This report shows that wall cooling can be an effective means of increasing the stability of laminar boundary layer flows. The stability of two general classes of cooled boundary layer flows was investigated; shock tube induced boundary layers, and cooled subsonic steady flow boundary layers (such as that on a cooled aerodynamic surface in free flight or in a wind tunnel).


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Stability of highly-cooled compressible laminar boundary layers


    Weitere Titelangaben:

    Stabilitaet stark gekuehlter kompressibler, laminarer Grenzschichten


    Beteiligte:
    Boehman, L.I. (Autor:in) / Mariscalco, M.G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1976


    Format / Umfang :

    131 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




    Self-Similar Compressible Laminar Boundary Layers

    Toro, P. G. P. / Rusak, Z. / Nagamatsu, H. T. et al. | British Library Conference Proceedings | 1997


    Self-similar compressible laminar boundary layers

    Toro, P. / Rusak, Z. / Nagamatsu, H. et al. | AIAA | 1997


    INSTABILITY OF COMPRESSIBLE LAMINAR BOUNDARY LAYERS

    GASPERUS, C. / ANTAR, B. | AIAA | 1985


    Machine Calculaltion of Compressible Laminar Boundary Layers

    A. M. O. Smith / Darwin W. Clutter | AIAA | 2003


    Machine calculation of compressible laminar boundary layers

    CLUTTER, D. W. / SMITH, A. M. O. | AIAA | 1965