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Progress in Favré-Reynolds stress closures for compressible flows [microform] / V. Adumitroaie, J.R. Ristorcelli, D.B. Taulbee (ICASE report ; no. 98-21) ([NASA contractor report] ; 2078423)

Progress in Favré-Reynolds stress closures for compressible flows [microform] / V. Adumitroaie, J.R. Ristorcelli, D.B. Taulbee (ICASE report ; no. 98-21) ([NASA contractor report] ; 2078423)
マイクロ図書
1998<YCA-NAS 1.26:208423>
国立国会図書館
  • 件名Mixing layers (Fluids) Reynolds stress Compressible flow Compressible boundary layer Mach number

Some results relevant to statistical closures for compressible turbulence [microform] / J.R. Ristorcelli (ICASE report ; no. 98-1) ([NASA contractor report] ; NASA/CR-1998-206902)

Some results relevant to statistical closures for compressible turbulence [microform] / J.R. Ristorcelli (ICASE report ; no. 98-1) ([NASA contractor report] ; NASA/CR-1998-206902)
マイクロ図書
1998<YCA-NAS 1.26:206902>
国立国会図書館
  • 件名...cal simulation Compressible boundary layer Mach number Stretching

Noise from supersonic coaxial jets. Part 1, Mean flow predictions [microform] / M.D. Dahl and P.J. Morris ([NASA contractor report] ; NASA/CR-97-207159)

Noise from supersonic coaxial jets. Part 1, Mean flow predictions [microform] / M.D. Dahl and P.J. Morris ([NASA contractor report] ; NASA/CR-97-207159)
マイクロ図書
1997<YCA-NAS 1.26:207159>
国立国会図書館
  • 件名...ayer equations Compressible boundary layer Turbulence models Reynolds av...

Boundary layer transition analysis of the scaled supersonic experimental airplane

Boundary layer transition analysis of the scaled supersonic experimental airplane
デジタル規格・テクニカルリポート類
吉田, 憲司, 岩宮, 敏幸, 上田, 良稲, 石川, 敬掲, Yoshida, Kenji, Iwamiya, Toshiyuki, Ueda, Yoshine, Ishikawa, Hiroaki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.85-90
全国の図書館
  • 件名...(exp N) method compressible boundary layer pressure distribution attachm...
  • 一般注記...an that by the compressible boundary layer code. (4) No transition due t...

Transition measurement on the natural laminar flow wing of the non-powered experimental airplane for supersonic transport

Transition measurement on the natural laminar flow wing of the non-powered experimental airplane for supersonic transport
デジタル規格・テクニカルリポート類
杉浦, 裕樹, 吉田, 憲司, 徳川, 直子, 高木, 正平, 西沢, 啓, Sugiura, Hiroki, Yoshida, Kenji, Tokugawa, Naoko, Takagi, Shohei, Nishizawa, Akira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 Laboratory48Tp.51-54
全国の図書館
  • 件名...e distribution compressible boundary layer transition measurement

Computer program manual

Computer program manual
紙図書
by J. Schneider and J. BoccioNational Aeronautics and Space Administration1972
全国の図書館
  • 件名...ary layer flow Compressible boundary layer Conservation equations Crocco...

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