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A Multi-domain Spectral Method for Supersonic Reactive FlowsThis paper has a dual purpose: it presents a multidomain Chebyshev method for the solution of the two-dimensional reactive compressible Navier-Stokes equations, and it reports the results of the application of this code to the numerical simulations of high Mach number reactive flows in recessed cavity. The computational method utilizes newly derived interface boundary conditions as well as an adaptive filtering technique to stabilize the computations. The results of the simulations are relevant to recessed cavity flameholders.
Document ID
20020079876
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Don, Wai-Sun
(Brown Univ. Providence, RI United States)
Gottlieb, David
(Institute for Computer Applications in Science and Engineering Hampton, VA United States)
Jung, Jae-Hun
(Brown Univ. Providence, RI United States)
Bushnell, Dennis M.
Date Acquired
September 7, 2013
Publication Date
August 1, 2002
Subject Category
Numerical Analysis
Report/Patent Number
NASA/CR-2002-211763
ICASE-2002-29
NAS 1.26:211763
Report Number: NASA/CR-2002-211763
Report Number: ICASE-2002-29
Report Number: NAS 1.26:211763
Funding Number(s)
CONTRACT_GRANT: DE-FG02-96ER-25346
CONTRACT_GRANT: F49620-02-1-0113
PROJECT: RTOP 505-90-52-01
CONTRACT_GRANT: NAS1-97046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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