plane: slightly reduced wing lift
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@ -63,7 +63,7 @@ local nor_frict_coeff = 0.8
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local tail_frict_coeff = 0.4
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local tail_area = 5.0
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local turn_coeff = 500.0
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local wing_lift = 0.5
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local wing_lift = 0.3
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local accel_speed = 400.0
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local decel_speed = 400.0
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local max_motorPower = ENGINE_MAX
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