Results of a parametric test program of low pressure ratio deflected nozzles show the performance changes to be significant for vectoring nozzles and variations in nozzle thrust coefficients should be included in engine cycle trade studies to obtain realistic aircraft performance. Low pressure ratio deflected nozzle performance is shown to be sensitive to nozzle pressure ratio, nozzle contraction ratio, turning radius, diffuser area ratio and the presence of an integral core flow exhaust stream. The effectiveness of venting the inside surface of the nozzle turn is also demonstrated. (Kursetz)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Development of low pressure ratio vectoring nozzles for V/STOL aircraft


    Additional title:

    Entwicklung von Vektorschubduesen mit niedrigem Druckgroessenverhaeltnis fuer Senkrechtstartflugzeuge


    Contributors:

    Published in:

    Publication date :

    1977


    Size :

    8 Seiten, 17 Bilder


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    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


    STOL characteristics of a tactical aircraft with thrust vectoring nozzles

    Tape, R.F. / Glidewell, R.J. / Berndt, D.E. | Tema Archive | 1987