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Dilution jet mixing program, supplementary reportThe velocity and temperature distributions predicted by a 3-D numerical model and experimental measurements are compared. Empirical correlations for the jet velocity trajectory developed are presented. The measured velocity distributions for all test cases of phase through phase 3 are presented in the form of contour and oblique plots. quantification of the effects of the following on the jet mixing characteristics with a confined crossflow are: (1) orifice geometry momentum flux ratio and density ratio; (2) nonuniform mainstream temperature and velocity profiles upstream of dilution orifices; (3) cold versus hot jet injection; (4) cross-stream flow are a convergence as encountered in practical dilution zone geometries; (5) 2-D slot versus circular orifices; (6) discrete noncirculcer orifices; (7) single-sided versus opposed jets; (8) single row of jets.
Document ID
19860014385
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Srinivasan, R.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
White, C.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1986
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
REPT-21-4705
NAS 1.26:175043
NASA-CR-175043
Report Number: REPT-21-4705
Report Number: NAS 1.26:175043
Report Number: NASA-CR-175043
Accession Number
86N23856
Funding Number(s)
PROJECT: RTOP 533-04-12
CONTRACT_GRANT: NAS3-22110
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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