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極超音速流中斜円柱付着線上境界層遷移への鈍頭度の効果に関する実験

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藤井, 啓介, 小山, 忠勇, 津田, 尚一, 平林, 則明, 関根, 英夫, 永井, 伸治, 榊原, 盛三, 穂積, 弘一, Fujii, Keisuke, Koyama, Tadao, Tsuda, Shoichi, Hirabayashi, Noriaki, Sekine, Hideo, Nagai, Shinji, Sakakibara, Seizo, Hozumi, Koichi航空宇宙技術研究所2000-10航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory753p.1-17

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Subject Heading...ere nose model attachment line transition hypersonic flow hypersonic wi...
Note (General)...Experiments on attachment line transition of two yawed cylinder models ...
Alternative Title...ness effect on attachment line transition of a yawed cylinder in hypers...

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