No AccessTurbulent Boundary Layer over a Piezoelectrically Excited Traveling Wave SurfacePatrick F. Musgrave and Pablo A. TarazagaPatrick F. MusgraveVirginia Polytechnic Institute and State UniversitySearch for more papers by this author and Pablo A. TarazagaVirginia Polytechnic Institute and State UniversitySearch for more papers by this authorAIAA 2019-1354Session: Structural Concepts for Improved Aerodynamics and Reduced VibrationPublished Online:6 Jan 2019https://doi.org/10.2514/6.2019-1354SectionsPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byFlow control and separation delay in morphing wing aircraft using traveling wave actuation14 January 2021 | Smart Materials and Structures, Vol. 30, No. 2Guidelines and procedure for tailoring high-performance, steady-state traveling waves for propulsion and solid-state motion7 January 2021 | Smart Materials and Structures, Vol. 30, No. 2 What's Popular AIAA Scitech 2019 Forum 7-11 January 2019San Diego, Californiahttps://doi.org/10.2514/6.2019-1354 CrossmarkInformationCopyright © 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. TopicsActuatorsAerodynamicsAeronautical EngineeringAeronauticsAvionicsBoundary LayersFlow RegimesFluid DynamicsFluid Flow PropertiesGuidance, Navigation, and Control SystemsSkin FrictionTurbulenceVortex DynamicsWind Tunnels KeywordsTurbulent Boundary LayerNo Slip ConditionSkin Friction CoefficientPiezoelectric ActuatorsLow Speed Wind TunnelLaser Doppler VibrometerFree Stream VelocityHot Wire AnemometryOpen LoopFlight Vehicle Topics Adaptive Structures