No AccessEffect of Rear Face Geometry on the Open Cavity Oscillatory Flow at M=0.9Sudip Das and Jacob CohenSudip DasBirla Institute of TechnologySearch for more papers by this author and Jacob CohenTechnion--Israel Institute of TechnologySearch for more papers by this authorAIAA 2016-3175Session: Cavity Flows IPublished Online:10 Jun 2016https://doi.org/10.2514/6.2016-3175SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byAnalysis of Cavity Corner Geometry Effect on Recirculation Zone Structure20 June 2022 | Applied Sciences, Vol. 12, No. 12Effect of cavity rear wall modifications on pressure fluctuations at supersonic speed1 Aug 2021 | Acta Astronautica, Vol. 185Study on Oscillation Phenomena in Morphing Cavities with Ramps of Leading WallZhe Liu, Fangli Ning, Qingbo Zhai, Hui Ding, Juan Wei and Baoqing Li15 October 2020 | Journal of Aircraft, Vol. 58, No. 3Volumetric Velocimetry of Complex Geometry Effects on Transonic Flow over CavitiesEdward P. DeMauro, Steven J. Beresh, Katya M. Casper, Justin L. Wagner, John F. Henfling and Russell W. Spillers19 February 2019 | AIAA Journal, Vol. 57, No. 5Influence of Impinging Wall Ramping Modification on the Flow Field of Open Cavity at M = 2.016 March 2018 | Journal of Fluids Engineering, Vol. 140, No. 7Reducing Pressure Oscillations by Change in Rear-Face Geometries at Subsonic and Transonic SpeedsS. Das and J. Cohen6 September 2017 | AIAA Journal, Vol. 55, No. 12 What's Popular 8th AIAA Flow Control Conference 13-17 June 2016Washington, D.C.https://doi.org/10.2514/6.2016-3175 CrossmarkInformationCopyright © 2016 by Sudip Das, Jacob Cohen. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAeroacousticsAerodynamicsAerospace SciencesAirspeedBoundary LayersComputational Fluid DynamicsFlow RegimesFluid DynamicsFluid MechanicsTurbulenceTurbulence ModelsVortex DynamicsWind Tunnels KeywordsReynolds Averaged Navier StokesNumerical SimulationTurbulence ModelsFighter AircraftBoundary Layer ThicknessVortex SheddingOverall Sound Pressure LevelAccelerating FlowHypersonic SpeedStatic PressureDigital Topics Applied Aerodynamics