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contributor authorMoses, Clifford
date accessioned2017-05-09T00:58:37Z
date available2017-05-09T00:58:37Z
date issued2013
identifier issn1528-8919
identifier othergtp_135_12_121503.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151730
description abstractAn increasing demand is being put on the fuel as a heat sink in modern aircraft. In the end, the fuel flows through the atomizer, which is both the hottest part in the thermal history of the fuel and the most critical for resisting deposition. Most studies have concentrated on the chemistry of deposition and in recent years there have been modeling efforts. Deposition is really the end product of a coupling between heat transfer to the fuel, chemical reactions to form insoluble gums, followed by the transport of these gums to the surface to form deposits. There is conflicting evidence and theory in the literature concerning the effect of turbulence on deposition, i.e., whether deposition increases or decreases with increasing Reynolds number. This paper demonstrates, through a heat transfer analysis, that the effect of the Reynolds number depends upon the boundary/initial conditions. If the flow is heated from the surface, deposition decreases with increasing Reynolds number; however, for isothermal flows, i.e., preheated, deposition can increase with the Reynolds number.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffect of Reynolds Number on Deposition in Fuels Flowing Over Heated Surfaces
typeJournal Paper
journal volume135
journal issue12
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4025147
journal fristpage121503
journal lastpage121503
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 012
contenttypeFulltext


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