No AccessAirfoil Tip Leakage Aeroacoustics Predictions using a Lattice Boltzmann Based MethodAdrien Mann, Min-Suk Kim, Jingshu Wu, Franck Perot, Julien Grilliat, Marc C. Jacob and Miles ColmanAdrien MannExa CorporationSearch for more papers by this author, Min-Suk KimExa CorporationSearch for more papers by this author, Jingshu WuExa CorporationSearch for more papers by this author, Franck PerotExa CorporationSearch for more papers by this author, Julien GrilliatUniversity of Erlangen-NürnbergSearch for more papers by this author, Marc C. JacobÉcole Centrale de LyonSearch for more papers by this author and Miles ColmanExa CorporationSearch for more papers by this authorAIAA 2016-2825Session: Turbomachinery Noise II: Flow DistortionPublished Online:27 May 2016https://doi.org/10.2514/6.2016-2825SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byAeroacoustic analysis of the tip-leakage flow of an Ultra High Bypass Ratio fan stage19 March 2023 | Physics of FluidsOn the origin of quadrupole sound from a two-dimensional aerofoil trailing edge27 February 2023 | Journal of Fluid Mechanics, Vol. 958On the tip leakage noise generating mechanisms of single-fixed aerofoilIvan Saraceno, Sergi Palleja-Cabre, Prateek Jaiswal, Chaitanya C. Paruchuri and Bharath Ganapathisubramani13 June 2022Large-Eddy Simulation of a Linear Compressor Cascade with Tip Gap: Aerodynamic and Acoustic AnalysisRegis Koch, Marlène Sanjosé and Stephane Moreau28 July 2021Large-Eddy Simulation of a Single Airfoil Tip-Leakage FlowRegis Koch, Marlene Sanjose and Stephane Moreau8 June 2020Benefits of curved serrations on broadband trailing-edge noise reduction1 Jul 2017 | Journal of Sound and Vibration, Vol. 400Numerical study on combed teeth serrations for wind turbine noise reductionWouter C. van der Velden and Stefan Oerlemans2 June 2017Numerical analysis of noise reduction mechanisms on improved trailing edge serrations using the Lattice Boltzmann methodWouter C. van der Velden and Stefan Oerlemans5 January 2017 What's Popular 22nd AIAA/CEAS Aeroacoustics Conference 30 May - 1 June, 2016Lyon, Francehttps://doi.org/10.2514/6.2016-2825 CrossmarkInformationCopyright © 2016 by Exa Corporation. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAeroacousticsAerodynamic PerformanceAerodynamicsAerospace SciencesBoundary LayersComputational Fluid DynamicsExperimental Fluid DynamicsFlow MeasurementFlow RegimesFluid DynamicsLattice Boltzmann MethodsVelocimetryVortex DynamicsWind Tunnels KeywordsAirfoil ProfilesComputational AeroacousticsAngle of AttackLaminar Turbulent TransitionVortex StructureLattice Boltzmann MethodsKelvin Helmholtz InstabilityWind TunnelsComputational Fluid DynamicsFlow ConditionsDigital Topics