No AccessMeasuring the Velocity of a Supersonic Airflow with Laser Ionization Tagged Radar Anemometry (LITRA)Sean McGuire, Sohail Zaidi, Arthur Dogariu, Phil Howard and Richard MilesSean McGuirePrinceton UniversitySearch for more papers by this author, Sohail ZaidiPrinceton UniversitySearch for more papers by this author, Arthur DogariuPrinceton UniversitySearch for more papers by this author, Phil HowardPrinceton UniversitySearch for more papers by this author and Richard MilesPrinceton UniversitySearch for more papers by this authorPublished Online:6 Nov 2012https://doi.org/10.2514/6.2012-989SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byVelocity, Mach Number, and Static Temperature Measurements in Supersonic Flows with 10 kHz Laser-Induced Schliere AnemometryLauren E. Lester and Mark Gragston29 December 2021 What's Popular 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 09 January 2012 - 12 January 2012Nashville, Tennesseehttps://doi.org/10.2514/6.2012-989 Crossmark TopicsAerodynamicsAerospace SciencesAviation CommunicationCommunication SystemComputational Fluid DynamicsComputing, Information, and CommunicationData AnalysisData AnalyticsData ScienceExperimental Fluid DynamicsFlow MeasurementFlow RegimesFluid DynamicsFluid MechanicsRADARVelocimetryWind Tunnels KeywordsSupersonic FlowRADARLasersSupersonic Wind TunnelsVelocimetryPitot ProbesRayleigh ScatteringCondensationGunn DiodesStatic PressurePDF Topics Aerospace Systems, Operations and Life Cycle
