Modified Aileron Tips Improve Lateral Stability

Joachim L. Grenestedt

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Modified Aileron Tips Improve Lateral Stability

机译：改进的副翼尖提高了横向稳定性

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摘要

The modified aileron tips improved the stick-free lateral stability of the particular aircraft, although not sufficiently to make the aircraft fulfill Federal Aviation Regulation Part 23 requirements [2]. It may be speculated that aileron tips with anhedral could possibly cure the stick-free lateral stability deficiency, although this was not investigated. Needless to say, aileron tips with anhedral could affect the aircraft in undesirable or even dangerous ways.

机译：尽管不足以使飞机满足联邦航空法规第23部分的要求[2]，但改进的副翼尖改善了特定飞机的不粘横向稳定性。可以推测，带有副翼的副翼尖端可能可以解决无杆侧向稳定性不足的问题，尽管尚未对此进行研究。不用说，带有副翼的副翼尖端可能会以不良或什至危险的方式影响飞机。

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来源
《Journal of Aircraft》 |2008年第6期|2176-2177|共2页
作者
Joachim L. Grenestedt;
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作者单位

Lehigh University, Bethlehem, Pennsylvania 18015;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
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Modified Aileron Tips Improve Lateral Stability

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