No AccessReduction of Skin Friction Drag in a Turbulent Boundary Layer Using Circular Synthetic JetsEmanuele Spinosa and Shan ZhongEmanuele SpinosaUniversity of ManchesterSearch for more papers by this author and Shan ZhongUniversity of ManchesterSearch for more papers by this authorAIAA 2017-0324Session: Synthetic JetsPublished Online:5 Jan 2017https://doi.org/10.2514/6.2017-0324SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byEffects of submerged synthetic jet on the coherent structures in turbulent boundary layer15 May 2022 | Acta Mechanica Sinica, Vol. 38, No. 12Influence of Synthetic Jets on Multiscale Features in Wall-Bounded Turbulence18 July 2022 | Actuators, Vol. 11, No. 7Formation and scaling of a coherent large-scale vortex from the impingement of a laminar synthetic jet16 April 2022 | Experiments in Fluids, Vol. 63, No. 4Characteristics of array of distributed synthetic jets and effect on turbulent boundary layer12 October 2020 | Acta Mechanica Sinica, Vol. 36, No. 6Reduction of turbulent boundary layer drag through dielectric-barrier-discharge plasma actuation based on the Spalding formula18 January 2019 | Plasma Science and Technology, Vol. 21, No. 4 What's Popular 55th AIAA Aerospace Sciences Meeting 9 - 13 January 2017Grapevine, Texashttps://doi.org/10.2514/6.2017-0324 CrossmarkInformationCopyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. TopicsAerodynamicsAerospace SciencesBoundary LayersComputational Fluid DynamicsExperimental Fluid DynamicsFlow MeasurementFlow RegimesFluid DynamicsFluid Flow PropertiesSkin FrictionTurbulenceVelocimetryVortex Dynamics KeywordsSkin Friction CoefficientTurbulent Boundary LayerParticle Image VelocimetryFree Stream VelocityVelocity ProfilesTurbulence IntensityShear StressVorticesDirect Numerical SimulationLaw of the WallDigital Topics Fluid Dynamics