A proposed method for calculating three-dimensional incompressible laminar and turbulent boundary layers is investigated with respect to its applicability to incompressible attachment line flow on an infinite swept wing. The calculation results obtained exhibit satisfactory agreement with experimental data.


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    Titel :

    Attachment-line flow on an infinite swept wing


    Beteiligte:
    Cebeci, T. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1974-02-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




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