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contributor authorP. J. Loftus
contributor authorT. V. Jones
date accessioned2017-05-08T23:15:29Z
date available2017-05-08T23:15:29Z
date copyrightJuly, 1983
date issued1983
identifier issn1528-8919
identifier otherJETPEZ-26783#615_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97075
description abstractFilm cooling experiments have been conducted at conditions which realistically simulate the gas turbine environment. Heat transfer has been measured using a short duration wind tunnel. Mainstream injection and wall temperatures have been varied independently in order to conduct a systematic investigation of the injection process. A model of the film cooling process based on the principle of superposition is used to interpret the experimental results. The effect of gas to wall temperature ratio on heat transfer to an uncooled plate has also been investigated.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Effect of Temperature Ratios on the Film Cooling Process
typeJournal Paper
journal volume105
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3227461
journal fristpage615
journal lastpage620
identifier eissn0742-4795
keywordsTemperature
keywordsCooling
keywordsHeat transfer
keywordsWall temperature
keywordsWind tunnels AND Gas turbines
treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 003
contenttypeFulltext


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