No AccessReynolds Stresses in a Hypersonic Boundary Layer with Streamline Curvature-Driven Favorable Pressure GradientsNathan Tichenor, Raymond Humble and Rodney BowersoxNathan TichenorPM&AM ResearchSearch for more papers by this author, Raymond HumbleTexas A&M UniversitySearch for more papers by this author and Rodney BowersoxTexas A&M UniversitySearch for more papers by this authorPublished Online:6 Sep 2012https://doi.org/10.2514/6.2012-3059SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byParticle image velocimetry measurements of Mach 3 turbulent boundary layers at low Reynolds numbers25 April 2018 | Experiments in Fluids, Vol. 59, No. 5Development of Non-Intrusive Velocity Measurement Capabilities at AEDC Tunnel 9Jonathan M. Brooks, Ashwani K. Gupta, Michael Smith and Eric C. Marineau10 January 2014 What's Popular 42nd AIAA Fluid Dynamics Conference and Exhibit 25 June 2012 - 28 June 2012New Orleans, Louisianahttps://doi.org/10.2514/6.2012-3059 Crossmark TopicsAerodynamicsBoundary LayersComputational Fluid DynamicsExperimental Fluid DynamicsFlow MeasurementFlow RegimesFluid DynamicsFluid Flow PropertiesFluid MechanicsSkin FrictionTurbulenceVelocimetryVortex DynamicsWind Tunnels KeywordsPressure GradientIncompressible Boundary LayerBoussinesq ApproximationNormal StrainParticle Image VelocimetryFreestream VelocityFlow ConditionsVelocity ProfilesWind Tunnel ModelsTurbulence IntensityPDF Topics Fluid Dynamics