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contributor authorSean Jenkins
contributor authorKrishnakumar Varadarajan
contributor authorDavid G. Bogard
date accessioned2017-05-09T00:14:43Z
date available2017-05-09T00:14:43Z
date copyrightJanuary, 2004
date issued2004
identifier issn0889-504X
identifier otherJOTUEI-28708#203_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131019
description abstractThis paper presents the combined effects of high turbulence and film cooling on the dispersion of a simulated hot streak as it passes over a scaled-up nozzle guide vane. Experimental data demonstrates a considerable decay in the strength of a hot streak due to turbulence effects alone. Film cooling further reduces the peak temperature values resulting in a reduction of the peak temperature in the hot streak on the order of 75% relative to the upstream peak temperature in the hot streak. Comparisons are made between high turbulence (Tu=20%) and moderate turbulence (Tu=3.5%) as well as between different blowing conditions for the suction side, showerhead, and pressure side film cooling holes on a simulated nozzle guide vane.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Effects of High Mainstream Turbulence and Turbine Vane Film Cooling on the Dispersion of a Simulated Hot Streak
typeJournal Paper
journal volume126
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1643911
journal fristpage203
journal lastpage211
identifier eissn1528-8900
keywordsTemperature
keywordsCooling
keywordsTurbulence
keywordsSuction
keywordsPressure
keywordsTurbines
keywordsCoolants AND Flow (Dynamics)
treeJournal of Turbomachinery:;2004:;volume( 126 ):;issue: 001
contenttypeFulltext


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