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Dilution jet mixing program, phase 3The objectives of the program were: (1) to extend the data base on mixing of a single-sided row of jets with a confined crossflow, (2) to collect a data base on mixing of multiple rows of jets with confined crossflow, (3) to develop empirical jet mixing correlations, and (4) to perform limited three-dimensional calculations for some of these test configurations. The tests were performed with uniform mainstream conditions for several orifice plate configurations. Schematics of the test section and the orifice configurations are given. Temperature and pressure measurements were made in the test section at 4 axial and 11 transverse stations, using a 60-element rake probe. The measured temperature distributions for these tests are reported.
Document ID
19880001771
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Srinivasan, R.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Myers, G.
(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
October 1, 1985
Publication Information
Publication: NASA. Lewis Research Center, Turbine Engine Hot Section Technology, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
88N11153
Funding Number(s)
CONTRACT_GRANT: NAS3-22110
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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