No AccessImmersed Boundary Lattice Green Function methods for External AerodynamicsGianmarco Mengaldo, Sebastian Liska, Ke Yu, Tim Colonius and Thierry JardinGianmarco MengaldoCalifornia Institute of TechnologySearch for more papers by this author, Sebastian LiskaCalifornia Institute of TechnologySearch for more papers by this author, Ke YuCalifornia Institute of TechnologySearch for more papers by this author, Tim ColoniusCalifornia Institute of TechnologySearch for more papers by this author and Thierry JardinHigher Institute of Aeronautics and SpaceSearch for more papers by this authorAIAA 2017-3621Session: Boundary and Interface TreatmentsPublished Online:2 Jun 2017https://doi.org/10.2514/6.2017-3621SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byImmersed Boundary Projection Methods16 May 2020Application of a lattice Boltzmann method to some challenges related to micro-air vehicles21 September 2018 | International Journal of Micro Air Vehicles, Vol. 10, No. 3 What's Popular 23rd AIAA Computational Fluid Dynamics Conference 5-9 June 2017Denver, Coloradohttps://doi.org/10.2514/6.2017-3621 CrossmarkInformationCopyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesComputational Fluid DynamicsConservation of Momentum EquationsEquations of Fluid DynamicsExperimental Fluid DynamicsFlow MeasurementFlow RegimesFluid DynamicsFluid Flow PropertiesNumerical AnalysisVelocimetryVortex Dynamics KeywordsDirac Delta FunctionFree Stream VelocityComputational Fluid DynamicsIncompressible FlowNavier Stokes EquationsLift CoefficientAdaptive Mesh RefinementNo Slip ConditionHigh Aspect RatioVortex ModelingDigital Submission Topic Computational Fluid Dynamics