The high-temperature environment poses an unusual challenge in understanding the basic physics of hypersonic flight. A lack of such understanding can lead to risks and uncertainties in the design of aerospace vehicles. Hypersonic Nonequilibrium Flows documents recent, unprecedented scientific advances in the field of nonequilibrium processes for aerospace applications. These advances have been driven primarily by interest in space access and exploration, or in developing military technologies involving hypersonic flight regimes.


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    Titel :

    High-Enthalpy Facilities and Plasma Wind Tunnels for Aerothermodynamics Ground Testing


    Beteiligte:
    Josyula, Eswar (Autor:in)


    Erscheinungsdatum :

    2015-01-01


    Format / Umfang :

    14 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Non-Reflected Shock Tunnel for High Enthalpy Aerothermodynamics - Review of Performance

    Mudford, N. R. / Gai, S. L. / IUTAM | British Library Conference Proceedings | 1994