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Computational modelling of dump combustors flowfieldA computational model aimed at predicting the flowfield of dump combustors is presented. The turbulent combustion model is based on the conserved scalar approach and on a convenient specification of its probability density function, which reduces the computation of the mean density to a closed form. Turbulence is modeled by means of the k-epsilon model. The averaged conservation equations are solved by a technique based on a staggered grid and on the SIMPLE solver. The computational model is applied to a simple dump combustor to assess the computer time requirements and accuracy. The turbulent combustion model is shown to reduce the computer time by an order of magnitude when compared to evaluating the mean density by numerical quadrature.
Document ID
19910011783
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lentini, D.
(La Sapienza Univ. Rome (Italy)., United States)
Jones, W. P.
(Imperial Coll. of Science and Technology London, United Kingdom)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA, Lewis Research Center, Computational Fluid Dynamics Symposium on Aeropropulsion
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
91N21096
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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