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contributor authorWilliam J. Kelnhofer
contributor authorCharles T. Derick
date accessioned2017-05-09T00:57:41Z
date available2017-05-09T00:57:41Z
date copyrightJanuary, 1971
date issued1971
identifier issn1528-8919
identifier otherJETPEZ-26690#57_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151423
description abstractStraight-walled diffuser-tailpipe systems with fully developed inlet conditions as encountered with gas turbine exhaust ducting systems have been tested. For constant length diffusers with varying tailpipe lengths, an increase in recovery and a slight increase in area ratio occurs at maximum performance condition. Test conditions included ratios of diffuser wall length to diffuser inlet width from 5.33 to 15.33. Maximum ratio of tailpipe length to diffuser inlet width was 10.47.
publisherThe American Society of Mechanical Engineers (ASME)
titleTailpipe Effects on Gas Turbine Diffuser Performance With Fully Developed Inlet Conditions
typeJournal Paper
journal volume93
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3445403
journal fristpage57
journal lastpage61
identifier eissn0742-4795
keywordsDiffusers
keywordsGas turbines AND Exhaust systems
treeJournal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 001
contenttypeFulltext


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