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contributor authorH. D. Ammari
contributor authorN. Hay
contributor authorD. Lampard
date accessioned2017-05-08T23:36:56Z
date available2017-05-08T23:36:56Z
date copyrightJuly, 1991
date issued1991
identifier issn0889-504X
identifier otherJOTUEI-28613#464_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109389
description abstractResults are presented of an experimental investigation into the influence of mainstream acceleration on the heat transfer coefficient downstream of injection through a row of 35 deg holes in a flat plate. A mass transfer analogue technique was used, with two uniform acceleration parameters, K ( = v(du∞ /dx)/u2 ∞ , of 1.9 × 10−6 and 5.0×10−6 in addition to the zero acceleration baseline case. Two injectants, air and carbon dioxide, were employed to give coolant-to-mainstream density ratios of 1.0 and 1.52, respectively. The blowing rate varied from 0.5 to 2.0. The heat transfer coefficient beneath the film decreased progressively as the acceleration increased, with maximum reductions from the zero acceleration datum case of about 27 percent. In the presence of acceleration, the heat transfer coefficient at a given blowing rate was dependent on the density ratio, an increase in the density ratio leading to a decrease in the heat transfer coefficient. An empirical correlation of the data over most of the range of densities and blowing rates of the experiments has been developed.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffect of Acceleration on the Heat Transfer Coefficient on a Film-Cooled Surface
typeJournal Paper
journal volume113
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2927897
journal fristpage464
journal lastpage471
identifier eissn1528-8900
keywordsHeat transfer coefficients
keywordsDensity
keywordsMass transfer
keywordsCoolants
keywordsCarbon dioxide AND Flat plates
treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 003
contenttypeFulltext


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