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Reentry-F flowfield solutions at 80,000 ft. [microform] / W.A. Wood, C.J. Riley, and F.M. Cheatwood (NASA technical memorandum ; 112856)

Reentry-F flowfield solutions at 80,000 ft. [microform] / W.A. Wood, C.J. Riley, and F.M. Cheatwood (NASA technical memorandum ; 112856)
Microform図書
1997<YCA-NAS 1.15:112856>
National Diet Library
  • Subject Heading...Turbulent flow Shock layers Navier-Stokes equation Numeri...

Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique [microform] : progress report for the period ended June 30, 1994 / by J.K. Ahuja, D.J. Singh, and S.N. Tiwari, principal investigator ([NASA contractor report] ; NASA CR-197013)

Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique [microform] : progress report for the period ended June 30, 1994 / by J.K. Ahuja, D.J. Singh, and S.N. Tiwari, principal investigator ([NASA contractor report] ; NASA CR-197013)
Microform図書
1994<YCA-NAS 1.26:197013>
National Diet Library
  • Subject Heading...on Projectiles Shock layers Shock waves Viscous flow

The development of a new viscous shock-layer code for computing hypersonic flows around blunted body and its applications

The development of a new viscous shock-layer code for computing hypersonic flows around blunted body and its applications
Digital文書・図像類
口石, 茂, Kuchiishi, Shigeru宇宙航空研究開発機構2005-10-03宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-05-001E
Other Libraries in Japan

READ実験

READ実験
Digital文書・図像類
安部, 隆士, 藤田, 和央, 若林, 昭, 伊地智, 幸一, Abe, Takashi, Fujita, Kazuhisa, Wakabayashi, Akira, Ijichi, Koichi宇宙航空研究開発機構2005-03-31宇宙航空研究開発機構研究開発報告: USERS REVカプセルの開発研究および飛行後解析 = JAXA Research and Development Report: Research and Development of USERS REV Capsule and its Post-flight AnalysisJAXA-RR-04-045p.127-135
Other Libraries in Japan

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