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A single mode approximation in the solution of nonlinear combustion instability problemsUnstable liquid propellant rocket engine nonlinear behavior, considering stability of cylindrical combustor with distributed steady state combustion process and multiorifice quasi-steady nozzle
Document ID
19710037947
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Powell, E. A.
Zinn, B. T.
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 71-208
Report Number: AIAA PAPER 71-208
Meeting Information
Meeting: AEROSPACE SCIENCES MEETING
Location: NEW YORK, NY
Start Date: January 25, 1971
End Date: January 27, 1971
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
71A18644
Funding Number(s)
CONTRACT_GRANT: NGR-11-002-083
Distribution Limits
Public
Copyright
Other

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