Problem of reducing drag due to lift of wing alone to its minimum value for given lift; minimum drag must be obtained by distributing total lift in most appropriate way over surface of wing; how general criterion may be employed to determine both lift distribution for minimum drag and actual shape of lifting surface.


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    Title :

    Wings with minimum drag due to lift in supersonic flow


    Additional title:

    J Aero/Space Sciences


    Contributors:
    Ginzel, I. (author) / Multhopp, H. (author)

    Published in:

    Publication date :

    1960


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :