The effect was studied of nose geometry on the transition criteria for the windward boundary layer, on the extent of separation, on the heat transfer perturbation due to the canopy, and on the surface pressure and the heat transfer in the separated region. The data for each of these problems is analyzed. A literature review that concentrates on separation and the leeward flow-field is presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    The effect of nose geometry on the aerothermodynamic environment of shuttle entry configurations


    Beteiligte:
    Bertin, J. J. (Autor:in) / Martindale, W. R. (Autor:in) / Faria, H. T. (Autor:in) / Graumann, B. W. (Autor:in) / Horn, M. K. (Autor:in) / Johnson, G. W. (Autor:in)

    Erscheinungsdatum :

    01.01.1973


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Effect of Nose Geometry on the Aerothermodynamic Environment of Shuttle Entry Configurations

    JOHN J. BERTIN / H. TOM FARIA / WINSTON D. GOODRICH AND W. R. MARTINDALE | AIAA | 1974


    Effect of nose geometry on the aerothermodynamic environment of shuttle entry configurations.

    Bertin, J. J. / Faria, H. T. / Goodrich, W. D. et al. | NTRS | 1973




    Aerothermodynamic Entry Environment of the Space Shuttle Orbiter

    Collicott, Howard E. / Bauer, Paul E. | AIAA | 1983