No AccessTransonic Flutter Characteristics of Advanced Fighter WingsOddvar O. BendiksenOddvar O. BendiksenUniversity of California, Los AngelesSearch for more papers by this authorAIAA 2015-0438Session: Flutter, LCO and Aeroelastic TailoringPublished Online:2 Jan 2015https://doi.org/10.2514/6.2015-0438SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byTransonic flutter characteristics of an airfoil with morphing devices30 August 2020 | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 235, No. 6Flutter Boundary Prediction of a Two Dimensional Airfoil in Transonic Flight Regime with the Preset Angles of Attack3 July 2018 | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, Vol. 36, No. 2Transonic Panel Flutter in Accelerating or Decelerating Flow ConditionsAnastasia Shishaeva, Vasily Vedeneev, Andrey Aksenov and Gennady Sushko24 January 2018 | AIAA Journal, Vol. 56, No. 3Transonic limit cycle oscillation behavior of an aeroelastic airfoil with free-play1 Oct 2016 | Journal of Fluids and Structures, Vol. 66 What's Popular 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 5-9 January 2015Kissimmee, Floridahttps://doi.org/10.2514/6.2015-0438 CrossmarkInformationCopyright © 2015 by O.O. Bendiksen. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamic PerformanceAerodynamicsAeroelasticityAerospace SciencesAirspeedBoundary LayersComputational Fluid DynamicsFinite Element MethodFlow RegimesFluid DynamicsNormal Shock WaveShock WavesVortex DynamicsWind Tunnels KeywordsFreestream Mach NumberHigh Aspect RatioDynamic PressureTransonic Wind TunnelRapid QuenchingStratosphereAngle of AttackNonlinear Aeroelastic SystemsWing RootAircraft WingsDigital Submission Topic Structural Dynamics