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contributor authorA. Kohli
contributor authorD. G. Bogard
date accessioned2017-05-08T23:58:15Z
date available2017-05-08T23:58:15Z
date copyrightJanuary, 1998
date issued1998
identifier issn0889-504X
identifier otherJOTUEI-28664#86_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/121357
description abstractThe film cooling flow field is the result of a highly complex interaction between the film cooling jets and the mainstream. Understanding this interaction is important in order to explain the physical mechanisms involved in the rapid decrease of effectiveness, which occurs close to the hole exit. Not surprisingly, it is this region that is not modeled satisfactorily with current film cooling models. This study uses a high-frequency-response temperature sensor, which provides new information about the film cooling flow in terms of actual turbulence levels and probability density functions of the thermal field. Mean and rms temperature results are presented for 35 deg round holes at a momentum flux ratio of I = 0.16, at a density ratio of DR = 1.05. Probability density functions of the temperature indicate penetration of the mainstream into the coolant core, and ejection of coolant into the mainstream. Extreme excursions in the fluctuating temperature measurements suggest existence of strong intermittent flow structures responsible for dilution and dispersion of the coolant jets.
publisherThe American Society of Mechanical Engineers (ASME)
titleFluctuating Thermal Field in the Near-Hole Region for Film Cooling Flows
typeJournal Paper
journal volume120
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2841393
journal fristpage86
journal lastpage91
identifier eissn1528-8900
treeJournal of Turbomachinery:;1998:;volume( 120 ):;issue: 001
contenttypeFulltext


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