Results of tests described applied to case of oscillating airfoil and problem of plane airfoil entering sharp edged gust; in latter case rate of increase of lift after entrance of airfoil into gust boundary is determined, it is shown that during entire process lift acts at quarter chord point of airfoil. Before Inst Aeronautical Sciences.


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    Title :

    Airfoil theory for non-uniform motion


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Publication date :

    1938


    Size :

    12 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Airfoil theory for non-uniform motion

    von Karman, T. / Sears, W.R. | Engineering Index Backfile | 1938


    On theory of unsteady motion of airfoil

    Sedov, L.I. | Engineering Index Backfile | 1947




    Improved thin-airfoil theory

    ZEDAN, M. F. / ABU-ABDOU, K. | AIAA | 1988