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contributor authorK. Mahesh
contributor authorG. Constantinescu
contributor authorS. Apte
contributor authorG. Iaccarino
contributor authorF. Ham
contributor authorP. Moin
date accessioned2017-05-09T00:18:38Z
date available2017-05-09T00:18:38Z
date copyrightMay, 2006
date issued2006
identifier issn0021-8936
identifier otherJAMCAV-26599#374_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133042
description abstractLarge-eddy simulation (LES) has traditionally been restricted to fairly simple geometries. This paper discusses LES of reacting flows in geometries as complex as commercial gas turbine engine combustors. The incompressible algorithm developed by (J. Comput. Phys., 2004, 197, 215–240) is extended to the zero Mach number equations with heat release. Chemical reactions are modeled using the flamelet/progress variable approach of and (J. Fluid Mech., 2004, 504, 73–97). The simulations are validated against experiment for methane-air combustion in a coaxial geometry, and jet-A surrogate/air combustion in a gas-turbine combustor geometry.
publisherThe American Society of Mechanical Engineers (ASME)
titleLarge-Eddy Simulation of Reacting Turbulent Flows in Complex Geometries
typeJournal Paper
journal volume73
journal issue3
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.2179098
journal fristpage374
journal lastpage381
identifier eissn1528-9036
keywordsDensity
keywordsFlow (Dynamics)
keywordsTurbulence
keywordsCombustion chambers
keywordsEquations
keywordsGeometry
keywordsGas turbines
keywordsEddies (Fluid dynamics)
keywordsSimulation AND Algorithms
treeJournal of Applied Mechanics:;2006:;volume( 073 ):;issue: 003
contenttypeFulltext


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