Research on reflection plane models of straight, swept, and delta wings in 3×4-ft transonic test facility at Cornell Aeronautical Laboratory.


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    Title :

    Flutter model testing at transonic speeds


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1957


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Nonlinear analysis of airfoil flutter at transonic speeds

    Morton, Scott / Beran, Philip | AIAA | 1995




    Hopf-Bifurcation Analysis of Airfoil Flutter at Transonic Speeds

    Scott A. Morton / Philip S. Beran | AIAA | 1999


    Hopf-bifurcation analysis of airfoil flutter at transonic speeds

    Morton, Scott / Beran, Philip | AIAA | 1996