Through application of linearized theory compressibility correction is obtained which gives thrust or torque coefficient in subsonic flow, for propeller or helicopter rotor, directly from incompressible flow values.


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    Title :

    Subsonic compressibility corrections for propellers and helicopter rotors


    Additional title:

    J. Aeronautical Sciences


    Contributors:
    Laitone, E.V. (author) / Talbot, L. (author)

    Published in:

    Publication date :

    1953


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English