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Using stability theory to analyse configurations of pulsed jets for flow control

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dc.contributor.author Skamnakis, D en
dc.contributor.author Papailiou, K en
dc.date.accessioned 2014-03-01T01:27:32Z
dc.date.available 2014-03-01T01:27:32Z
dc.date.issued 2007 en
dc.identifier.issn 1386-6184 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/18495
dc.subject Flow control en
dc.subject Pulsating jets en
dc.subject Stability analysis en
dc.subject Synthetic jets en
dc.subject.classification Thermodynamics en
dc.subject.classification Mechanics en
dc.subject.other Actuators en
dc.subject.other Flow control en
dc.subject.other Flow measurement en
dc.subject.other Optimization en
dc.subject.other Flow stability en
dc.subject.other Pulsating jets en
dc.subject.other Stability analysis en
dc.subject.other Synthetic jets en
dc.subject.other Jets en
dc.title Using stability theory to analyse configurations of pulsed jets for flow control en
heal.type journalArticle en
heal.identifier.primary 10.1007/s10494-007-9074-6 en
heal.identifier.secondary http://dx.doi.org/10.1007/s10494-007-9074-6 en
heal.language English en
heal.publicationDate 2007 en
heal.abstract During the last decade, efforts for simulating active flow control behavior by the use of pulsating jets have multiplied. In the present work, a URANS is used mostly for simulation, where the resulting flow characteristics can be reproduced with fair but adequate accuracy for engineering applications. This computational tool provides information concerning the effect on the flow, of the flow control. An additional computational tool is introduced, that of flow stability analysis, which allows to optimize the frequency and the position of the actuators (here pulsating jets). This tool will be developed through flow stability arguments. Both tools will be used within the context of the present paper and for reasons explained below, for suppressing only flow separation in internal flow cases. Once the computational tools are described/developed, they will be applied to a specific case. The optimization procedure will be demonstrated and discussed. © Springer Science+Business Media B.V. 2007. en
heal.publisher SPRINGER en
heal.journalName Flow, Turbulence and Combustion en
dc.identifier.doi 10.1007/s10494-007-9074-6 en
dc.identifier.isi ISI:000246563400012 en
dc.identifier.volume 78 en
dc.identifier.issue 3-4 en
dc.identifier.spage 445 en
dc.identifier.epage 463 en


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