No AccessSensitivity analysis of crossflow boundary layer and transition delay using plasma actuatorZhefu Wang, Liang Wang and Song FuZhefu WangTsinghua UniversitySearch for more papers by this author, Liang WangTsinghua UniversitySearch for more papers by this author and Song FuTsinghua UniversitySearch for more papers by this authorAIAA 2016-3933Session: Crossflow Transition and SeparationPublished Online:10 Jun 2016https://doi.org/10.2514/6.2016-3933SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for references What's Popular 8th AIAA Flow Control Conference 13-17 June 2016Washington, D.C.https://doi.org/10.2514/6.2016-3933 CrossmarkInformationCopyright © 2016 by Zhefu Wang. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesBoundary LayersComputational Fluid DynamicsExperimental Fluid DynamicsFinite Element MethodFlow MeasurementFlow RegimesFluid DynamicsFluid Flow PropertiesVelocimetryVortex Dynamics KeywordsSensitivity AnalysisPlasma ActuatorBoundary Layer TransitionSwept WingGortler VorticesDielectric Barrier DischargeParabolized Stability EquationsAdverse Pressure GradientKinematic ViscosityNatural Laminar FlowDigital Topics Fluid Dynamics