SLENDER WING ROCK REVISITED

被引：15

作者：

ERICSSON, LE

机构：

[1] Lockheed Missiles and Space Company, Inc., Sunny vale, CA

来源：

JOURNAL OF AIRCRAFT | 1993年 / 30卷 / 03期

关键词：

D O I：

10.2514/3.46341

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Analysis of experimental results for slender delta wings reveals that asymmetric liftoff of the leading-edge vortices on slender delta wings does not start the wing rock, although it is responsible for the large limit cycle amplitude observed in experiments. As a consequence, the interaction of slender wing rock does not depend upon the interaction between the two leading-edge vortices, but can be generated by one wing half by itself, making slender wing rock more likely to occur on high agility aircraft than previously thought.

引用

页码：352 / 356

页数：5

共 14 条

[1]

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[2]

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[3]

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[4]

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[5]

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[6]

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[7]

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[8]

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[9]

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[10]

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