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contributor authorT. Verstraete
contributor authorZ. Alsalihi
contributor authorR. A. Van den Braembussche
date accessioned2017-05-09T00:26:06Z
date available2017-05-09T00:26:06Z
date copyrightOctober, 2007
date issued2007
identifier issn0889-504X
identifier otherJOTUEI-28742#835_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137002
description abstractThis paper presents a numerical investigation of the heat transfer inside a micro gas turbine and its impact on the performance. The large temperature difference between turbine and compressor in combination with the small dimensions results in a high heat transfer causing a drop in efficiency of both components. Present study aims to quantify this heat transfer and to reveal the different mechanisms that contribute to it. A conjugate heat transfer solver has been developed for this purpose. It combines a three-dimensional (3D) conduction calculation inside the rotor and the stator with a 3D flow calculation in the radial compressor, turbine and gap between stator and rotor. The results for micro gas turbines of different size and shape and different material characteristics are presented and the impact on performance is evaluated.
publisherThe American Society of Mechanical Engineers (ASME)
titleNumerical Study of the Heat Transfer in Micro Gas Turbines
typeJournal Paper
journal volume129
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2720874
journal fristpage835
journal lastpage841
identifier eissn1528-8900
treeJournal of Turbomachinery:;2007:;volume( 129 ):;issue: 004
contenttypeFulltext


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