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Hub wall rotation influence on high-speed compressor cascade performance

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dc.contributor.author Doukelis, A en
dc.contributor.author Mathioudakis, K en
dc.contributor.author Papailiou, K en
dc.date.accessioned 2014-03-01T01:16:37Z
dc.date.available 2014-03-01T01:16:37Z
dc.date.issued 2001 en
dc.identifier.issn 0748-4658 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/14125
dc.subject High Speed en
dc.subject.classification Engineering, Aerospace en
dc.subject.other Boundary layers en
dc.subject.other Energy transfer en
dc.subject.other Probes en
dc.subject.other Turbomachine blades en
dc.subject.other Viscous flow en
dc.subject.other Hub walls en
dc.subject.other Mach nubmer en
dc.subject.other Compressors en
dc.title Hub wall rotation influence on high-speed compressor cascade performance en
heal.type journalArticle en
heal.identifier.primary 10.2514/2.5823 en
heal.identifier.secondary http://dx.doi.org/10.2514/2.5823 en
heal.language English en
heal.publicationDate 2001 en
heal.abstract The influence of the magnitude of the relative wall speed on the performance of an annular compressor cascade with hub clearance is examined. Five-hole probe measurements, conducted at the inlet and outlet of the cascade, are used to derive blade performance characteristics, in the form of loss and turning distributions. Characteristics are presented in the form of circumferentially mass-averaged profiles, whereas distributions on the exit plane provide information useful to interpret the performance of the blading. Four different rotational speeds of the hub have been examined, giving the possibility to observe the dependence of performance characteristics on hub rotational speed. Increasing the rotational speed is found to improve the performance of the cascade by decreasing losses in the clearance region, while it affects the flow in the entire passage. en
heal.publisher AMER INST AERONAUT ASTRONAUT en
heal.journalName Journal of Propulsion and Power en
dc.identifier.doi 10.2514/2.5823 en
dc.identifier.isi ISI:000169952700020 en
dc.identifier.volume 17 en
dc.identifier.issue 4 en
dc.identifier.spage 902 en
dc.identifier.epage 908 en


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