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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    Title :

    Two-dimensional secondary jet interaction with supersonic stream


    Additional title:

    AIAA J


    Contributors:
    Hawk, N.E. (author) / Amick, J.L. (author)

    Published in:

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


    Publication date :

    1967


    Size :

    16 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



    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 Flows Due to Supersonic Secondary Jets

    Charwat, Andrew F. | Springer Verlag | 1968