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Neutral Acoustic Wave Modes in Supersonic Impinging Jets

2022; American Institute of Aeronautics and Astronautics; Volume: 61; Issue: 2 Linguagem: Inglês

10.2514/1.j062262

1533-385X

Fabien Ferreira, Maxime Fiore, Hélène Parisot-Dupuis, Romain Gojon,

Computational Fluid Dynamics and Aerodynamics

No AccessTechnical NotesNeutral Acoustic Wave Modes in Supersonic Impinging JetsFabien Ferreira, Maxime Fiore, Hélène Parisot-Dupuis and Romain GojonFabien FerreiraUniversity of Toulouse, 31400 Toulouse, France, Maxime Fiore https://orcid.org/0000-0003-1740-4581University of Toulouse, 31400 Toulouse, France, Hélène Parisot-DupuisUniversity of Toulouse, 31400 Toulouse, France and Romain Gojon https://orcid.org/0000-0003-4543-338XUniversity of Toulouse, 31400 Toulouse, FrancePublished Online:20 Oct 2022https://doi.org/10.2514/1.J062262SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Powell A., "On Edge Tones and Associated Phenomena," Acta Acustica, Vol. 3, No. 1, 1953, pp. 233–243. Google Scholar[2] Ho C. M., and Nosseir, N. S., "Dynamics of an Impinging Jet. 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See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAeroacousticsAerodynamicsAeronautical EngineeringAeronauticsComputational Fluid DynamicsControl TheoryFeedback ControlFlow RegimesFluid DynamicsGuidance, Navigation, and Control SystemsVortex Dynamics KeywordsLESVortex SheetFeedback LoopMach NumberAmbient FlowSound Pressure LevelStagnation TemperatureConvergent NozzlesAcknowledgmentsThis work was performed using resources from Grand Équipement National de Calcul Intensif (GENCI) [CCRT-CINES-IDRIS] (grant 2021-[A0102A07178]) and CALculateur MIdi-Pyrénées (CALMIP) (project 1425-21A).PDF Received19 July 2022Accepted12 September 2022Published online20 October 2022