Concept of rotation loss with reference to trailing vortex induced by flow ejected from GEM or ram wing; authors designate reduction of parasite drag "interference thrust" and propose that it must be taken into account on estimating GEM performance because of its large amount; investigation of mechanism of interference thrust may be useful to improve GEM performance or to find superior types of GEM.


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    Title :

    Aerodynamic drag of ground effect machines


    Additional title:

    Aerospace Eng


    Contributors:
    Ando, S. (author) / Miyashita, J. (author)

    Published in:

    Publication date :

    1961


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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