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contributor authorC. Gau
contributor authorW. B. Hwang
date accessioned2017-05-08T23:34:04Z
date available2017-05-08T23:34:04Z
date copyrightOctober, 1990
date issued1990
identifier issn0889-504X
identifier otherJOTUEI-28606#786_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107706
description abstractExperiments have been performed in a large circular pipe to study and obtain the film cooling effectivenesses with the presence of weak swirling flow in the mainstream. The swirling flow is generated by a flat vane swirler situated upstream. Cooling film is injected from an annular slot formed by the pipe wall and the circular cover plate. The radial temperature distribution measurements at several axial locations were used to infer the rate of mixing of film jet with swirling flow. The swirl number, which increases with turbulence intensity and swirl velocity in the mainstream, can significantly increase the mixing rate of film jet with swirl flow and decrease the film cooling effectiveness. During the course of the experiments, the blowing ratio ranged from 0.5 to 1.75 and the swirl number ranged from 0 to 0.6. Correlation equations for the film cooling effectiveness, which account for the effect of swirling flow, are obtained.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffect of Weak Swirling Flow on Film Cooling Performance
typeJournal Paper
journal volume112
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2927722
journal fristpage786
journal lastpage791
identifier eissn1528-8900
keywordsCooling
keywordsSwirling flow
keywordsPipes
keywordsEquations
keywordsMeasurement
keywordsTurbulence
keywordsTemperature distribution AND Flow (Dynamics)
treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 004
contenttypeFulltext


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