Relationship of swept wing to compressibility and shock wave is shown graphically; reference made to German practice; factors involved in design for Mach Numbers approaching unity and beyond are studied; compromise wing design is suggested.


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    Title :

    Swept wing at high velocity


    Additional title:

    Aeroplane


    Published in:

    Aeroplane ; 70 , n 1823


    Publication date :

    1946


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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