No AccessNoise Prediction of the LAGOON Landing Gear Using Acoustic Analogy and Proper Orthogonal DecompositionPaulo Azevedo and William WolfPaulo AzevedoUniversity of CampinasSearch for more papers by this author and William WolfUniversity of CampinasSearch for more papers by this authorAIAA 2016-2768Session: Airframe Noise II: Landing GearPublished Online:27 May 2016https://doi.org/10.2514/6.2016-2768SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byOn the differences in noise predictions based on solid and permeable surface Ffowcs Williams–Hawkings integral solutions22 November 2019 | International Journal of Aeroacoustics, Vol. 18, No. 6-7Acoustic Prediction of LAGOON Landing Gear: Cavity Noise and Coherent StructuresTulio R. Ricciardi, William R. Wolf and Rachelle Speth30 September 2018 | AIAA Journal, Vol. 56, No. 11 What's Popular 22nd AIAA/CEAS Aeroacoustics Conference 30 May - 1 June, 2016Lyon, Francehttps://doi.org/10.2514/6.2016-2768 CrossmarkInformationCopyright © 2016 by The authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAeroacousticsAerodynamicsAerospace SciencesComputational Fluid DynamicsEquations of Fluid DynamicsFlow Diagnostics and ControlFlow RegimesFluid DynamicsNumerical AnalysisWind Tunnels KeywordsLanding GearComputational Fluid DynamicsFast Multipole MethodUnsteady Turbulent FlowAirbusPower Spectral DensityFreestream Mach NumberTotal EnergySingular Value DecompositionComputational AeroacousticsDigital Topics