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Vertical tail buffeting of fighter aircraft

机译:战斗机的垂直尾巴抖振

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摘要

Vertical tail buffeting at high angles of attack is a phenomenon associated with the impact of vortical flows generated by the aircraft on the fins. This poses a serious problem for both single-and twin-tail fighter aircraft from the point of view of combat maneuverability and structural integrity. The research activities to understand the flow physics with an aim to alleviate buffet loads were quite intense during the period from the late 1970s to the early 1990s.
机译:在高攻角处的垂直尾巴抖振是一种与飞机产生的涡流对鳍片的冲击有关的现象。从作战机动性和结构完整性的角度来看,这对单尾翼和双尾翼战斗机都构成了严重的问题。从1970年代末到1990年代初,旨在减轻流动载荷的研究活动非常活跃。

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