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NASA dilution jet mixing, phase 3Many of the gas turbine combustors in operation use multiple rows of dilution jets, and some have geometries that are different from circular holes. The data base available in literature is generally applicable to a single row of circular holes. Tests were performed with uniform mainstream conditions for several orifice plate configurations. Temperature and pressure measurements were made in the test section at 4 axial and 11 transverse stations. These measurements were made with a 60-element rake probe. Test results for some of these cases are discussed.
Document ID
19870001769
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Srinivasan, R.
(Garrett Corp. Phoenix, AZ, United States)
Myers, G.
(Garrett Corp. Phoenix, AZ, United States)
White, C.
(Garrett Corp. Phoenix, AZ, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Turbine Engine Hot Section Technology, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
87N11202
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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