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Stabilization of premixed combustorsIn order to attain a sufficiently good insight into the fluid mechanical processes taking place in combustors operating on premixed, prevaporized, and preheated gases, an experimental facility was developed where the flow field is tractable both experimentally and analytically. The configuration adopted for the initial stage of the study is based on the use of a step to stabilized the combustion zone. The primary purpose of the experimental apparatus is to provide a facility for studying the effects of the elementary fluid mechanical processes on the stability of a model combustion system in order to further the understanding of the intrinsic mechanism of nonsteady phenomena, rather than to provide criteria for unstable operation of combustors, as expressed by overall performance parameters, such as the blowout and flashback limits.
Document ID
19790016838
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sawyer, R. F.
(California Univ. Berkeley, CA, United States)
Daily, J. W.
(California Univ. Berkeley, CA, United States)
Oppenheim, A. K.
(California Univ. Berkeley, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA. Lewis Res. Center Premixed Prevaporized Combustor Technol. Forum
Subject Category
Aircraft Propulsion And Power
Accession Number
79N25009
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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