No AccessExperimental Validation of a Forced Response Analysis Using a Time-Linearized MethodSimon L. Bittner, Christian Keller, Christopher E. Meinzer and Jörg R. SeumeSimon L. BittnerLeibniz UniversitySearch for more papers by this author, Christian KellerLeibniz UniversitySearch for more papers by this author, Christopher E. MeinzerLeibniz UniversitySearch for more papers by this author and Jörg R. SeumeLeibniz UniversitySearch for more papers by this authorAIAA 2018-0461Session: Limit Cycle Oscillations and Gust ResponsePublished Online:7 Jan 2018https://doi.org/10.2514/6.2018-0461SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byAerodynamic and Aeroelastic Effects of Design-Based Geometry Variations on a Low-Pressure Compressor24 September 2020 | International Journal of Turbomachinery, Propulsion and Power, Vol. 5, No. 4 What's Popular 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 8–12 January 2018Kissimmee, Floridahttps://doi.org/10.2514/6.2018-0461 CrossmarkInformationCopyright © 2018 by Leibniz Universitaet Hannover. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamicsAeroelasticityAerospace SciencesCFD CodesComputational Fluid DynamicsFinite Element MethodFinite Element SoftwareFlow RegimesFluid DynamicsFluid MechanicsNumerical AnalysisTurbulenceTurbulence Models KeywordsReynolds Averaged Navier StokesAxial CompressorsAircraft EnginesTurbomachineryCFD CodesAeroelasticityVibration AmplitudeModal AnalysisRotor BladesFuel ConsumptionDigital Topics Structural Dynamics