Experimental determination of lift and moment on oscillating airfoil; results compared with predictions of vortex sheet theory as described in NACA -- Report 496, 1935; use of theory on aeroelastic problems such as flutter could then be verified or modified. Supersedes NACA -- Tech Note 2465.


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    Title :

    Experimental aerodynamic derivatives of sinusoidally oscillating. Airfoil in two-dimensional flow


    Additional title:

    NACA -- Report


    Contributors:


    Publication date :

    1952


    Size :

    44 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :