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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    Titel :

    Notes on propellers with swept back tips


    Weitere Titelangaben:

    Am Helicopter


    Beteiligte:
    Lawton, F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1947


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    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