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Application of advanced diagnostics to airblast injector flowsThis effort is concerned with the application of both conventional laser velocimetry and phase Doppler anemometry to the flow produced by an airblast nozzle. The emphasis is placed on the acquisition of data using actual engine injector/swirler components at (noncombusting) conditions simulating those encountered in the engine. The objective of the effort was to test the applicability of the instrumentation to real injector flows, to develop information on the behavior of injectors at high flow, and to provide data useful in the development of physical models of injector flows.
Document ID
19890007935
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mcvey, John B.
(United Technologies Research Center East Hartford, CT, United States)
Kennedy, Jan B.
(United Technologies Research Center East Hartford, CT, United States)
Russell, Sid
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Publication Information
Publication: NASA, Lewis Research Center, Turbine Engine Hot Section Technology, 1987
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
89N17306
Funding Number(s)
CONTRACT_GRANT: NAS3-24352
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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