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contributor authorJing Shi
contributor authorShiying Zhou
contributor authorYaoko Zhang
contributor authorMengyu She
contributor authorMingfu Zhu
contributor authorJianyuan Han
date accessioned2017-05-08T23:22:26Z
date available2017-05-08T23:22:26Z
date copyrightApril, 1986
date issued1986
identifier issn1528-8919
identifier otherJETPEZ-26634#265_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101120
description abstractAn investigation was made to compare the performance of a highly loaded transonic turbine stage with and without compound leaned vanes. In both cases, velocity distribution along the vane surfaces was calculated from a full three-dimensional time-marching finite volume method. Nozzles were tested in a wind tunnel. Through rig tests, velocity profile at the stage exit was measured and the stage overall performance obtained. Performance in both tip and hub regions was improved by using the compound leaned vanes so that the stage efficiency increased by approximately 1 percent. The improvement is particularly remarkable at off-design points.
publisherThe American Society of Mechanical Engineers (ASME)
titleAn Investigation of a Highly Loaded Transonic Turbine Stage With Compound Leaned Vanes
typeJournal Paper
journal volume108
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3239898
journal fristpage265
journal lastpage269
identifier eissn0742-4795
keywordsTurbines
keywordsFinite volume methods
keywordsWind tunnels
keywordsDesign AND Nozzles
treeJournal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 002
contenttypeFulltext


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