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An application of numerical optimization to a wing twist of SST wing-nacelle configuration
An application of numerical optimization to a wing twist of SST wing-nacelle configuration
Digital
文書・図像類
山崎, 哲夫, 斎藤, 充, Yamazaki, Tetsuo, Saito, Mitsuru
航空宇宙技術研究所
2000-12
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory
49T
p.131-132
Other Libraries in Japan
Subject Heading
SST 超音速輸送機 翼・ナセル形状
翼捩れ
CFD 計算流体力学 数値最適化法 表面翼圧力分布 翼・ナ...
Note (General)
...のある航空機を解析した。始めの
翼捩れ
は0度である。表面翼圧力分布を始めの形状と最適化したとき比較...
Alternative Title
SSTの翼・ナセル形状の
翼捩れ
に対する数値最適化の適用
Reached to the end of result.
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