3
|
||||||
electric_pump = 0
|
electric_pump = 0
|
||||||
@ -178,7 +178,7 @@ lift_coef_horizontal_incidence = 0.91357
|
|||||||
lift_coef_flaps = 1
|
lift_coef_flaps = 1
|
||||||
lift_coef_spoilers = 0
|
lift_coef_spoilers = 0
|
||||||
drag_coef_zero_lift = 0.02539
|
drag_coef_zero_lift = 0.02539
|
||||||
drag_coef_flaps = 0.0789
|
drag_coef_flaps = 0.1339
|
||||||
drag_coef_gear = 0.0549
|
drag_coef_gear = 0.0549
|
||||||
drag_coef_spoilers = 0.05207
|
drag_coef_spoilers = 0.05207
|
||||||
side_force_slip_angle = -0.77392
|
side_force_slip_angle = -0.77392
|
||||||
@ -268,7 +268,7 @@ cruise_lift_scalar = 1
|
|||||||
parasite_drag_scalar = 1
|
parasite_drag_scalar = 1
|
||||||
induced_drag_scalar = 1
|
induced_drag_scalar = 1
|
||||||
flap_induced_drag_scalar = 1
|
flap_induced_drag_scalar = 1
|
||||||
elevator_effectiveness = 1
|
elevator_effectiveness = 1.1
|
||||||
elevator_maxangle_scalar = 1
|
elevator_maxangle_scalar = 1
|
||||||
aileron_effectiveness = 1
|
aileron_effectiveness = 1
|
||||||
rudder_effectiveness = 1
|
rudder_effectiveness = 1
|
||||||
@ -365,7 +365,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
|||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 155, 0.54, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.1]
|
[FLAPS.1]
|
||||||
type = 1
|
type = 1
|
||||||
@ -386,7 +386,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
|||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 155, 0.54, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.2]
|
[FLAPS.2]
|
||||||
type = 2
|
type = 2
|
||||||
|
|||||||
@ -1,4 +1,4 @@
|
|||||||
; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.1_GE_F 24JAN26
|
; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.8.0_GE_F 04FEB26
|
||||||
|
|
||||||
[MODULAR_MERGE]
|
[MODULAR_MERGE]
|
||||||
auto = true
|
auto = true
|
||||||
@ -6,13 +6,13 @@ auto = true
|
|||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 2
|
minor = 8
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
empty_weight = 248567
|
empty_weight = 248567
|
||||||
reference_datum_position = 0, 0, 0
|
reference_datum_position = 0, 0, 0
|
||||||
empty_weight_CG_position = -13.3, 0, 0
|
empty_weight_CG_position = -10.0, 0, 0
|
||||||
CG_forward_limit = 0.12
|
CG_forward_limit = 0.12
|
||||||
CG_aft_limit = 0.34
|
CG_aft_limit = 0.34
|
||||||
empty_weight_pitch_MOI = 20897456
|
empty_weight_pitch_MOI = 20897456
|
||||||
@ -56,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
|
|||||||
emergency_extension_type = 2
|
emergency_extension_type = 2
|
||||||
hyd_need_power_to_function= 0
|
hyd_need_power_to_function= 0
|
||||||
min_castering_angle = 0.05236
|
min_castering_angle = 0.05236
|
||||||
max_castering_angle = 1.32645
|
max_castering_angle = 3.142
|
||||||
allow_stopped_steering = 1
|
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.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.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
|
||||||
@ -85,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
|||||||
RightTip = -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
|
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||||
//KH From 5.00, -2.00, -3.00, 0.00, 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
|
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||||
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
|
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||||
fuel_type = 2
|
fuel_type = 2
|
||||||
number_of_tank_selectors = 3
|
number_of_tank_selectors = 3
|
||||||
electric_pump = 0
|
electric_pump = 0
|
||||||
@ -172,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
|
|||||||
lift_coef_flaps = 1
|
lift_coef_flaps = 1
|
||||||
lift_coef_spoilers = 0
|
lift_coef_spoilers = 0
|
||||||
drag_coef_zero_lift = 0.02539
|
drag_coef_zero_lift = 0.02539
|
||||||
drag_coef_flaps = 0.0789
|
drag_coef_flaps = 0.1339
|
||||||
drag_coef_gear = 0.0549
|
drag_coef_gear = 0.0549
|
||||||
drag_coef_spoilers = 0.05207
|
drag_coef_spoilers = 0.05207
|
||||||
side_force_slip_angle = -0.77392
|
side_force_slip_angle = -0.77392
|
||||||
@ -262,7 +262,7 @@ cruise_lift_scalar = 1
|
|||||||
parasite_drag_scalar = 1
|
parasite_drag_scalar = 1
|
||||||
induced_drag_scalar = 1
|
induced_drag_scalar = 1
|
||||||
flap_induced_drag_scalar = 1
|
flap_induced_drag_scalar = 1
|
||||||
elevator_effectiveness = 1
|
elevator_effectiveness = 1.1
|
||||||
elevator_maxangle_scalar = 1
|
elevator_maxangle_scalar = 1
|
||||||
aileron_effectiveness = 1
|
aileron_effectiveness = 1
|
||||||
rudder_effectiveness = 1
|
rudder_effectiveness = 1
|
||||||
@ -354,7 +354,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
|||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 155, 0.54, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
|
|
||||||
[FLAPS.1]
|
[FLAPS.1]
|
||||||
@ -376,7 +376,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
|||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 155, 0.54, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.2]
|
[FLAPS.2]
|
||||||
type = 2
|
type = 2
|
||||||
|
|||||||
@ -1,4 +1,4 @@
|
|||||||
; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.1_GE_F 24JAN26
|
; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.8.0_GE_F 04FEB26
|
||||||
|
|
||||||
[MODULAR_MERGE]
|
[MODULAR_MERGE]
|
||||||
auto = true
|
auto = true
|
||||||
@ -6,13 +6,13 @@ auto = true
|
|||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 2
|
minor = 8
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
empty_weight = 248567
|
empty_weight = 248567
|
||||||
reference_datum_position = 0, 0, 0
|
reference_datum_position = 0, 0, 0
|
||||||
empty_weight_CG_position = -13.3, 0, 0
|
empty_weight_CG_position = -10.0, 0, 0
|
||||||
CG_forward_limit = 0.12
|
CG_forward_limit = 0.12
|
||||||
CG_aft_limit = 0.34
|
CG_aft_limit = 0.34
|
||||||
empty_weight_pitch_MOI = 20897456
|
empty_weight_pitch_MOI = 20897456
|
||||||
@ -56,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
|
|||||||
emergency_extension_type = 2
|
emergency_extension_type = 2
|
||||||
hyd_need_power_to_function= 0
|
hyd_need_power_to_function= 0
|
||||||
min_castering_angle = 0.05236
|
min_castering_angle = 0.05236
|
||||||
max_castering_angle = 1.32645
|
max_castering_angle = 3.142
|
||||||
allow_stopped_steering = 1
|
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.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.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
|
||||||
@ -85,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
|||||||
RightTip = -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
|
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||||
//KH From 5.00, -2.00, -3.00, 0.00, 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
|
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||||
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
|
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||||
fuel_type = 2
|
fuel_type = 2
|
||||||
number_of_tank_selectors = 3
|
number_of_tank_selectors = 3
|
||||||
electric_pump = 0
|
electric_pump = 0
|
||||||
@ -172,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
|
|||||||
lift_coef_flaps = 1
|
lift_coef_flaps = 1
|
||||||
lift_coef_spoilers = 0
|
lift_coef_spoilers = 0
|
||||||
drag_coef_zero_lift = 0.02539
|
drag_coef_zero_lift = 0.02539
|
||||||
drag_coef_flaps = 0.0789
|
drag_coef_flaps = 0.1339
|
||||||
drag_coef_gear = 0.0549
|
drag_coef_gear = 0.0549
|
||||||
drag_coef_spoilers = 0.05207
|
drag_coef_spoilers = 0.05207
|
||||||
side_force_slip_angle = -0.77392
|
side_force_slip_angle = -0.77392
|
||||||
@ -262,7 +262,7 @@ cruise_lift_scalar = 1
|
|||||||
parasite_drag_scalar = 1
|
parasite_drag_scalar = 1
|
||||||
induced_drag_scalar = 1
|
induced_drag_scalar = 1
|
||||||
flap_induced_drag_scalar = 1
|
flap_induced_drag_scalar = 1
|
||||||
elevator_effectiveness = 1
|
elevator_effectiveness = 1.1
|
||||||
elevator_maxangle_scalar = 1
|
elevator_maxangle_scalar = 1
|
||||||
aileron_effectiveness = 1
|
aileron_effectiveness = 1
|
||||||
rudder_effectiveness = 1
|
rudder_effectiveness = 1
|
||||||
@ -354,7 +354,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
|||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 155, 0.54, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
|
|
||||||
[FLAPS.1]
|
[FLAPS.1]
|
||||||
@ -376,7 +376,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
|||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 155, 0.54, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.2]
|
[FLAPS.2]
|
||||||
type = 2
|
type = 2
|
||||||
|
|||||||
@ -1,4 +1,4 @@
|
|||||||
; TFDi Designs MD-11F (P&W PW4662) vRC1.7.1_PW_F 24JAN26
|
; TFDi Designs MD-11F (P&W PW4662) vRC1.8.0_PW_F 04FEB26
|
||||||
|
|
||||||
[MODULAR_MERGE]
|
[MODULAR_MERGE]
|
||||||
auto = true
|
auto = true
|
||||||
@ -6,13 +6,13 @@ auto = true
|
|||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 2
|
minor = 8
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
empty_weight = 248567
|
empty_weight = 248567
|
||||||
reference_datum_position = 0, 0, 0
|
reference_datum_position = 0, 0, 0
|
||||||
empty_weight_CG_position = -13.3, 0, 0
|
empty_weight_CG_position = -10.0, 0, 0
|
||||||
CG_forward_limit = 0.12
|
CG_forward_limit = 0.12
|
||||||
CG_aft_limit = 0.34
|
CG_aft_limit = 0.34
|
||||||
empty_weight_pitch_MOI = 20897456
|
empty_weight_pitch_MOI = 20897456
|
||||||
@ -56,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
|
|||||||
emergency_extension_type = 2
|
emergency_extension_type = 2
|
||||||
hyd_need_power_to_function= 0
|
hyd_need_power_to_function= 0
|
||||||
min_castering_angle = 0.05236
|
min_castering_angle = 0.05236
|
||||||
max_castering_angle = 1.32645
|
max_castering_angle = 3.142
|
||||||
allow_stopped_steering = 1
|
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.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.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
|
||||||
@ -85,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
|||||||
RightTip = -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
|
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||||
//KH From 5.00, -2.00, -3.00, 0.00, 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
|
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||||
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
|
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||||
fuel_type = 2
|
fuel_type = 2
|
||||||
number_of_tank_selectors = 3
|
number_of_tank_selectors = 3
|
||||||
electric_pump = 0
|
electric_pump = 0
|
||||||
@ -172,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
|
|||||||
lift_coef_flaps = 1
|
lift_coef_flaps = 1
|
||||||
lift_coef_spoilers = 0
|
lift_coef_spoilers = 0
|
||||||
drag_coef_zero_lift = 0.02539
|
drag_coef_zero_lift = 0.02539
|
||||||
drag_coef_flaps = 0.0789
|
drag_coef_flaps = 0.1339
|
||||||
drag_coef_gear = 0.0549
|
drag_coef_gear = 0.0549
|
||||||
drag_coef_spoilers = 0.05207
|
drag_coef_spoilers = 0.05207
|
||||||
side_force_slip_angle = -0.77392
|
side_force_slip_angle = -0.77392
|
||||||
@ -262,7 +262,7 @@ cruise_lift_scalar = 1
|
|||||||
parasite_drag_scalar = 1
|
parasite_drag_scalar = 1
|
||||||
induced_drag_scalar = 1
|
induced_drag_scalar = 1
|
||||||
flap_induced_drag_scalar = 1
|
flap_induced_drag_scalar = 1
|
||||||
elevator_effectiveness = 1
|
elevator_effectiveness = 1.1
|
||||||
elevator_maxangle_scalar = 1
|
elevator_maxangle_scalar = 1
|
||||||
aileron_effectiveness = 1
|
aileron_effectiveness = 1
|
||||||
rudder_effectiveness = 1
|
rudder_effectiveness = 1
|
||||||
@ -354,7 +354,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
|||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 155, 0.54, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.1]
|
[FLAPS.1]
|
||||||
type = 1
|
type = 1
|
||||||
@ -375,7 +375,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
|||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 155, 0.54, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.2]
|
[FLAPS.2]
|
||||||
type = 2
|
type = 2
|
||||||
|
|||||||
@ -1,4 +1,4 @@
|
|||||||
; TFDi Designs MD-11F (P&W PW4662) vRC1.7.1_PW_F 24JAN26
|
; TFDi Designs MD-11F (P&W PW4662) vRC1.8.0_PW_F 04FEB26
|
||||||
|
|
||||||
[MODULAR_MERGE]
|
[MODULAR_MERGE]
|
||||||
auto = true
|
auto = true
|
||||||
@ -6,13 +6,13 @@ auto = true
|
|||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 2
|
minor = 8
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
empty_weight = 248567
|
empty_weight = 248567
|
||||||
reference_datum_position = 0, 0, 0
|
reference_datum_position = 0, 0, 0
|
||||||
empty_weight_CG_position = -13.3, 0, 0
|
empty_weight_CG_position = -10.0, 0, 0
|
||||||
CG_forward_limit = 0.12
|
CG_forward_limit = 0.12
|
||||||
CG_aft_limit = 0.34
|
CG_aft_limit = 0.34
|
||||||
empty_weight_pitch_MOI = 20897456
|
empty_weight_pitch_MOI = 20897456
|
||||||
@ -56,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
|
|||||||
emergency_extension_type = 2
|
emergency_extension_type = 2
|
||||||
hyd_need_power_to_function= 0
|
hyd_need_power_to_function= 0
|
||||||
min_castering_angle = 0.05236
|
min_castering_angle = 0.05236
|
||||||
max_castering_angle = 1.32645
|
max_castering_angle = 3.142
|
||||||
allow_stopped_steering = 1
|
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.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.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
|
||||||
@ -85,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
|||||||
RightTip = -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
|
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||||
//KH From 5.00, -2.00, -3.00, 0.00, 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
|
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||||
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
|
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||||
fuel_type = 2
|
fuel_type = 2
|
||||||
number_of_tank_selectors = 3
|
number_of_tank_selectors = 3
|
||||||
electric_pump = 0
|
electric_pump = 0
|
||||||
@ -172,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
|
|||||||
lift_coef_flaps = 1
|
lift_coef_flaps = 1
|
||||||
lift_coef_spoilers = 0
|
lift_coef_spoilers = 0
|
||||||
drag_coef_zero_lift = 0.02539
|
drag_coef_zero_lift = 0.02539
|
||||||
drag_coef_flaps = 0.0789
|
drag_coef_flaps = 0.1339
|
||||||
drag_coef_gear = 0.0549
|
drag_coef_gear = 0.0549
|
||||||
drag_coef_spoilers = 0.05207
|
drag_coef_spoilers = 0.05207
|
||||||
side_force_slip_angle = -0.77392
|
side_force_slip_angle = -0.77392
|
||||||
@ -262,7 +262,7 @@ cruise_lift_scalar = 1
|
|||||||
parasite_drag_scalar = 1
|
parasite_drag_scalar = 1
|
||||||
induced_drag_scalar = 1
|
induced_drag_scalar = 1
|
||||||
flap_induced_drag_scalar = 1
|
flap_induced_drag_scalar = 1
|
||||||
elevator_effectiveness = 1
|
elevator_effectiveness = 1.1
|
||||||
elevator_maxangle_scalar = 1
|
elevator_maxangle_scalar = 1
|
||||||
aileron_effectiveness = 1
|
aileron_effectiveness = 1
|
||||||
rudder_effectiveness = 1
|
rudder_effectiveness = 1
|
||||||
@ -354,7 +354,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
|||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 155, 0.54, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.1]
|
[FLAPS.1]
|
||||||
type = 1
|
type = 1
|
||||||
@ -375,7 +375,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
|||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 155, 0.54, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.2]
|
[FLAPS.2]
|
||||||
type = 2
|
type = 2
|
||||||
|
|||||||
@ -32,7 +32,7 @@
|
|||||||
/******************************** Constants ********************************/
|
/******************************** Constants ********************************/
|
||||||
// Module identification
|
// Module identification
|
||||||
#define MODULE_NAME "[KHOFMANN TFDi MD-11 Load Manager] "
|
#define MODULE_NAME "[KHOFMANN TFDi MD-11 Load Manager] "
|
||||||
#define VERSION_STRING "1.14"
|
#define VERSION_STRING "1.15"
|
||||||
// COMM BUS
|
// COMM BUS
|
||||||
#define COMM_BUS_LIVE_DATA_EVENT "khofmann_tfdi_md-11_load_manager_live_data"
|
#define COMM_BUS_LIVE_DATA_EVENT "khofmann_tfdi_md-11_load_manager_live_data"
|
||||||
#define COMM_BUS_UPDATE_TARGET_EVENT "khofmann_tfdi_md-11_load_manager_update_target"
|
#define COMM_BUS_UPDATE_TARGET_EVENT "khofmann_tfdi_md-11_load_manager_update_target"
|
||||||
|
|||||||
@ -26,7 +26,7 @@
|
|||||||
#define MAX_FUEL(IS_IMPERIAL) ((IS_IMPERIAL) ? (256207) : (116213))
|
#define MAX_FUEL(IS_IMPERIAL) ((IS_IMPERIAL) ? (256207) : (116213))
|
||||||
#define MAX_FUEL_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (282619) : (128193))
|
#define MAX_FUEL_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (282619) : (128193))
|
||||||
// Arms Shared
|
// Arms Shared
|
||||||
#define ARM_EMPTY -159.6
|
#define ARM_EMPTY -120.0
|
||||||
#define ARM_PILOT 984.0
|
#define ARM_PILOT 984.0
|
||||||
#define ARM_FIRST_OFFICER 984.0
|
#define ARM_FIRST_OFFICER 984.0
|
||||||
#define ARM_ENGINEER 960.0
|
#define ARM_ENGINEER 960.0
|
||||||
|
|||||||
Loading…
x
Reference in New Issue
Block a user