Equations are developed using the source distribution method for the velocity potential function and pressure on thin wings in steady and unsteady motion. Closed form solutions are given for harmonically oscillating wings of general plan form including the effect of the wing wake. Some useful examples are presented in an appendix for arrow, semielliptical, and hexagonal plan form wings.


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    Title :

    Finite Span Wings in Compressible Flow


    Contributors:

    Publication date :

    1956-09-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Finite span wings in compressible flow

    Krasilshchikova, E.A. | Engineering Index Backfile | 1956



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    Goossens, E. | Emerald Group Publishing | 1947


    Downwash behind wings of finite span

    Goossens, E. | Engineering Index Backfile | 1947