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[American Institute of Aeronautics and Astronautics 20th Aerospace Sciences Meeting - Orlando,FL,U.S.A. (11 January 1982 - 14 January 1982)] 20th Aerospace Sciences Meeting - Heat transfer rate for laminar, transition and turbulent boundary layer and transition phenomenon on shock tube wall

✍ Scribed by DILLON, JR., R.; NAGAMATSU, H.

Book ID: 121029399
Publisher: American Institute of Aeronautics and Astronautics
Year: 1982
Weight: 568 KB
Category: Article
DOI: 10.2514/6.1982-32

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