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contributor authorDavid R. Buttsworth
contributor authorAbdalla Agrira
contributor authorRay Malpress
contributor authorTalal Yusaf
date accessioned2017-05-09T00:43:49Z
date available2017-05-09T00:43:49Z
date copyrightFebruary, 2011
date issued2011
identifier issn1528-8919
identifier otherJETPEZ-27155#022802_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/146099
description abstractSimulation of internal combustion engine heat transfer using low-dimensional thermodynamic modeling often relies on quasisteady heat transfer correlations. However, unsteady thermal boundary layer modeling could make a useful contribution because of the inherent unsteadiness of the internal combustion engine environment. Previous formulations of the unsteady energy equations for internal combustion engine thermal boundary layer modeling appear to imply that it is necessary to adopt the restrictive assumption that isentropic processes occur in the gas external to the thermal boundary layer. Such restrictions are not required and we have investigated if unsteady modeling can improve the simulation of crank-resolved heat transfer. A modest degree of success is reported for the present modeling, which relies on a constant effective turbulent thermal conductivity. Improvement in the unsteady thermal boundary layer simulations is expected in the future when the temporal and spatial variations in effective turbulent conductivity are correctly modeled.
publisherThe American Society of Mechanical Engineers (ASME)
titleSimulation of Instantaneous Heat Transfer in Spark Ignition Internal Combustion Engines: Unsteady Thermal Boundary Layer Modeling
typeJournal Paper
journal volume133
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4001080
journal fristpage22802
identifier eissn0742-4795
keywordsHeat transfer
keywordsEngines
keywordsSimulation
keywordsInternal combustion engines
keywordsModeling
keywordsEquations
keywordsHeat flux
keywordsThermal boundary layers AND Pressure
treeJournal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 002
contenttypeFulltext


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