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Investigation on the effects of an improved blade section pressure distributions on turbine blade tip region losses

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Investigation on the effects of an improved blade section pressure distributions on turbine blade tip region losses

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dc.contributor.author Xiang, Xiaorong
dc.contributor.author Zhao, Qingjun
dc.contributor.author Xu, Jianzhong
dc.contributor.author Zhao, Wei en_US
dc.contributor.other International Society for Air Breathing Engines
dc.date.accessioned 2015-10-22T15:51:02Z
dc.date.available 2015-10-22T15:51:02Z
dc.date.created 2015 en_US
dc.date.issued 2015-10-22
dc.identifier 20066 en_US
dc.identifier.uri http://hdl.handle.net/2374.UC/745675
dc.description This paper is part of the conference proceedings from the 22nd International Symposium on Air Breathing Engines. en_US
dc.relation.ispartof ISABE 2015 (Awatef Hamed, Faculty Work and Research, College of Engineering and Applied Science) en_US
dc.rights Attribution-NonCommercial-NoDerivs 3.0 United States en_US
dc.rights.uri http://creativecommons.org/licenses/by-nc-nd/3.0/us/ en_US
dc.subject Compressors axial and centripetal turbines: Axial and other turbines en_US
dc.subject.lcsh Airplanes -- Motors en_US
dc.subject.lcsh Airplanes -- Jet propulsion en_US
dc.subject.lcsh Aircraft gas-turbines en_US
dc.title Investigation on the effects of an improved blade section pressure distributions on turbine blade tip region losses en_US


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Attribution-NonCommercial-NoDerivs 3.0 United States Except where otherwise noted, this item's license is described as Attribution-NonCommercial-NoDerivs 3.0 United States

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