An implicit finite-difference computer code that uses a two-layer algebraic eddy viscosity model and exact geometric specification of the airfoil has been used to simulate transonic aileron buzz. The calculated results, which were performed on both the Illiac IV parallel computer processor and the Control Data 7600 computer, are in essential agreement with the original expository wind-tunnel data taken in the Ames 16-Foot Wind Tunnel just after World War II. These results and a description of the pertinent numerical techniques are included. (Kursetz)


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    Title :

    Calculation of transonic aileron buzz


    Additional title:

    Berechnung von Querruder-Summgeraeuschen bei transsonischen Geschwindigkeiten


    Contributors:
    Steger, J.L. (author) / Bailey, H.E. (author)

    Published in:

    AIAA-Papers ; Jan ; 1-12


    Publication date :

    1979


    Size :

    12 Seiten, 16 Bilder, 15 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Calculation of transonic aileron buzz

    STEGER, J. / BAILEY, H. | AIAA | 1979


    Calculation of Transonic Aileron Buzz

    J. L. Steger / H. E. Bailey | AIAA | 1980


    Calculation of transonic aileron buzz

    Steger, J.L. / Bailey, H.E. | Tema Archive | 1980


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