No AccessAssessment of Conceptual Noise Reduction Devices for A Main Landing Gear using SNGR MethodHuadong Yao, Lars Davidson, Shia-Hui Peng, Francesco Capizzano, Mattia Barbarino and Giuseppe MingioneHuadong YaoChalmers University of TechnologySearch for more papers by this author, Lars DavidsonChalmers University of TechnologySearch for more papers by this author, Shia-Hui PengSwedish Defense Research Agency (FOI)Search for more papers by this author, Francesco CapizzanoItalian Aerospace Research Center (CIRA)Search for more papers by this author, Mattia BarbarinoItalian Aerospace Research Center (CIRA)Search for more papers by this author and Giuseppe MingioneItalian Aerospace Research Center (CIRA)Search for more papers by this authorAIAA 2015-2692Session: Airframe Noise IIPublished Online:18 Jun 2015https://doi.org/10.2514/6.2015-2692SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byAirfoil trailing-edge noise prediction based on CFD/CAA coupled boundary method7 June 2023 | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, Vol. 41, No. 2Adjoint-based Broadband Noise Minimization using Stochastic Noise GenerationBeckett Yx Zhou, Nicolas R. Gauger, Huadong Yao, Shia-Hui Peng and Lars Davidson18 May 2019 What's Popular 21st AIAA/CEAS Aeroacoustics Conference 22-26 June 2015Dallas, TXhttps://doi.org/10.2514/6.2015-2692 CrossmarkInformationCopyright © 2015 by Hua-Dong Yao, Lars Davidson. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAeroacousticsAerodynamic PerformanceAerodynamicsAerospace SciencesBoundary Element MethodComputational Fluid DynamicsFinite Element MethodFinite Volume MethodFlow RegimesFluid DynamicsMesh GenerationTurbulenceTurbulence Models KeywordsSound Pressure LevelLanding GearReynolds Averaged Navier StokesComputational Fluid DynamicsAngle of AttackCompressible FlowItalian Aerospace Research CentreKinetic EnergyMach NumberBoundary Element MethodDigital Topics Aeroacoustics