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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    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






    High Efficiency Forward Swept Propellers at Low Speed

    Paxton, C. / Gryn, P. / Hines, E. et al. | British Library Conference Proceedings | 2003


    High Efficiency Forward Swept Propellers at Low Speeds

    Paxton, Craig / Gryn, Peter / Hines, Erisa et al. | AIAA | 2003


    General notes on propellers

    Engineering Index Backfile | 1949