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Axial mode shock wave combustion instability in liquid propellant rocket enginesAxial mode shock wave combustion instability in liquid propellant rocket engines
Document ID
19670025271
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mitchell, C. E. (Princeton Univ. NJ, United States)
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
AMS-TR-798
NASA-CR-72259
Report Number: AMS-TR-798
Report Number: NASA-CR-72259
Accession Number
67N34600
Funding Number(s)
CONTRACT_GRANT: NASR-217
CONTRACT_GRANT: NSG-99-60
CONTRACT_GRANT: NSF GP-579
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK WAVE
LIQUID PROPELLANT ROCKET ENGINE
COMBUSTION INSTABILITY

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