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contributor authorDieter Bohn
contributor authorTom Heuer
contributor authorKarsten Kusterer
date accessioned2017-05-09T00:16:09Z
date available2017-05-09T00:16:09Z
date copyrightJuly, 2005
date issued2005
identifier issn1528-8919
identifier otherJETPEZ-26871#663_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131781
description abstractIn this paper a three-dimensional conjugate calculation has been performed for a passenger car turbo charger. The scope of this work is to investigate the heat fluxes in the radial compressor, which can be strongly influenced by the hot turbine. As a result of this, the compressor efficiency may deteriorate. Consequently, the heat fluxes have to be taken into account for the determination of the efficiency. To overcome this problem a complex three-dimensional model has been developed. It contains the compressor, the oil cooled center housing, and the turbine. Twelve operating points have been numerically simulated composed of three different turbine inlet temperatures and four different mass flows. The boundary conditions for the flow and for the outer casing were derived from experimental test data (Bohn et al.). Resulting from these conjugate calculations various one-dimensional calculation specifications have been developed. They describe the heat transfer phenomena inside the compressor with the help of a Nusselt number, which is a function of an artificial Reynolds number and the turbine inlet temperature.
publisherThe American Society of Mechanical Engineers (ASME)
titleConjugate Flow and Heat Transfer Investigation of a Turbo Charger
typeJournal Paper
journal volume127
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1839919
journal fristpage663
journal lastpage669
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsHeat
keywordsTemperature
keywordsHeat transfer
keywordsFluids
keywordsCompressors
keywordsFlux (Metallurgy)
keywordsTurbines
keywordsBoundary-value problems AND Reynolds number
treeJournal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 003
contenttypeFulltext


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