Analysis presented provides background for program, and data indicating effect of various components on overall drag of model; attention is devoted to drag of various hub-pylon combinations tested, and effect of rotor height above fuselage; conclusions pertaining to performance capabilities of helicopters of light observation category.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Full scale wind tunnel investigation of helicopter drag


    Additional title:

    Am Helicopter Soc -- J


    Contributors:
    Moser, H.H. (author)


    Publication date :

    1961


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :