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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規格・テクニカルリポート類
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...layer analysis stagnation streamline shock layer thermodynamic pro...
  • Note (General)...ach to solving stagnation streamline profiles both quickly and acc...

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