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contributor authorElizaveta M. Ivanova
contributor authorBerthold E. Noll
contributor authorManfred Aigner
date accessioned2017-05-09T00:43:48Z
date available2017-05-09T00:43:48Z
date copyrightFebruary, 2011
date issued2011
identifier issn1528-8919
identifier otherJETPEZ-27155#021505_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/146086
description abstractThis paper presents numerical simulations of turbulent mixing of a jet in crossflow. The test case is chosen to resemble scalar mixing processes in the premixing zones of gas turbine combustion chambers. Steady and unsteady simulations employing three different computational approaches are presented: steady Reynolds-averaged Navier–Stokes, unsteady Reynolds-averaged Navier–Stokes, and scale-adaptive simulations. Presented results comprise the (time-averaged) profiles of flow velocities, turbulent kinetic energy of the flow, Reynolds stresses, passive scalar distribution, turbulent scalar fluxes, and the turbulent variance of the passive scalar. All presented results are directly validated against experimental data. Additionally, two parameter studies are presented. Both studies are related to the accuracy of the turbulent scalar mixing predictions for all used simulation methods. In the first study, the dependence of the scalar mixing predictions on the value of the turbulent Schmidt number is considered. In the second study, the dependence of the predicted turbulent scalar variance on the used modeling approach is analyzed.
publisherThe American Society of Mechanical Engineers (ASME)
titleComputational Modeling of Turbulent Mixing of a Transverse Jet
typeJournal Paper
journal volume133
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4002015
journal fristpage21505
identifier eissn0742-4795
keywordsScalars
keywordsTurbulence
keywordsEngineering simulation
keywordsFlow (Dynamics)
keywordsReynolds-averaged Navier–Stokes equations
keywordsComputer simulation AND Kinetic energy
treeJournal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 002
contenttypeFulltext


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