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contributor authorR. C. Adkins
date accessioned2017-05-08T23:04:42Z
date available2017-05-08T23:04:42Z
date copyrightJuly, 1978
date issued1978
identifier issn1528-8919
identifier otherJETPEZ-26742#444_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/90977
description abstractA simple mathematical model has been devised which is intended to make a powerful aid to combustor design and development. The model has confirmed that nonuniform flow conditions at inlet to the precombustor diffuser can seriously deter combustor performance.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Effect of Compressor Exit Flow Distribution on Air Placement in Annular Combustors
typeJournal Paper
journal volume100
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3446377
journal fristpage444
journal lastpage451
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsCompressors
keywordsCombustion chambers
keywordsDiffusers AND Design
treeJournal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 003
contenttypeFulltext


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