Design and experimental studies are reviewed which demonstrate the effect of vectored nozzle type, shape, location and orientation on V/STOL aircraft design and performance. Single and twin engine aircraft differences are discussed. Complete aircraft sizing and mission results are displayed for twin engine aircraft.


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    Title :

    Effect of Exhaust Deflectors on the Design of Lift Plus Lift/Cruise V/STOL Aircraft


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    National Aerospace Engineering and Manufacturing Meeting ; 1973



    Publication date :

    1973-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English