The plane problem of the vibrating airfoil in supersonic flow is dealt with and solved within the scope of a linearized theory by the method of the acceleration potential.


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    Title :

    Two-Dimensional Wing Theory in the Supersonic Range


    Contributors:
    Hoenl, H. (author)


    Publication date :

    1949-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Two-dimensional wing theory in supersonic range

    Hoenl, H. | Engineering Index Backfile | 1949



    Two-dimensional supersonic wing theory

    Vincenti, W. G. | NTRS | 1948


    Wing theory in supersonic flow

    Carafoli, Elie | TIBKAT | 1969