No AccessEvaluation of PSE as a Model for Supersonic Jet Using Transfer FunctionsVitor G. Kleine, Kenzo Sasaki, André V. Cavalieri, Guillaume A. Brès and Tim ColoniusVitor G. KleineTechnological Institute of Aeronautics (ITA)Search for more papers by this author, Kenzo SasakiTechnological Institute of Aeronautics (ITA)Search for more papers by this author, André V. CavalieriTechnological Institute of Aeronautics (ITA)Search for more papers by this author, Guillaume A. BrèsCascade Technologies, Inc.Search for more papers by this author and Tim ColoniusCalifornia Institute of TechnologySearch for more papers by this authorAIAA 2017-4194Session: Jet Noise XI: AnalysisPublished Online:2 Jun 2017https://doi.org/10.2514/6.2017-4194SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byWavepacket modelling of broadband shock-associated noise in supersonic jets5 May 2021 | Journal of Fluid Mechanics, Vol. 918A Parabolised Stability Equation based Broadband Shock-Associated Noise ModelMarcus H. Wong, Daniel M. Edgington-Mitchell, Damon Honnery, André V. Cavalieri and Peter Jordan18 May 2019 What's Popular 23rd AIAA/CEAS Aeroacoustics Conference 5-9 June 2017Denver, Coloradohttps://doi.org/10.2514/6.2017-4194 CrossmarkInformationCopyright © 2017 by André Valdetaro Gomes Cavalieri. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsActuatorsAeronauticsAvionicsComputational Fluid DynamicsControl SystemsControl TheoryFlow RegimesFluid DynamicsGuidance, Navigation, and Control SystemsSensorsShock WavesTransducersVortex Dynamics KeywordsParabolized Stability EquationsLarge Eddy SimulationClosed Loop ControlMach WavesSingle Input Single OutputActuatorsSensorsFrequency DomainStrouhal NumbersSubsonic JetPDF Topics Aeroacoustics