Investigation in static test facility at Langley Laboratory is part of research program examining wing propeller configurations designed for VTOL and STOL applications; work extended to configuration having two propellers per semispan and covers effects of changes in vertical and longitudinal positions of propellers.


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    Title :

    Effects of propeller position and overlap on slipstream deflection characteristics of wing-propeller configuration equipped with sliding and fowler flap


    Additional title:

    NACA -- Tech Note


    Contributors:

    Published in:

    Publication date :

    1958


    Size :

    81 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




    Simulated propeller slipstream effects on a supercritical wing

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    Roosenboom, E. / Heider, A. / Schroder, A. et al. | British Library Conference Proceedings | 2007