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[American Institute of Aeronautics and Astronautics Aircraft Engineering, Technology, and Operations Congress - Los Angeles,CA,U.S.A. (19 September 1995 - 21 September 1995)] Aircraft Engineering, Technology, and Operations Congress - Calculation method for supersonic/hypersonic flows over configurations with blunt leading edges

✍ Scribed by Voevodenko, N

Book ID: 121043202
Publisher: American Institute of Aeronautics and Astronautics
Year: 1995
Weight: 472 KB
Category: Article
DOI: 10.2514/6.1995-3924

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