No AccessAeroelastic Level Set Topology Optimization for a 3D WingSandilya Kambampati, Scott Townsend and Hyunsun A. KimSandilya KambampatiUniversity of California, San DiegoSearch for more papers by this author, Scott TownsendCardiff UniversitySearch for more papers by this author and Hyunsun A. KimUniversity of California, San DiegoSearch for more papers by this authorAIAA 2018-2151Session: Aeroelastic and Aero-Structures Optimization IIPublished Online:7 Jan 2018https://doi.org/10.2514/6.2018-2151SectionsPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byDesign Methodology for Aeroelastic Tailoring of Additively Manufactured Lattice Structures Using Low-Order MethodsMax M. J. Opgenoord and Karen E. Willcox19 September 2019 | AIAA Journal, Vol. 57, No. 11 What's Popular 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 8–12 January 2018Kissimmee, Floridahttps://doi.org/10.2514/6.2018-2151 CrossmarkInformationCopyright © 2018 by Sandilya Kambampati, Scott Townsend, Hyunsun Alicia Kim. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAircraft Components and StructureAircraft DesignAircraft Operations and TechnologyAircraft Stability and ControlAircraft Wing DesignAirfoilAirfoil NomenclatureComputational Fluid DynamicsFinite Element MethodFluid DynamicsStructures, Design and TestWing ConfigurationsWing Planforms KeywordsTopology OptimizationFinite Element AnalysisAircraft Wing DesignAircraft SkinAerodynamic CenterBending StiffnessAngle of AttackCantilever BeamElastic ModulusWing Box Structure Topics Multidisciplinary Design Optimization