A discussion of some elements of ejector technology, as developed at DHC (DeHavilland Aircraft Co.), is presented. Three operational areas are considered, i.e. (a) Static or hovering condition; (b) Low forward speed (STOL regime); (c) High subsonic cruise. Subsequently, three project study aircraft are introduced to illustrate the application of ejectors in their respective operational areas. These aircraft are: (a) An advanced turbo fan powered STOL transport; (b) A STOVL supersonic combat aircraft; and (c) A STOVL subsonic support aircraft.


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    Title :

    Some Applications of Ejector Technology to STOL and V/STOL Aircraft Projects


    Contributors:

    Publication date :

    1982


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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