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contributor authorR. W. Foster-Pegg
date accessioned2017-05-08T23:20:40Z
date available2017-05-08T23:20:40Z
date copyrightJanuary, 1964
date issued1964
identifier issn1528-8919
identifier otherJETPEZ-26632#50_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/100101
description abstractThe generally used boiler efficiency concept is not convenient when combustion air is not varied in direct proportion to fuel. This situation may arise, for example, if combustion is being performed in gases exhausted by a gas turbine and the flow of these gases is determined by the requirement to carry a definite load on the gas turbine. This paper outlines a method of calculation alternative to the normal boiler efficiency method whereby the heat content in effluent gases from a combustion process such as stack gases may be divided into losses associated with the combustion air and a loss proportional to fuel. Some heat-balance calculations of a hypothetical cycle are included in an Appendix to demonstrate use of the method.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Procedure for Solution of Gas-Turbine and Other Combustion Heat-Balance Problems With Predetermined Airflow
typeJournal Paper
journal volume86
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3675415
journal fristpage50
journal lastpage56
identifier eissn0742-4795
keywordsHeat
keywordsCombustion
keywordsAir flow
keywordsGas turbines
keywordsGases
keywordsFuels
keywordsBoilers
keywordsFlow (Dynamics)
keywordsStress AND Cycles
treeJournal of Engineering for Gas Turbines and Power:;1964:;volume( 086 ):;issue: 001
contenttypeFulltext


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