Tests were conducted in University of Michigan 8 × 13-in. supersonic tunnel at 3.97 Mach and 0.12 × 106/in. Re; test model consisted of wedge of rectangular planform equipped with side plates and fullspan jet slot near base; primary data taken were jet mass flow, normal force increment due to jet, and schlieren photographs; for range of variables covered, momentum flux ratio was found to govern flow geometry, including location of transition in separated shear layer; data on aerodynamic interaction in case of approximately 2-dimensional slot-jet configurations were collected from four sources.


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    Titel :

    Two-dimensional secondary jet interaction with supersonic stream


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Hawk, N.E. (Autor:in) / Amick, J.L. (Autor:in)

    Erschienen in:

    AIAA Journal ; 5 , n 4 ; p 655-670


    Erscheinungsdatum :

    1967


    Format / Umfang :

    16 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Interaction of supersonic stream and transverse supersonic jet

    Charwat, A.F. / Allegre, J. | Engineering Index Backfile | 1964


    Interaction of a supersonic stream and a transverse supersonic jet

    ALLEGRE, J. / CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE / LABORATOIRE D'AEROTHERMIQUE et al. | AIAA | 1964


    Supersonic transverse injection into a supersonic stream.

    MAHAFFEY, R. E. / SCHETZ, J. A. | AIAA | 1968


    Interaction between supersonic stream and parallel subsonic stream bounded by fluid at rest

    Ribner, H.S. / Arnoff, E.L. | Engineering Index Backfile | 1952