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Using HPC in Gas Turbines blade fault diagnosis

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dc.contributor.author Stamatis, AG en
dc.contributor.author Papailiou, KD en
dc.date.accessioned 2014-03-01T01:13:29Z
dc.date.available 2014-03-01T01:13:29Z
dc.date.issued 1997 en
dc.identifier.issn 0302-9743 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/12506
dc.subject Coarse Grained en
dc.subject Fault Diagnosis en
dc.subject Fault Identification en
dc.subject Gas Turbine en
dc.subject Iteration Method en
dc.subject Real Time en
dc.subject.classification Computer Science, Theory & Methods en
dc.title Using HPC in Gas Turbines blade fault diagnosis en
heal.type journalArticle en
heal.identifier.primary 10.1007/BFb0031575 en
heal.identifier.secondary http://dx.doi.org/10.1007/BFb0031575 en
heal.language English en
heal.publicationDate 1997 en
heal.abstract Parallelization of two approaches used for identification of faults in blades of a gas turbine is presented. The first approach, termed as direct simulation, is aiming to populate a fault diagnosis database allowing early identification of faults. The second approach, termed as the inverse one, gives a more focused solution to fault identification, by using the direct approach in an iterative way which permits the estimation of the blade geometry alterations. By using state of the art parallel tools such as ScaLAPACK library and exploiting inherent coarse-grained parallelism in calculating the elements of the Jacobian needed in the iterative method encouraging speedups have been obtained. The test cases presented include theoretically produced fault signals as well as experimental cases, where actual measurement data are shown to produce in quasi real time the geometrical deformations which existed in the test engine. en
heal.publisher SPRINGER-VERLAG BERLIN en
heal.journalName HIGH-PERFORMANCE COMPUTING AND NETWORKING en
heal.bookName LECTURE NOTES IN COMPUTER SCIENCE en
dc.identifier.doi 10.1007/BFb0031575 en
dc.identifier.isi ISI:000074015300002 en
dc.identifier.volume 1225 en
dc.identifier.spage 11 en
dc.identifier.epage 20 en


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