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Combustion stabilization with acoustic cavities.An experimental and analytical study has been performed to develop the technology necessary for effective use of acoustic cavities to suppress acoustic modes of combustion instability. An unbaffled variation of the LM ascent engine has been made dynamically stable with acoustic cavities only; five different cavity configurations were found sufficient to produce dynamic stability. An analytical model was developed to calculate the damping contributed by the cavity. Further, subscale tests were made to determine the nonlinear acoustic impedance of these cavities.
Document ID
19720030288
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Oberg, C. L.
(North American Rockwell Corp. Rocketdyne Div., Canoga Park, Calif., United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1971
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 8
Subject Category
Thermodynamics And Combustion
Accession Number
72A13954
Funding Number(s)
CONTRACT_GRANT: NAS9-7498
Distribution Limits
Public
Copyright
Other

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