Measurements have been made of the lift on an airfoil in pitching oscillation with a continuous-recording, instantaneous-force balance. The experimental values for the phase difference between the angle of attack and the lift are shown to be in close agreement with theory.


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    Title :

    Experimental Verification of the Theory of Oscillating Airfoils


    Contributors:

    Publication date :

    1939-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



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