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1.27m、マッハ10極超音速風洞の気流検定結果について

1.27m、マッハ10極超音速風洞の気流検定結果について
Digital文書・図像類
平林, 則明, 小山, 忠勇, 津田, 尚一, 関根, 英夫, 永井, 伸治, 榊原, 盛三, Hirabayashi, Noriaki, Koyama, Tadao, Tsuda, Shoichi, Sekine, Hideo, Nagai, Shinji, Sakakibara, Seizo航空宇宙技術研究所2000-07航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory45p.113-120
Other Libraries in Japan
  • Subject Heading...oothing method trial and error method pressure wave Mach number jet...
  • Note (General)...cs) and by the trial and error method using the smoo......main flow, the trial and error method was used to determine the cut...

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