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Aerodynamic design of natural laminar flow supersonic aircraft wings

Aerodynamic design of natural laminar flow supersonic aircraft wings
Digital文書・図像類
生越, 博景, Ogoshi, Hirokage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 Laboratory49Tp.203-209
Other Libraries in Japan
  • Subject Heading...ign supersonic aircraft wing natural laminar flow boundary...
  • Note (General)...for supersonic aircraft wings was conducted by using 3-D C...

e(exp N)法に基づく境界層の遷移予測とその検証

e(exp N)法に基づく境界層の遷移予測とその検証
Digital文書・図像類
跡部, 隆, 山本, 稀義, Atobe, Takashi, Yamamoto, Kiyoshi航空宇宙技術研究所1999-11航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1390p.1-12
Other Libraries in Japan
  • Subject Heading...ental aircraft aircraft wing computation accuracy yawed ci...

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