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Bifurcation Analysis of Surge and Rotating Stall in Axial Flow Compressors

dc.contributor.authorAbed, Eyad H.en_US
dc.contributor.authorHoupt, Paul K.en_US
dc.contributor.authorHosny, Wishaa M.en_US
dc.date.accessioned2007-05-23T09:45:26Z
dc.date.available2007-05-23T09:45:26Z
dc.date.issued1990en_US
dc.identifier.urihttp://hdl.handle.net/1903/4977
dc.description.abstractIn this paper, the surge and rotating stall post instability behaviors of anial flow compressors are investigated from a bifurcation-theoretic perspective. A sequence of local and global bifurcations of the nonlinear system dynamics is uncovered. This includes a previously unknown global bifurcation of a pair of large amplitude periodic solutions. Resulting from this bifurcation are a stable oscillation ("surge") and an unstable oscillation ("antisurge"). The latter oscillation is found to have a deciding significance regarding post-instability behavior experienced by the compressor. These results are used to reconstruct Greitzer's (1976) findings regarding the manner in which post-instability behavior depends on system parameters. Moreover, the results provide significant new insight deemed valuable in the prediction, analysis and control of stall instabilities in gas turbine jet engines.en_US
dc.format.extent919841 bytes
dc.format.mimetypeapplication/pdf
dc.language.isoen_USen_US
dc.relation.ispartofseriesISR; TR 1990-27en_US
dc.subjectIntelligent Servomechanismsen_US
dc.titleBifurcation Analysis of Surge and Rotating Stall in Axial Flow Compressorsen_US
dc.typeTechnical Reporten_US
dc.contributor.departmentISRen_US


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