Wave drag of cylindrical leading edge of slipping swept wing, and its dependence on angle of attack and angle of sweepback are investigated; it is shown that leading edge wave drag of swept wings and delta wings increases considerably when sweepback exceeds 30° of arc.


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    Title :

    Drag of blunt leading edge of swept wing in hypersonic flow


    Additional title:

    Soprotivlenie strelovidnoi zatuplennoi kromki kryla pri giperzvukovykh skorostyakh


    Contributors:


    Publication date :

    1964


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Russian


    Keywords :