Pt 1: Propulsive characteristics of 2-and 3-bladed adjustable pitch propellers extended to fairly large blade angles; tip loss; blade deflection; wind tunnel wall interference. Pt 2: Airplane characteristics as affected by operation of propulsive system; experimental results and analysis of effect of power on lift, drag, performance, pitching moment, longitudinal stability, and elevator effectiveness.


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    Title :

    Wind tunnel tests on high wing monoplane with running propeller


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Publication date :

    1936


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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