Transonic tunnel test was performed to determine the static performance of five twin-engine nonaxisymmetric nozzles and a base-line axisymmetric nozzle at three nozzle power settings. Static thrust-vectoring and thrust-reversing performance were also determined. Nonaxisymmetric-nozzle concepts included two-dimensional convergent-divergent nozzles, wedge nozzles, and a nozzle with a single external-expansion ramp. All nonaxisymmetric nozzles had essentially the same statis performance as the axisymmetric nozzle. Effective thrust vectoring and reversing was also achieved.


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    Titel :

    Static performance of five twin-engine nonaxisymmetric nozzles with vectoring and reversing capability


    Beteiligte:
    Capone, F. J. (Autor:in)

    Erscheinungsdatum :

    01.07.1978


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Static Performance of Vectoring/Reversing Nonaxisymmetric Nozzles

    C.M. Willard / F. J. Capone / M. Konarski et al. | AIAA | 1979


    Installed Performance of Vectoring/Reversing Nonaxisymmetric Nozzles

    P. E. Hiley / D. E. Kitzmiller / C. M. Willard | AIAA | 1979


    Thrust reversing effects on twin-engine aircraft having nonaxisymmetric nozzles

    Capone, F. J. / Re, R. J. / Bare, E. A. | NTRS | 1981