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Neural network prediction of new aircraft design coefficients [microform] / Magnus Nørgaard, Charles C. Jorgensen, James C. Ross (NASA technical memorandum ; 112197)

Neural network prediction of new aircraft design coefficients [microform] / Magnus Nørgaard, Charles C. Jorgensen, James C. Ross (NASA technical memorandum ; 112197)
Microform図書
1997<YCA-NAS 1.15:112197>
National Diet Library
  • Subject Heading...nel tests Lift Lift drag ratio Aerodynamic drag Angle of att...

Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle [microform] / Roger A. Lepsch, Jr. and George M. Ware, Ian O. MacConochie (NASA technical memorandum ; 4726)

Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle [microform] / Roger A. Lepsch, Jr. and George M. Ware, Ian O. MacConochie (NASA technical memorandum ; 4726)
Microform図書
1996<YCA-NAS 1.15:4726>
National Diet Library
  • Subject Heading...tional control Lift drag ratio

Low-speed wind tunnel tests of two waverider configuration models [microform] / Robert J. Pegg, David E. Hahne, Charles E. Cockrell, Jr (NASA-TM ; 111795)

Low-speed wind tunnel tests of two waverider configuration models [microform] / Robert J. Pegg, David E. Hahne, Charles E. Cockrell, Jr (NASA-TM ; 111795)
Microform図書
1995<YCA-NAS 1.15:111795>
National Diet Library
  • Subject Heading...onal stability Lift drag ratio Aerodynamic stability Aerodyn...

低ブームSSBJの概念設計について

低ブームSSBJの概念設計について
Digital文書・図像類
堀之内, 茂, Horinouchi, Shigeru宇宙航空研究開発機構2007-03-31宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-05-045
Other Libraries in Japan
  • Subject Heading...et Mach number lift drag ratio

極超音速流中における超音速逆噴射のカプセル空力特性への影響

極超音速流中における超音速逆噴射のカプセル空力特性への影響
Digital文書・図像類
渡辺, 光則, 野村, 茂昭, 山本, 行光, 吉沢, 昭, 穂積, 弘一, 小山, 忠勇, Watanabe, Mitsunori, Nomura, Shigeaki, Yamamoto, Yukimitsu, Yoshizawa, Akira, Hozumi, Koichi, Koyama, Tadao航空宇宙技術研究所1997-07航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1329p.1-37
Other Libraries in Japan
  • Subject Heading...ft coefficient lift drag ratio

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