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Transition mixing study empirical model reportThe empirical model developed in the NASA Dilution Jet Mixing Program has been extended to include the curvature effects of transition liners. This extension is based on the results of a 3-D numerical model generated under this contract. The empirical model results agree well with the numerical model results for all tests cases evaluated. The empirical model shows faster mixing rates compared to the numerical model. Both models show drift of jets toward the inner wall of a turning duct. The structure of the jets from the inner wall does not exhibit the familiar kidney-shaped structures observed for the outer wall jets or for jets injected in rectangular ducts.
Document ID
19880020692
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Srinivasan, R.
(Garrett Engine Co. Phoenix, AZ, United States)
White, C.
(Garrett Engine Co. Phoenix, AZ, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1988
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:182139
NASA-CR-182139
GARRETT-21-6689
Report Number: NAS 1.26:182139
Report Number: NASA-CR-182139
Report Number: GARRETT-21-6689
Accession Number
88N30076
Funding Number(s)
CONTRACT_GRANT: NAS3-24340
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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