Present study is extension of work described in NASA - Memo n 2-18-59 W indexed in Engineering Index 1959 p 12, and includes effects of surface curvature on pressure levels characteristic of separation and on length of separated region.


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    Titel :

    Shock-wave laminar-boundary-layer interaction on convex wall


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Greber, I. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    28 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Interaction of oblique shock wave with laminar boundary layer

    Hakkinen, R.J. / Greber, I. / Trilling, L. et al. | Engineering Index Backfile | 1959



    Interactions between shock wave and hypersonic laminar boundary layer near convex corner

    Hawboldt, R. J. / Sullivan, P. A. / Gottlieb, J. J. | AIAA | 1995


    Real Gas Effects on Hypersonic Shock Wave Laminar Boundary Layer Interaction

    Holden, Michael / Wadhams, Timothy / Candler, Graham | AIAA | 2003