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Analysis of velocity-coupled response function data from the dual rotating valveThe results of a re-evaluation of the propellant combustion data obtained using the dual valve approach for measuring velocity-coupling characteristics of solid propellants are presented. Data analysis and testing procedures are described. The velocity response is compared to pressure-coupled response data within the context of thermal wave response theory. This comparison shows important inconsistencies which cast doubt on inferring the velocity response from pressure-coupled response functions.
Document ID
19810007745
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brown, R. S.
(United Technologies Corp. Sunnyvale, CA, United States)
Waugh, R. C.
(United Technologies Corp. Sunnyvale, CA, United States)
Date Acquired
August 11, 2013
Publication Date
November 1, 1980
Publication Information
Publication: NASA. Langley Research Center The 17th JANNAF Combust. Meeting, Vol. 1
Subject Category
Propellants And Fuels
Accession Number
81N16261
Funding Number(s)
CONTRACT_GRANT: F49620-77-C-00448
Distribution Limits
Public
Copyright
Other

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