Based on slipstream theory and blade theory, certain requirements for obtaining high degree of thrust are determined; possibilities of minimizing disadvantages resulting from high degree of thrust, discussed.


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    Titel :

    Physical limitations of attainable propeller thrust


    Weitere Titelangaben:

    Physikalische Grenzen des erroichbaren Standschubs


    Beteiligte:
    Betz, A. (Autor:in)


    Erscheinungsdatum :

    1938


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Deutsch


    Schlagwörter :


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