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Numerical simulation of blade fault signatures from unsteady wall pressure signals

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dc.contributor.author Dedoussis, V en
dc.contributor.author Mathioudakis, K en
dc.contributor.author Papailiou, KD en
dc.date.accessioned 2014-03-01T01:13:13Z
dc.date.available 2014-03-01T01:13:13Z
dc.date.issued 1997 en
dc.identifier.issn 0742-4795 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/12370
dc.subject Numerical Simulation en
dc.subject.classification Engineering, Mechanical en
dc.title Numerical simulation of blade fault signatures from unsteady wall pressure signals en
heal.type journalArticle en
heal.identifier.primary 10.1115/1.2815583 en
heal.identifier.secondary http://dx.doi.org/10.1115/1.2815583 en
heal.language English en
heal.publicationDate 1997 en
heal.abstract A method for establishing signatures of faults in the rotating blades of a gas turbine compressor is presented. The method employs a panel technique for the calculation of the flow field around blade cascades, with disrupted periodicity, a situation encountered when a blade fault has occurred. From this calculation, time signals of the pressure at a location on the casing wall, facing the rotating blades, are constituted. Processing these signals, in combination with ""healthy"" pressure signals, allows the constitution of fault signatures. The proposed method employs geometric data, as well as data about the operating point of the engine. It gives the possibility of establishing the fault signatures without the need of performing experiments with implanted faults. The successful application of the method is demonstrated by comparison of signatures obtained by simulation to signatures derived from experiments with implanted blade faults, in an industrial gas turbine. en
heal.publisher ASME-AMER SOC MECHANICAL ENG en
heal.journalName Journal of Engineering for Gas Turbines and Power en
dc.identifier.doi 10.1115/1.2815583 en
dc.identifier.isi ISI:A1997WW75100014 en
dc.identifier.volume 119 en
dc.identifier.issue 2 en
dc.identifier.spage 362 en
dc.identifier.epage 368 en


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