No AccessNumerical comparison between the Dynamic mode decomposition and the Arnoldi extraction technique on an afterburner test caseGuillaume Jourdain and Lars-Erik ErikssonGuillaume JourdainChalmers University of TechnologySearch for more papers by this author and Lars-Erik ErikssonChalmers University of TechnologySearch for more papers by this authorPublished Online:11 Nov 2012https://doi.org/10.2514/6.2012-2147SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byCombined applications of analytic methods for detection of combustion instability triggering1 Nov 2021 | Aerospace Science and Technology, Vol. 118Applications of Dynamic Mode Decomposition to Unstable Shock-Induced Combustion1 Apr 2017 | Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 2Modeling and Simulation of Bluff Body Stabilized Turbulent Premixed FlamesAdam L. Comer, Cheng Huang, Brent A. Rankin, Matthew E. Harvazinski and Venke Sankaran2 January 2016Application of dynamic mode decomposition to acoustic-modes identification and damping in a 3-dimensional chamber with baffled injectors1 Sep 2013 | Journal of Sound and Vibration, Vol. 332, No. 18 What's Popular 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference) 04 June 2012 - 06 June 2012Colorado Springs, COhttps://doi.org/10.2514/6.2012-2147 Crossmark TopicsAircraft EnginesCombustion ChambersCombustorsComputational Fluid DynamicsConservation of Momentum EquationsEquations of Fluid DynamicsFinite Volume MethodFluid DynamicsFluid Flow PropertiesFuel InjectionGas TurbineIgnition SystemsJet EnginesPropulsion and PowerTurbinesTurbomachinery KeywordsAfterburnerAcoustic InstabilityNavier Stokes EquationsCombustorsReynolds Averaged Navier StokesResonance FrequenciesEddy ViscosityVolvo Aero CorporationFinite Volume MethodK Epsilon Turbulence ModelDigital Topics Aeroacoustics