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Nonlinear Dynamics of Axial Flow Compressors: A Parametric Study

dc.contributor.authorLiaw, Der-Cherngen_US
dc.contributor.authorAdomaitis, Raymond A.en_US
dc.contributor.authorAbed, Eyad H.en_US
dc.date.accessioned2007-05-23T09:47:43Z
dc.date.available2007-05-23T09:47:43Z
dc.date.issued1991en_US
dc.identifier.urihttp://hdl.handle.net/1903/5080
dc.description.abstractThis paper presents the analysis of the dynamics of a representative axial flow compressor model, emphasizing the influence of two important control parameters. These are a nondimensional parameter B (previously introduced by Greitzer (1976) as a primary determinant of post-stall behavior) and the setting of the throttle line. Greitzer's lumped-parameter model is employed in this study, with a specific choice of compressor and throttle characteristics. Our analysis shows the presence of a rich variety of global as well as local bifurcations as the two control parameters are varied. The analysis leads to a characterization of compressor operation into three major zones: the stalled zone, the pre-stall zone, and the normal (unstalled) zone. Simulation results demonstrate the qualitatively different dynamical behaviors within each regime of parameter space.en_US
dc.format.extent641784 bytes
dc.format.mimetypeapplication/pdf
dc.language.isoen_USen_US
dc.relation.ispartofseriesISR; TR 1991-32en_US
dc.subjectaircraften_US
dc.subjectnonlinear systemsen_US
dc.subjectrobust controlen_US
dc.subjectstabilityen_US
dc.subjectIntelligent Servomechanismsen_US
dc.titleNonlinear Dynamics of Axial Flow Compressors: A Parametric Studyen_US
dc.typeTechnical Reporten_US
dc.contributor.departmentISRen_US


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