Plane problem of vibrating wing in supersonic flow treated by method of acceleration potential. English translation from (ZWB) Forschungsbericht n 1903 Jan 1944.


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    Title :

    Two-dimensional wing theory in supersonic range


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:
    Hoenl, H. (author)


    Publication date :

    1949


    Size :

    34 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :