Pressure distributions on nozzle block of two-dimensional, oblique-exit-plane nozzle with turbulent flow were predicted and experimentally measured; thrusts, thrust vectors, and torques were calculated from pressure distributions; performance characteristics were strongly dependent upon plenum and ambient pressures and upon exit plane orientations; because of exit plane area changes, axial and lateral thrusts were found to exceed symmetric nozzle thrust values for certain conditions; results were predicted well by theory of characteristics and Gadd's formula for flow separation; at high altitudes, torque that can be obtained may be useful for maneuvering.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Thrust vectoring produced by supersonic nozzle with oblique exit plane


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Dunn, B.M. (Autor:in) / Emery, A.F. (Autor:in)

    Erschienen in:

    Journal of Spacecraft and Rockets ; 3 , n 10 ; p 1500-1503


    Erscheinungsdatum :

    1966


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Thrust-Vectoring Nozzle Performance Modeling

    Erich A. Wilson / Dan Adler / Pinhas Bar-Yoseph | AIAA | 2003


    Counterflow thrust vectoring of supersonic jets

    Strykowski, P. / Krothapalli, A. / Forliti, D. | AIAA | 1996


    Counterflow Thrust Vectoring of Supersonic Jets

    Strykowski, P.J. | Online Contents | 1996