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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Vented vectoring-nozzle for STOL and V/STOL aircraft


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

    Erscheinungsdatum :

    01.05.1974


    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


    STOL characteristics of a tactical aircraft with thrust vectoring nozzles

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



    Integration of vectoring nozzles in a STOL transonic tactical aircraft

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