trim better, appr thrust adj
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@@ -243,7 +243,8 @@ yaw_moment_roll_rate_mach_table = 0:0
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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
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aileron_scaling_table = -0.785:1 ;0:1
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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
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elevator_lift_coef=3
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//KH From 3
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elevator_lift_coef=4
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rudder_lift_coef=2
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aileron_load_factor_effectiveness_table = 0:1
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lift_coef_at_drag_zero = 0.1
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@@ -284,14 +285,15 @@ ground_crosswind_effect_zero_speed=10
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ground_crosswind_effect_max_speed=150
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ground_high_speed_steeringwheel_static_friction_scalar=1.5
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ground_high_speed_otherwheel_static_friction_scalar=1.2
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//KH New ground physics
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//KH START New ground physics
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ground_new_contact_model_gear_flex=0.0044
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ground_new_contact_model_gear_flex_damping=7
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ground_new_contact_model_rolling_stickyness=0.25
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ground_new_contact_model_rolling_stickyness=0.15
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ground_new_contact_model_up_to_speed_lateral=10000
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ground_new_contact_model_up_to_speed_lateral_steering=10000
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ground_new_contact_model_up_to_speed_longitudinal=10000
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enable_high_accuracy_integration=1
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//KH END New ground physics
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[REFERENCE SPEEDS]
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full_flaps_stall_speed = 115
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@@ -381,7 +383,7 @@ damaging-speed = 250
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blowout-speed = 300
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maneuvering_flaps = 0
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lift_scalar = 0.5
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drag_scalar = 0.75
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drag_scalar = 0.475
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pitch_scalar = 1
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max_on_ground_position = 1
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flaps-position.0 = 0, -1, 0
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@@ -396,7 +398,7 @@ damaging-speed = 250
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blowout-speed = 300
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maneuvering_flaps = 0
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lift_scalar = 0.5
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drag_scalar = 0.75
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drag_scalar = 0.475
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pitch_scalar = 1
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max_on_ground_position = 1
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flaps-position.0 = 0, -1, 0
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