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Simultaneous Scalar and Velocity Imaging in a Mach Five Boundary Layer

2019; American Institute of Aeronautics and Astronautics; Volume: 57; Issue: 11 Linguagem: Inglês

10.2514/1.j058614

1533-385X

Christopher S. Combs, Noel Clemens,

Gas Dynamics and Kinetic Theory

No AccessTechnical NotesSimultaneous Scalar and Velocity Imaging in a Mach Five Boundary LayerChristopher S. Combs and Noel T. ClemensChristopher S. CombsUniversity of Texas at San Antonio, San Antonio, Texas 78249*Dee Howard Endowed Assistant Professor, Department of Mechanical Engineering. Member AIAA.Search for more papers by this author and Noel T. ClemensUniversity of Texas at Austin, Austin, Texas 78712†Bob R. Dorsey Professor in Engineering, Department of Aerospace Engineering and Engineering Mechanics. Associate Fellow AIAA.Search for more papers by this authorPublished Online:26 Aug 2019https://doi.org/10.2514/1.J058614SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Greathouse J. S., Kirk B. S., Lillard R. P., Truong T. H., Robinson P. and Cerimele C. 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All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamicsAeronautical EngineeringAeronauticsBoundary LayersComputational Fluid DynamicsExperimental Fluid DynamicsFlow MeasurementFlow RegimesFluid DynamicsFluid Flow PropertiesFluid MechanicsVelocimetryVortex DynamicsWind Tunnels KeywordsIncompressible Turbulent Boundary LayerPlanar Laser Induced FluorescenceParticle Image VelocimetryHypersonic FlowsVelocity ProfilesDirect Numerical SimulationFluorescenceWind Tunnel TestsFreestream VelocitySchmidt NumbersAcknowledgmentThis work was supported by a NASA Office of the Chief Technologist’s Space Technology Research Fellowship Grant (No. NNX11AN55H).PDF Received1 May 2019Accepted1 August 2019Published online26 August 2019