Type of flow is associated with thrust vector control of rocket motors by gas injection, and occurs when gaseous fuel is injected into supersonic burner; analytic model of flow-field was constructed in which conservation of momentum is applied to control volume at jet nozzle exit; series of flat-plate experiments was conducted with normal, sonic jets at external flow Mach numbers of 2.61, 3.50, and 4.54; comparisons of trends predicted by analysis with two-dimensional force data from experiments and other sources showed good agreement; results of correlation of data obtained from experiments with finite-span slots.


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    Title :

    Study of interaction of gaseous jets from transverse slots with supersonic external flows


    Additional title:

    AIAA J


    Contributors:
    Spaid, F.W. (author) / Zukoski, E.E. (author)

    Published in:

    AIAA Journal ; 6 , n 2


    Publication date :

    1968


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :