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contributor authorM. E. Crawford
contributor authorW. M. Kays
contributor authorR. J. Moffat
date accessioned2017-05-08T23:08:35Z
date available2017-05-08T23:08:35Z
date copyrightOctober, 1980
date issued1980
identifier issn1528-8919
identifier otherJETPEZ-26762#1006_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93208
description abstractExperimental research into heat transfer from full-coverage film-cooled surfaces with three injection geometries was described in Part I. This part has two objectives. The first is to present a simple numerical procedure for simulation of heat transfer with full-coverage film cooling. The second objective is to present some of the Stanton number data that was used in Part I of the paper. The data chosen for presentation are the low-Reynolds number, heated-starting-length data for the three injection geometries with five-diameter hole spacing. Sample data sets with high blowing ratio and with ten-diameter hole spacing are also presented. The numerical procedure has been successfully applied to the Stanton number data sets.
publisherThe American Society of Mechanical Engineers (ASME)
titleFull-Coverage Film Cooling—Part II: Heat Transfer Data and Numerical Simulation
typeJournal Paper
journal volume102
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3230335
journal fristpage1006
journal lastpage1012
identifier eissn0742-4795
keywordsHeat transfer
keywordsCooling
keywordsComputer simulation AND Simulation
treeJournal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 004
contenttypeFulltext


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