Formulas for supersonic loading, lift, and drag of flat swept-back wings with leading edges behind mach lines. (35¢)


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    Title :

    Formulas for supersonic loading, lift, and drag of flat swept-back wings with leading edges behind mach lines


    Additional title:

    NACA -- Report


    Contributors:
    Cohen, D. (author)


    Publication date :

    1951


    Size :

    40 pages


    Remarks:

    Diagrams, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :