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contributor authorW. E. Hill
contributor authorN. R. Dibelius
date accessioned2017-05-09T00:35:59Z
date available2017-05-09T00:35:59Z
date copyrightJuly, 1970
date issued1970
identifier issn1528-8919
identifier otherJETPEZ-26687#310_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142266
description abstractThe radiation heat load assumes an important role in gas turbine life and performance as firing temperatures and pressures are increased. This first phase of a program for assessing radiant heat loading was mainly concerned with devising measurement techniques. An experimental method for measuring the temperature of luminous flames with a two-color pyrometer and radiant intensity by means of a total radiation pyrometer is described. Emittance data from two combustion liner configurations is included for chamber pressures of from 2 to 7.5 atmospheres over the turbine inlet temperature range of 900 to 1950 deg F.
publisherThe American Society of Mechanical Engineers (ASME)
titleMeasurement of Flame Temperature and Emittance in Gas Turbine Combustors
typeJournal Paper
journal volume92
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3445355
journal fristpage310
journal lastpage314
identifier eissn0742-4795
keywordsTemperature
keywordsCombustion chambers
keywordsGas turbines
keywordsFlames
keywordsPyrometers
keywordsRadiation (Physics)
keywordsStress
keywordsCombustion
keywordsTurbines
keywordsFiring (materials)
keywordsRadiant heat AND Heat
treeJournal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003
contenttypeFulltext


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