Using helium hypersonic wind tunnel, exploratory studies are made of flow over simple 2- and 3-dimensional bodies at Mach numbers from 11 to 19; studies of flow over flat plate and preliminary results for other configurations, including flat plates with flaps, delta wings, base pressure models, blunt models and slim cones; some preliminary results of boundary layer studies and dissolving models.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Exploratory studies of hypersonic fluid mechanics


    Additional title:

    AGARD Report


    Contributors:

    Published in:

    Publication date :

    1957


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Exploratory hypersonic boundary-layer transition studies

    HENDERSON, A. / ROGALLO, R. S. / SPITZER, C. R. et al. | AIAA | 1965


    Exploratory Studies of Turbulence/Chemistry Interaction in Hypersonic Flows

    Martin, M. P. / AIAA | British Library Conference Proceedings | 2003


    Hypersonic Flight Mechanics

    A. Busemann / N. X. Vinh / R. D. Culp | NTIS | 1976


    Hypersonic Flight Mechanics

    Busemann, A. / Vinh, N. X. / Culp, R. D. | NTRS | 1976