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Computing Instability In Combustion Of Liquid PropellantsComputational fluid dynamics (CFD) code developed for use in design analyses of flow instabilities associated with combustion of sprayed liquid propellants in rocket engines. Code also contributes to design of improved commercial sprayed-fuel combustors in furnaces and jet engines. Proves robust, user-friendly software tool with comprehensive analysis capability. Enables characterization of stability or instability of engine in terms of such physically meaningful parameters as initial conditions of spray, spatial distribution of ratio between concentrations of fuel and oxidizer at injector faces, geometry of combustor, and configurations of baffles.
Document ID
19950071257
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Chen, Yen-Sen
(Engineering Sciences, Inc.)
Shang, Huan-Min
(Engineering Sciences, Inc.)
Date Acquired
August 17, 2013
Publication Date
December 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 12
ISSN: 0145-319X
Subject Category
Physical Sciences
Report/Patent Number
MFS-26268
Accession Number
95B10653
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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