No AccessThree-dimensional imaging of hypersonic flow at MHz-rateRichard Miles, Alexander Smits, Mark Huntley and Pingfan WuRichard MilesPrinceton Univ., NJSearch for more papers by this author, Alexander SmitsPrinceton Univ., NJSearch for more papers by this author, Mark HuntleyWhitehall Manufacturing Corp., Chester, PASearch for more papers by this author and Pingfan WuADC Telecommunications, Ewing, NJSearch for more papers by this authorPublished Online:22 Aug 2012https://doi.org/10.2514/6.2001-846SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byHypersonic Boundary Layer Transition Visualized via CO2-enhanced Rayleigh ScatteringJonathan L. Hill and Matthew P. Borg4 January 2024Implementation of Self-Aligned Focusing Schlieren for Hypersonic Boundary Layer MeasurementsJonathan L. Hill, Matthew P. Borg, Elizabeth K. Benitez, Carson L. Running and Mark F. Reeder19 January 2023Design of the Purdue Experimental Turbine Aerothermal Laboratory for Optical and Surface Aerothermal Measurements31 August 2018 | Journal of Engineering for Gas Turbines and Power, Vol. 141, No. 1Further Development of Temporally Resolved PDV and Its Application to Compressible Free Shear LayersBrian Thurow, Mo Samimy, Walter Lempert, M. Blohm and N. Jiang19 June 2012 What's Popular 39th Aerospace Sciences Meeting and Exhibit 08 January 2001 - 11 January 2001Reno,NV,U.S.A.https://doi.org/10.2514/6.2001-846 Crossmark TopicsAerodynamicsAerospace SciencesBoundary LayersComputational Fluid DynamicsFlow RegimesFluid DynamicsFluid Flow PropertiesTurbulenceVortex DynamicsWind Tunnels KeywordsTransitional FlowBoundary Layer ThicknessRayleigh ScatteringAeronauticsAstronauticsHypersonic VehiclesFree Stream VelocityStagnation PressureCondensationLaser Induced FluorescenceDigital Topics Aerospace Systems, Operations and Life Cycle