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.
Mixing of unbounded coaxial compressible streams
Jet Propulsion
Jet Propulsion ; 27 , n 12
1957
8 pages
Article (Journal)
English
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