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contributor authorG. W. Jumper
contributor authorR. B. Rivir
contributor authorW. C. Elrod
date accessioned2017-05-08T23:36:57Z
date available2017-05-08T23:36:57Z
date copyrightJuly, 1991
date issued1991
identifier issn0889-504X
identifier otherJOTUEI-28613#479_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109393
description abstractThe mechanisms influencing film cooling effectiveness on a flat plate in high free-stream turbulence using a single row of 30 deg slant-hole injectors are examined. The primary area of focus is the area within 40 diameters downstream of injection. Of interest are blowing ratios for optimum film cooling effectiveness within 10 diameters downstream of injection, and the decay of film cooling effectiveness down the plate. Film cooling flow Reynolds numbers. Re, from 24,700 to 86,600 and free-stream turbulence intensities from 14 to 17 percent were examined. Changes in Reynolds number or free-stream turbulence broadened and increased the blowing ratios for optimum film cooling effectiveness. In comparison with tests conducted at 0.5 percent free-stream turbulence, higher free-stream turbulence causes a faster decay in film cooling effectiveness, or a reduction in the effective cooling length, and a reduction of the level of cooling effectiveness at the higher Reynolds numbers.
publisherThe American Society of Mechanical Engineers (ASME)
titleFilm Cooling Effectiveness in High-Turbulence Flow
typeJournal Paper
journal volume113
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2927899
journal fristpage479
journal lastpage483
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsCooling
keywordsTurbulence
keywordsReynolds number
keywordsEjectors
keywordsFlat plates AND Mechanisms
treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 003
contenttypeFulltext


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