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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    Title :

    Attachment-line flow on an infinite swept wing


    Contributors:
    Cebeci, T. (author)

    Published in:

    Publication date :

    1974-02-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :






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