The progress with the use of deflected thrust in European V/STOL airplanes is reviewed. The difficulties which arise in adopting this concept are examined and commented upon in the light of the practical experience which has been accumulated.Several configurations are discussed: the single sided deflector, a more complex rotating cascade version, the tilting pod-engine configuration, and the vectoring nozzle.


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    Title :

    Development of Thrust Deflection and Vectoring - V/STOL


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    National Aeronautic and Space Engineering and Manufacturing Meeting ; 1966



    Publication date :

    1966-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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