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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...極超音速風洞実験圧縮性流体 bluntness effect yawed cylinder model hemisphe...
Note (General)... expected. The bluntness effect at an angle of attack of 40 d...
Alternative TitleExperiments to ascertain the bluntness effect on attachment line transition...

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