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Perspectives on dilution jet mixingA microcomputer code which displays 3-D oblique and 2-D plots of the temperature distribution downstream of jets mixing with a confined crossflow has been used to investigate the effects of varying the several independent flow and geometric parameters on the mixing. Temperature profiles calculated with this empirical model are presented to show the effects of orifice size and spacing, momentum flux ratio, density ratio, variable temperature mainstream, flow area convergence, orifice aspect ratio, and opposed and axially staged rows of jets.
Document ID
19860064876
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Holdeman, J. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Srinivasan, R.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 86-1611
Accession Number
86A49614
Distribution Limits
Public
Copyright
Other

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