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Resonant combustionCircumferential variations in resonant pressure wave, resonant combustion diagnostic techniques, and hydrodynamic response of injectors to high amplitude chamber pressure oscillations
Document ID
19670006401
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Clayton, R. M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sotter, J. G. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Woodward, J. W. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
October 31, 1966
Subject Category
Thermodynamics And Combustion
Accession Number
67N15730
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
INJECTOR
COMBUSTION PHYSICS
PRESSURE WAVE
ROTATIONAL FLOW
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