Boundary layer in neighborhood of centerline of symmetry with adverse pressure gradients and heat transfer is studied with view toward assessing importance of three-dimensional effects on such boundary layers in hypersonic inlets of airbreathing engines; two approaches are employed; in one, analysis is performed so that parameters describing external flow and surface geometry are restricted to those yielding similar boundary layers; numerical results are presented; second approach is integral method which can be applied for similar and nonsimilar flows. (See also AIAA-ASME -- Hypersonic Ramjet Conference -- Paper 63-115 1963 36 p)


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    Titel :

    Laminar boundary layer near plane of symmetry of hypersonic inlet


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Libby, P.A. (Autor:in) / Fox, H. (Autor:in) / Sanator, R.J. (Autor:in) / DeCarlo, J. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 12


    Erscheinungsdatum :

    1963


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch