Spatially Resolved Compressor Characteristics for Modeling and Control of Blade-Scale Flow Instabilities

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dc.contributor.authorAdomaitis, Raymond A.en_US
dc.contributor.departmentISRen_US
dc.date.accessioned2007-05-23T09:59:01Z
dc.date.available2007-05-23T09:59:01Z
dc.date.issued1995en_US
dc.description.abstractA numerical techniques cable of simulating blade-scale compression system flow instabilities over times scales spanning tens of rotor revolutions is presented. Simulations of stall inception, growth to fully-developed rotating stall, and evidence for hysteresis, secondary instabilities, and other nonlinear phenomena are presented. signal processing techniques for flow asymmetry characterization are discussed in the context of obtaining low-order representations of the flow disturbances with the ultimate goal of active stall suppression.en_US
dc.format.extent560168 bytes
dc.format.mimetypeapplication/pdf
dc.identifier.urihttp://hdl.handle.net/1903/5632
dc.language.isoen_USen_US
dc.relation.ispartofseriesISR; TR 1995-44en_US
dc.subjectaircraften_US
dc.subjectdistributed parameter systemsen_US
dc.subjectnonlinear systemsen_US
dc.subjectcomputational fluid dynamics en_US
dc.subjectAxial compressorsen_US
dc.subjectIntelligent Control Systemsen_US
dc.titleSpatially Resolved Compressor Characteristics for Modeling and Control of Blade-Scale Flow Instabilitiesen_US
dc.typeTechnical Reporten_US

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