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Numerical flutter simulation: Application to structural design of main surface of SST experimental aircraft
Numerical flutter simulation: Application to structural design of main surface of SST experimental aircraft
Digital
文書・図像類
中道, 二郎, Kheirandish, Hamid Reza, Nakamichi, Jiro
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.179-182
Other Libraries in Japan
Subject Heading
...速度 SST実験機 構造設計
遷音速領域
空力弾性応答 非定常オイラー方程式 線形理論 エルロンフラ...
Note (General)
...の超音速輸送(SST)実験機の
遷音速領域
近傍における空力弾性応答の数値...
...についてもまた線形理論を用いて
遷音速領域
を除いて決定した。マッハ数0.6〜1.0の領域に対して、フラ...
Reached to the end of result.
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