Investigation proves that ratio of net static thrust on single engined airplane to propeller shaft thrust varied from 0.85 on high wing monoplane with several struts in slip stream to 0.95 on streamlined low wing monoplane.


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    Title :

    Some full scale static propeller characteristics


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Enos, L.H. (author)


    Publication date :

    1937


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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