Investigation of effect of bluntness on two-dimensional hypersonic inlet type flows; tests were performed on two geometric configurations -- flat plate and isentropic compression ramp -- each accommodating leading edges of three different radii; results are compared with theoretical analyses and reflect blunt leading-edge effects on inviscid-flow profiles, surface-pressure phenomena and viscous-layer growth along models, with and without incident shock wave-boundary layer interactions. (09561)


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    Titel :

    Effect of bluntness on hypersonic two-dimensional inlet type flows


    Weitere Titelangaben:

    NASA CR


    Beteiligte:
    Sanator, R.J. (Autor:in) / Boccio, J.L. (Autor:in) / Shamshins, D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    91 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :