The results of a finite-difference calculation of hypersonic transitional boundary-layer flow are presented. Precursor-transition and low Reynolds number turbulence effects are included. These calculation results are compared with data from a source where profiles are available at the beginning, middle and end of the hypersonic transitional flow. The results indicate that the low Reynolds number effect is the most important.


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    Titel :

    Calculation of transitional boundary-layer flows.


    Beteiligte:
    Bushnell, D. M. (Autor:in) / Alston, D. W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1973-04-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Calculation of transitional boundary-layer flows.

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





    Calculation of separated boundary-layer flows

    Cebeci, T. / Khalil, E.E. / Whitelaw, Y.H. | Tema Archiv | 1979