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Effect of chamber pressure, flow per element, and contraction ratio on acoustic-mode instability in hydrogen-oxygen rocketsChamber pressure, contraction ratio, and flow per element effects on acoustic mode instability in hydrogen oxygen engines
Document ID
19680021046
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Feiler, C. E. (NASA Lewis Research Center Cleveland, OH, United States)
Morgan, C. J. (NASA Lewis Research Center Cleveland, OH, United States)
Wanhainen, J. P. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1968
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-4733
Report Number: NASA-TN-D-4733
Accession Number
68N30518
Funding Number(s)
CONTRACT_GRANT: 128-31-06-05-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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