Applicability of boundary layer transition and turbulent heat transfer data for lifting reentry vehicle at hypersonic speed to space shuttles


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    Title :

    Transitional and turbulent heat transfer correlations for a lifting entry vehicle at Mach 10


    Contributors:
    Reda, D. C. (author) / Roberge, A. M. (author) / Young, C. H. (author)


    Publication date :

    1970-07-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Hypersonic Transitional and Turbulent Flow Studies on a Lifting Entry Vehicle

    C. H. YOUNG / D. C. REDA / AND A. M. ROBERGE | AIAA | 1972



    Flat surface heat-transfer correlations for Martian entry

    Tauber, M. E. / Yang, L. / Paterson, J. | NTRS | 1993



    Measurements in a transitional/turbulent Mach 10 boundary layer at high-Reynolds numbers.

    Watson, R. D. / Harris, J. E. / Anders, J. B., Jr. | NTRS | 1973