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Amplification of Reynolds number dependent processes by wave distortionThe amplification of a Reynolds number dependent process by wave distortion and the possibility of applying the results to other similar Reynolds number dependent processes were investigated. The process investigated was that associated with the operation of a constant-temperature hot-wire anemometer. The application of vaporization limited combustion, the type of combustion typically associated with liquid propellant rocket engines, was studied. A series of experiments were carried out to determine the effect of wave distortion on a Reynolds number dependent process and to establish the analogy between the anemometer process and the combustion process. Parametric trends, behavior common to different chamber geometries, and stability boundaries were identified. The results indicate a high degree of similarity between the two processes and the possibility of using the anemometer system to investigate combustion instability. The nonlinear aspects of a Reynolds number dependent process appear to be the dominant mechanisms controlling instability.
Document ID
19800004938
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ventrice, M.
(Tennessee Technological Univ. Cookeville, TN, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1979
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
NASA-CR-159732
Report Number: NASA-CR-159732
Accession Number
80N13193
Funding Number(s)
CONTRACT_GRANT: NGR-43-003-015
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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