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Interactive computer modeling of combustion chemistry and coalescence-dispersion modeling of turbulent combustionAn interactive computer code for simulation of a high-intensity turbulent combustor as a single point inhomogeneous stirred reactor was developed from an existing batch processing computer code CDPSR. The interactive CDPSR code was used as a guide for interpretation and direction of DOE-sponsored companion experiments utilizing Xenon tracer with optical laser diagnostic techniques to experimentally determine the appropriate mixing frequency, and for validation of CDPSR as a mixing-chemistry model for a laboratory jet-stirred reactor. The coalescence-dispersion model for finite rate mixing was incorporated into an existing interactive code AVCO-MARK I, to enable simulation of a combustor as a modular array of stirred flow and plug flow elements, each having a prescribed finite mixing frequency, or axial distribution of mixing frequency, as appropriate. Further increase the speed and reliability of the batch kinetics integrator code CREKID was increased by rewriting in vectorized form for execution on a vector or parallel processor, and by incorporating numerical techniques which enhance execution speed by permitting specification of a very low accuracy tolerance.
Document ID
19840012485
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pratt, D. T.
(Washington Univ. Seattle, WA, United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Combust. Fundamentals Res.
Subject Category
Inorganic And Physical Chemistry
Accession Number
84N20553
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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