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Dilution Jet Mixing Program, phase 1The effect of jet to mainstream density ratio, flow area convergence as encounted in transition sections, and nonuniform mainstream profile upstream of dilution orifices on the mixing of a row of jets with a confined cross flow was quantified. It is found that: (1) jet spreading rate in transverse direction is increased with increasing J, H/D and with decreasing S/D; (2) the density ratio has only a second order effect on the jet mixing characteristics for a constant momentum ratio; (3) the temperature distributions in the jet mixing region are strongly influenced by the undisturbed mainstream profile; (4) flow area convergence enhances mixing in radial and transverse directions. An asymmetric convergent duct with flat wall injection has the same jet mixing characteristics as a symmetric convergent duct. An asymmetric convergent duct with slant wall injection has a faster jet spreading rate in the transverse direction.
Document ID
19830007319
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Srinivasan, R.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Berenfeld, A.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Mongia, H. C.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
GARRETT-21-4302
NASA-CR-168031
NAS 1.26:168031
Report Number: GARRETT-21-4302
Report Number: NASA-CR-168031
Report Number: NAS 1.26:168031
Accession Number
83N15590
Funding Number(s)
CONTRACT_GRANT: NAS3-22110
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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