Advantage of swept back wing as compared to normal rectangular wing is in lower drag coefficients at higher Mach numbers; attempt made to show that propeller design by incorporating recent advances in theoretical and experimental airfoil design will continue to find application in modern high speed aircraft.


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    Title :

    Notes on propellers with swept back tips


    Additional title:

    Am Helicopter


    Contributors:
    Lawton, F. (author)

    Published in:

    Publication date :

    1947


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English