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contributor authorJ. F. Muska
contributor authorM. Suo
contributor authorR. W. Fish
date accessioned2017-05-08T23:00:30Z
date available2017-05-08T23:00:30Z
date copyrightOctober, 1976
date issued1976
identifier issn1528-8919
identifier otherJETPEZ-26728#457_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88534
description abstractA method of superposition which predicts the cumulative effect of film cooling has been described in the literature by Sellers. This method predicts the magnitude and extent of film cooling downstream of multiple injection stations by accounting for the effectiveness level from each upstream station individually. Sellers compared the method with results from multiple slots and good agreement was demonstrated. Because of the simplicity of the method it was proposed as a method to predict the cumulative effect of film cooling from rows of holes. To substantiate this, experiments were conducted with film cooling schemes on flat plates and airfoils. The results of these experiments demonstrate that the method is satisfactory for design of film cooled airfoils in the required range of geometries and coolant flows.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Additive Nature of Film Cooling From Rows of Holes
typeJournal Paper
journal volume98
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3446214
journal fristpage457
journal lastpage463
identifier eissn0742-4795
keywordsCooling
keywordsAirfoils
keywordsFlow (Dynamics)
keywordsCoolants
keywordsDesign AND Flat plates
treeJournal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 004
contenttypeFulltext


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