Experimental results suggest that the boundary-layer mean profiles in hypersonic flows may be highly transitional in the outer part of the boundary layer before the transition process is detected at the surface. Means of determining the initial location where the transition process begins in the outer part of the boundary layer are considered.


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    Titel :

    Cone transitional boundary-layer structure at Me = 14.


    Beteiligte:
    Fischer, M. C. (Autor:in) / Weinstein, L. M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1972-05-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Cone Transitional Boundary-Layer Structure at Me = 14

    MICHAEL C. FIXHER AND LEONARD M. WEINSTEIN | AIAA | 1972


    Transitional Shock Wave-Boundary Layer Interaction over a Cone Flare Model at Hypersonic Conditions

    Asma, C. / European Space Agency / CIRA et al. | British Library Conference Proceedings | 2002


    Calculation of transitional boundary-layer flows.

    BUSHNELL, D. M. / ALSTON, D. W. | AIAA | 1973


    Calculation of transitional boundary-layer flows.

    Bushnell, D. M. / Alston, D. W. | NTRS | 1973