Such mixing of two turbulent streams is of interest in problem of spreading of turbojet or rocket engine exhausts in flight; it is simplest logical extension of free jet mixing; experiments to determine effects on mixing of varying initial Mach numbers and stagnation temperature ratio; results exhibited marked effect of secondary Mach number; this was greatest for subsonic primary Mach numbers; practical correlation between spreading rates found for subsonic Mach numbers.


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    Title :

    Mixing of unbounded coaxial compressible streams


    Additional title:

    Jet Propulsion


    Contributors:
    Willis, D.R. (author) / Glassman, I. (author)

    Published in:

    Jet Propulsion ; 27 , n 12


    Publication date :

    1957


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :