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J-GLOBAL ID:201002064593789161   Reference number:76A0295488

A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets.

翼端小翼の設計方針と高亜音速におけるその風試結果
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Issue: D-8260  Page: 32P  Publication year: 1976 
JST Material Number: B0433A  CODEN: NASCA  Document type: Reports
Article type: 原著論文  Country of issue: United States (USA)  Language: ENGLISH (EN)
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