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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    Title :

    Effect of bluntness on hypersonic two-dimensional inlet type flows


    Additional title:

    NASA CR


    Contributors:

    Published in:

    Publication date :

    1968


    Size :

    91 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :