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contributor authorR. J. Goldstein
contributor authorP. Jin
contributor authorR. L. Olson
date accessioned2017-05-09T00:01:17Z
date available2017-05-09T00:01:17Z
date copyrightApril, 1999
date issued1999
identifier issn0889-504X
identifier otherJOTUEI-28669#225_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123030
description abstractA special naphthalene sublimation technique is used to study the film cooling performance downstream of one row of holes of 35 deg inclination angle with 3d hole spacing and relatively small hole length to diameter ratio (L/d = 6.3). Both film cooling effectiveness and mass/heat transfer coefficient are determined for blowing rates from 0.5 to 2.0 with density ratio of 1.0. The mass transfer coefficient is measured using pure air film injection, while the film cooling effectiveness is derived from comparison of mass transfer coefficients obtained following injection of naphthalene-vapor-saturated air with those from pure air injection. This technique enables one to obtain detailed local information on film cooling performance. The laterally averaged and local film cooling effectiveness agree with previous experiments. The difference between mass/heat transfer coefficients and previous heat transfer results indicates that conduction error may play an important role in the earlier heat transfer measurements.
publisherThe American Society of Mechanical Engineers (ASME)
titleFilm Cooling Effectiveness and Mass/Heat Transfer Coefficient Downstream of One Row of Discrete Holes
typeJournal Paper
journal volume121
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2841305
journal fristpage225
journal lastpage232
identifier eissn1528-8900
keywordsCooling
keywordsHeat transfer coefficients
keywordsMass transfer
keywordsHeat transfer
keywordsDensity
keywordsVapors
keywordsMeasurement
keywordsHeat conduction AND Errors
treeJournal of Turbomachinery:;1999:;volume( 121 ):;issue: 002
contenttypeFulltext


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