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Multi-phase simulations of coaxial injector combustionA multiphase computational fluid dynamics code (ARICC-3D) is presented and results of two simulations are discussed. The numerical framework of the CFD code is reviewed as well as some of the two-phase physical submodels. The simulations performed include a single coaxial element injector and a multielement injector using LOX/Hydrogen reactants. The single element injector simulation verified the interaction among the code's submodels. The multielement injector simulation transient results include the chamber response to a transverse pressure wave with and without a chamber baffle. The results of these simulations demonstrate the current capabilities and their limitations to model complex two-phase combustion phenomena. Possible ways to exceed these limitations are suggested.
Document ID
19920043166
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Liang, P. Y.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Ungewitter, R. J.
(Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 92-0345
Accession Number
92A25790
Funding Number(s)
CONTRACT_GRANT: NAS8-37480
Distribution Limits
Public
Copyright
Other

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