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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 Numer...

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
  • Subject Heading...c flow viscous shock layer analysis stagn......ion streamline shock layer thermodynamic property blunte...

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
  • Subject Heading...iative heating shock layer shock wave emission spectrum ...
  • Note (General)...ating from the shock layer generated in f......nerated at the shock layer was introduced......ating from the shock layer, and its intensity was strong...

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