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    Attachment-line flow on an infinite swept wing (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-06-27
    Description: 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.
    Keywords: AERODYNAMICS
    Type: AIAA Journal; 12; Feb. 197
    Format: text
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