首页> 美国政府科技报告 >Free-spinning-tunnel investigation to determine the effect on spins and recoveries of wing leading-edge chord-extensions and drooped leading-edge flaps on scale models of two sweptback-wing fighter airplanes
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Free-spinning-tunnel investigation to determine the effect on spins and recoveries of wing leading-edge chord-extensions and drooped leading-edge flaps on scale models of two sweptback-wing fighter airplanes

机译:自由旋转隧道调查,以确定两个后掠翼战斗机飞机的比例模型对机翼前缘弦杆延伸和下垂前缘襟翼的旋转和恢复的影响

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