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Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings
Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings
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机译:使用超音速层流机翼的后缘控制面进行升力和扭转控制
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摘要
An aircraft comprising a fuselage, thin supersonic wings on the fuselage, there being trailing edge flaps carried by the wings, the flaps configured to provide flap deflection to simultaneously control wing twist and to reduce drag, when the aircraft is operated at subsonic flight conditions.
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