Effects of Reynolds number on characteristics of fixed and rotary wings

被引：4

作者：

Sunada, S ^{[1
]}

Kawachi, K

机构：

[1] Osaka Prefecture Univ, Grad Sch Engn, Dept Aerosp Engn, Osaka 5998531, Japan

[2] Univ Tokyo, Dept Aeronaut & Astronaut, Tokyo 1138656, Japan

来源：

JOURNAL OF AIRCRAFT | 2004年 / 41卷 / 01期

关键词：

D O I：

10.2514/1.2695

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The effects of Reynolds number on the characteristics of an airfoil of a fixed and rotary wing was analyzed, using a circulation model. The effect of three-dimensionality on the characteristics was also discussed. The circulation model represented equations for the effect of three-dimensionality on the characteristics. Results show that a geometrical angle of attack for an optimal flight is larger with the Reynolds number.

引用

页码：189 / 192

页数：4

共 7 条

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[2]

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[3]

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[4]

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[5]

PROUTY RW, 1990, HELICOPTER PERFORMAN, pCH1

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Sunada, S ;

Yasuda, T ;

Yasuda, K ;

Kawachi, K .

JOURNAL OF AIRCRAFT, 2002, 39 (02) :331-338

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