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衝撃波干渉を伴う超音速フィルム冷却の実験　第2報

衝撃波干渉を伴う超音速フィルム冷却の実験　第2報
Digital文書・図像類
小野, 文衛, 苅田, 丈士, 斎藤, 俊仁, 若松, 義男, Ono, Fumiei, Kanda, Takeshi, Saito, Toshihito, Wakamatsu, Yoshio航空宇宙技術研究所1997-12航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1340p.1-12
Other Libraries in Japan
  • Subject Heading...nic flow field supersonic film cooling shock wave interaction slot i...
  • Note (General)...生が予測できることを示した。 Supersonic film cooling was tested in a Mach 2.35 win...
  • Alternative TitleExperimental studies of supersonic film cooling with shock wave interaction, ...

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