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Search results 6

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)
Microform図書
1998<YCA-NAS 1.26:208423>
National Diet Library
  • Subject HeadingMixing 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)
Microform図書
1998<YCA-NAS 1.26:206902>
National Diet Library
  • Subject Heading...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)
Microform図書
1997<YCA-NAS 1.26:207159>
National Diet Library
  • Subject Heading...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
Digital文書・図像類
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
Other Libraries in Japan
  • Subject Heading...(exp N) method compressible boundary layer pressure distribution attachm...
  • Note (General)...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
Digital文書・図像類
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
Other Libraries in Japan
  • Subject Heading...e distribution compressible boundary layer transition measurement

Computer program manual

Computer program manual
Paper図書
by J. Schneider and J. BoccioNational Aeronautics and Space Administration1972
Other Libraries in Japan
  • Subject Heading...ary layer flow Compressible boundary layer Conservation equations Crocco...
  • Subject Heading (ID)...ary layer flow Compressible boundary layer Conservation equations Crocco...

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