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Dilution jet mixing programParametric tests were conducted to quantify the mixing of opposed rows of jets (two-sided injection) in a confined cross flow. Results show that jet penetrations for two sided injections are less than that for single-sided injections, but the jet spreading rates are faster for a given momentum ratio and orifice plate. Flow area convergence generally enhances mixing. Mixing characteristics with asymmetric and symmetric convergence are similar. For constant momentum ratio, the optimum S/H(0) with in-line injections is one half the optimum value for single sided injections. For staggered injections, the optimum S/H(0) is twice the optimum value for single-sided injection. The correlations developed predicted the temperature distributions within first order accuracy and provide a useful tool for predicting jet trajectory and temperature profiles in the dilution zone with two-sided injections.
Document ID
19840018634
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Srinivasan, R.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Coleman, E.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Johnson, K.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-174624
NAS 1.26:174624
GARRETT-21-4804
Report Number: NASA-CR-174624
Report Number: NAS 1.26:174624
Report Number: GARRETT-21-4804
Accession Number
84N26702
Funding Number(s)
CONTRACT_GRANT: NAS3-22110
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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