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Jet mixing into a heated cross flow in a cylindrical duct - Influence of geometry and flow variationsTo examine the mixing characteristics of jets in an axi-symmetric can geometry, temperature measurements were obtained downstream of a row of cold jets injected into a heated cross stream. Parametric, non-reacting experiments were conducted to determine the influence of geometry and flow variations on mixing patterns in a cylindrical configuration. Results show that jet to mainstream momentum flux ratio and orifice geometry significantly impact the mixing characteristics of jets in a can geometry. For a fixed number of orifices, the coupling between momentum flux ratio and injector determines (1) the degree of jet penetration at the injection plane, and (2) the extent of circumferential mixing downstream of the injection plane. The results also show that, at a fixed momentum flux ratio, jet penetration decreases with (1) an increase in slanted slot aspect ratio, and (2) an increase in the angle of the slots with respect to the mainstream direction.
Document ID
19920044486
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hatch, M. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Sowa, W. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Samuelson, G. S.
(California, University Irvine, United States)
Holdeman, J. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 92-0773
Accession Number
92A27110
Funding Number(s)
CONTRACT_GRANT: NAG3-1110
Distribution Limits
Public
Copyright
Other

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