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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    Title :

    Physical limitations of attainable propeller thrust


    Additional title:

    Physikalische Grenzen des erroichbaren Standschubs


    Contributors:
    Betz, A. (author)


    Publication date :

    1938


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German




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