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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    Title :

    Calculation of transitional boundary-layer flows.


    Contributors:

    Published in:

    Publication date :

    1973-04-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Calculation of transitional boundary-layer flows.

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





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