No AccessA Study on the Aerodynamic Efficiency and Static Stability of a Tailless AircraftYoshifumi Kashiwagura and Koji ShimoyamaYoshifumi KashiwaguraTohoku UniversitySearch for more papers by this author and Koji ShimoyamaTohoku UniversitySearch for more papers by this authorAIAA 2018-1914Session: Aerodynamic Shape Optimization IIPublished Online:7 Jan 2018https://doi.org/10.2514/6.2018-1914SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesRelated articlesCorrection: A Study on the Aerodynamic Efficiency and Static Stability of a Tailless Aircraft26 Jan 2018AIAA SciTech Forum What's Popular 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 8–12 January 2018Kissimmee, Floridahttps://doi.org/10.2514/6.2018-1914 CrossmarkInformationCopyright © 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. TopicsAerodynamic PerformanceAerodynamicsCFD CodesComputational Fluid DynamicsFinite Volume MethodFluid DynamicsHeat TransferNumerical AnalysisNumerical Heat TransferSlip (Aerodynamics)Thermophysics and Heat TransferTurbulenceTurbulence ModelsWind Tunnels KeywordsMean Aerodynamic ChordAerodynamic PerformanceCamberAngle of SideslipComputational Fluid DynamicsDutch RollAerodynamic Shape OptimizationKriging ModelReynolds Averaged Navier StokesAircraft ConfigurationsPDF Topics Multidisciplinary Design Optimization