The present report discusses launcher flow-field data from complementary cold-gas test programs conducted at the University of Texas at Austin. Based on these data, flow-field models for the constrictive launcher configurations have been defined as a function of the nozzle-exit location and of the stagnation pressure in the nozzle reservoir. The conclusions are based on the configurations of the present experimental program.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Experimental Study of an Underexpanded, Supersonic Nozzle Exhausting into a Constrictive Launch Tube


    Beteiligte:
    J. J. Bertin (Autor:in) / R. R. Morris (Autor:in) / G. M. Garms (Autor:in) / M. R. Motal (Autor:in) / H. T. Faria (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    61 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Study of the exhaust plume for highly underexpanded supersonic nozzles exhausting into quiescent air

    Sutter, S.J. / Bertin, J.J. / Zihlman, E.J. jun. et al. | Tema Archiv | 1979



    Underexpanded jets exhausting from a rectangular channel into a slot ambient space

    Kiselev, S. P. / Kiselev, V. P. / Zaikovskii, V. N. | American Institute of Physics | 2021

    Freier Zugriff

    Underexpanded Supersonic Jets from Elliptical Nozzle with Aft Deck

    Nageswara Rao, A. / Kushari, Abhijit | AIAA | 2020