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Experimental clean combustor program noise measurement addendum, phase 1The test results of combustor noise measurements taken with waveguide probes are presented. Waveguide probes were shown to be a viable measurement technique for determining high sound pressure level broadband noise. A total of six full-scale annular combustors were tested and included the three advanced combustor designs: swirl-can, radial/axial, and double annular.
Document ID
19750022104
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Emmerling, J. J.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GE75AEG315
NASA-CR-134853
Report Number: GE75AEG315
Report Number: NASA-CR-134853
Accession Number
75N30177
Funding Number(s)
CONTRACT_GRANT: NAS3-16830
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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