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contributor authorSirakov, Borislav
contributor authorCasey, Michael
date accessioned2017-05-09T01:03:30Z
date available2017-05-09T01:03:30Z
date issued2013
identifier issn0889-504X
identifier otherturb_135_2_021011.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153420
description abstractTest data on several small turbochargers with different levels of heat transfer from the turbine to the compressor have been obtained through cooling of the turbocharger center housing and by testing in hot and cold test stands. This data identifies the strong effect of the heat transfer on the apparent efficiency of the compressor and turbine, particularly at low speeds and low mass flows. A simplified theory is used to explain the apparent effect of the heat transfer on the work input and efficiency. The results confirm that conventional performance maps underestimate the efficiency of the compressor stage and overestimate the efficiency of the turbine by as much as 20% points at low speeds. A correction procedure for this effect is defined which converts performance maps obtained with heat transfer to performance maps for adiabatic conditions (for both compressor and turbine) without any prior knowledge or measurement of the heat transfer. The practical significance of the results with regard to turbocharger performance and the relevance to a broader class of turbomachines is discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleEvaluation of Heat Transfer Effects on Turbocharger Performance
typeJournal Paper
journal volume135
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4006608
journal fristpage21011
journal lastpage21011
identifier eissn1528-8900
treeJournal of Turbomachinery:;2013:;volume( 135 ):;issue: 002
contenttypeFulltext


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