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Evaluation of acoustic cavities for combustion stabilization.The stabilizing influence of acoustic cavities (quarterwave acoustic resonators) on acoustic modes of combustion instability has been studied. The ability to analytically predict cavity damping was improved. Relatively good agreement between predicted damping and measured stability was demonstrated. Full-scale motor firings were made to evaluate the influence of several parameters on stability. Results from these firings showed that stability was changed, but not dramatically, by changes in the engine operating conditions. Variations in the film-coolant flowrate do not significantly affect cavity stabilization. The ability to stabilize an engine with unconventional cavity configurations was demonstrated.
Document ID
19730028650
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Oberg, C. L.
Wong, T. L.
Ford, W. M.
(North American Rockwell Corp. Rocketdyne Div., Canoga Park, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 72-1147
Meeting Information
Meeting: Joint Propulsion Specialist Conference
Location: New Orleans, LA
Country: US
Start Date: November 29, 1972
End Date: December 1, 1972
Sponsors: Society of Automotive Engineers, American Institute of Aeronautics and Astronautics
Accession Number
73A13452
Funding Number(s)
CONTRACT_GRANT: NAS9-9866
Distribution Limits
Public
Copyright
Other

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