Vented vectoring-nozzle has superior thrust coefficient and is lighter in weight because it does not require completely enclosed elbow duct ordinarily used to deflect nozzle flow. Improved nozzle has primary nozzle and three-sided elbow deflector.


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    Titel :

    Vented vectoring-nozzle for STOL and V/STOL aircraft


    Beteiligte:
    Esker, D. W. (Autor:in)

    Erscheinungsdatum :

    1974-05-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Application of thrust vectoring for STOL

    Whitten, P. D. / Woodrey, R. W. / Hames, J. E. | NTRS | 1981


    Application of thrust vectoring for STOL

    WHITTEN, P. / WOODREY, R. / HAMES, J. | AIAA | 1981



    Integration of vectoring nozzles in a STOL transonic tactical aircraft

    BERNDT, D. / GLIDEWELL, R. / BARNES, G. | AIAA | 1985


    STOL characteristics of a tactical aircraft with thrust vectoring nozzles

    TAPE, ROBERT / GLIDEWELL, RONALD / BERNDT, DAVID | AIAA | 1987