Stability expressed in terms of position of axis of rotation of airfoil, reduced frequency, Mach number, ratio of amplitudes of torsonial and flexural modes, and phase angle between modes and evaluations are made for Mach numbers ranging from 1.2 to 2.0 and for reduced frequencies from 0.1 to 2.0; tables of aerodynamic parameters for oscillating airfoil in supersonic flow given.


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    Title :

    Stability of oscillating airfoil in supersonic airflow


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1948


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English