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

Simple item page
dc.contributor.authorXiang, Xiaorong
dc.contributor.authorZhao, Qingjun
dc.contributor.authorXu, Jianzhong
dc.contributor.authorZhao, Weien_US
dc.contributor.otherInternational Society for Air Breathing Engines
dc.date.accessioned2015-10-22T15:51:02Z
dc.date.available2015-10-22T15:51:02Z
dc.date.created2015en_US
dc.date.issued2015-10-22
dc.descriptionThis paper is part of the conference proceedings from the 22nd International Symposium on Air Breathing Engines.en_US
dc.identifier20066en_US
dc.identifier.urihttp://hdl.handle.net/2374.UC/745675
dc.relation.ispartofISABE 2015 (Awatef Hamed, Faculty Work and Research, College of Engineering and Applied Science)en_US
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 United Statesen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/us/en_US
dc.subjectCompressors axial and centripetal turbines: Axial and other turbinesen_US
dc.subject.lcshAirplanes -- Motorsen_US
dc.subject.lcshAirplanes -- Jet propulsionen_US
dc.subject.lcshAircraft gas-turbinesen_US
dc.titleInvestigation on the effects of an improved blade section pressure distributions on turbine blade tip region lossesen_US
Files
Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
ISABE2015_CS&A_Wei Zhao_47_MANUSCRIPT_20066.pdf
Size:
1007.06 KB
Format:
Adobe Portable Document Format
Description:
Download
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
557-CopyrightInfo-copyright.tiff
Size:
1.96 MB
Format:
Tag Image File Format
Description:
Download
Collections
ISABE 2015