No AccessA Study of the Aeroelastic Behavior of Flat Plates and Membranes with Mixed Boundary Conditions in Axial Subsonic FlowLiz Bloomhardt and Earl DowellLiz BloomhardtDuke UniversitySearch for more papers by this author and Earl DowellDuke UniversitySearch for more papers by this authorPublished Online:14 Jun 2012https://doi.org/10.2514/6.2011-1995SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byFinite element model to investigate the dynamic instability of rectangular plates subjected to supersonic airflowJournal of Fluids and Structures, Vol. 103Stability of Rectangular Plates in Subsonic Flow with Various Boundary ConditionsS. Chad Gibbs IV, Ivan Wang and Earl H. Dowell9 May 2014 | Journal of Aircraft, Vol. 52, No. 2Aeroelastic Behavior of Noise-Reducing Membranes for Aircraft Lifting Surfaces Part I: TheorySamuel Gibbs IV, Ivan Wang, Liz Bloomhardt and Earl Dowell14 June 2012A Nested Extreme Response Surface Approach for RBDO with Time-Dependent Probabilistic ConstraintsZequn Wang and Pingfeng Wang14 June 2012 What's Popular 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 04 April 2011 - 07 April 2011Denver, Coloradohttps://doi.org/10.2514/6.2011-1995 Crossmark TopicsAerodynamicsAeroelasticityAerospace SciencesComputational Fluid DynamicsEquations of Fluid DynamicsFinite Element MethodFlow RegimesFluid DynamicsFluid MechanicsVortex DynamicsWind Tunnels KeywordsPotential FlowMixed Boundary ConditionHigh Aspect RatioDynamic PressureAerodynamic ForceLanding GearTransport AircraftAircraft LandingStiffness MatricesElastic ModulusPDF Topics