A REVIEW ON INVESTIGATIONS OF WING ROCK PROBLEMS UNDER HIGH ANGLES OF ATTACK
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摘要: 机翼摇滚是现代战斗机、导弹设计中普遍遇到的横向不稳定现象之一,属于典型的大攻角动态特性问题. 20多年来,机翼摇滚问题在国内外航空工业界、学术界都引起了极大的重视和兴趣,并在实(试)验、计算方面发表了许多文章,对机翼摇滚问题的认识也取得了较大的进展.本文对自1981年Nguyen、Yip及Chambers最早研究机翼摇滚现象以来,在该问题研究方面的近100多篇有代表性的论文进行了综述,内容涉及实(试)验研究、计算研究的各个方面,并对今后的发展趋势提出了自己的看法.Abstract: Wing rock, as a typical problem ofdynamic characteristics under high angle of attack, is one ofthe phenomena of lateral-directional instability that are often encounteredin the design of modern fighters and missiles. In the recent twenty years,wing rock problems have been attracted much attention inaviation-industry and research institutions. Many papers on experiment and calculation method have been published on this problem and great progress has been made. In this paper, the researches of wing rock in experiment and calculation are summarized by referencing more than 100 articles on this problem and the furtherresearch directions on wing rock are suggested.
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