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Improving turbine performance by use of simple computational means

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dc.contributor.author Sieros, G en
dc.contributor.author Papailiou, KD en
dc.contributor.author Kundera, R en
dc.date.accessioned 2014-03-01T02:49:24Z
dc.date.available 2014-03-01T02:49:24Z
dc.date.issued 2003 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/34585
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-0345760008&partnerID=40&md5=afef9045c148d5856327607a48eff53a en
dc.subject.other Aspect ratio en
dc.subject.other Compressors en
dc.subject.other Computational methods en
dc.subject.other Correlation methods en
dc.subject.other Nozzles en
dc.subject.other Optimization en
dc.subject.other Recuperators en
dc.subject.other Rotors en
dc.subject.other Stators en
dc.subject.other Thickness measurement en
dc.subject.other Turbogenerators en
dc.subject.other Turbomachine blades en
dc.subject.other Flow separation en
dc.subject.other Thermal efficiency en
dc.subject.other Gas turbines en
dc.title Improving turbine performance by use of simple computational means en
heal.type conferenceItem en
heal.publicationDate 2003 en
heal.abstract A design effort was undertaken to improve the efficiency of the turbine that is used in a turbo-generator unit. Based on an existing design, an improved two-stage axial turbine was designed and tested. The design procedure and guidelines are described. For this redesign effort simple computational tools were used. The resulting turbine was manufactured and tested at PBS. Results from the tests and a comparison with the existing turbine are given. en
heal.journalName Proceedings of the 2003 International Joint Power Generation Conference en
dc.identifier.spage 185 en
dc.identifier.epage 193 en


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