Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Mach Six Quiet Tunnel

No AccessTechnical NotesFemtosecond Laser Electronic Excitation Tagging Velocimetry in a Mach Six Quiet TunnelJordan M. Fisher, Brandon C. Chynoweth, Michael E. Smyser, Austin M. Webb, Mikhail N. Slipchenko, Joseph S. Jewell, Terrence R. Meyer and Steven J. BereshJordan M. FisherPurdue University, West Lafayette, Indiana 47907, Brandon C. ChynowethPurdue University, West Lafayette, Indiana 47907, Michael E. SmyserPurdue University, West Lafayette, Indiana 47907, Austin M. WebbPurdue University, West Lafayette, Indiana 47907, Mikhail N. SlipchenkoPurdue University, West Lafayette, Indiana 47907, Joseph S. JewellPurdue University, West Lafayette, Indiana 47907, Terrence R. MeyerPurdue University, West Lafayette, Indiana 47907 and Steven J. BereshSandia National Laboratories, Albuquerque, New Mexico 87185Published Online:8 Jan 2021https://doi.org/10.2514/1.J059879SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Michael J. B., Edwards M. R., Dogariu A. and Miles R. B., "Femtosecond Laser Electronic Excitation Tagging for Quantitative Velocity Imaging in Air," Applied Optics, Vol. 50, No. 26, 2011, pp. 5158–5162. https://doi.org/10.1364/AO.50.005158 CrossrefGoogle Scholar[2] Miles R., "Femtosecond Laser Electronic Excitation Tagging (FLEET) for Imaging Flow Structure in Unseeded Hot or Cold Air or Nitrogen," 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA Paper 2013-0340, 2013. https://doi.org/10.2514/6.2013-340 LinkGoogle Scholar[3] Schneider S. 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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 KeywordsVelocimetryFreestream VelocityStagnation PressureHypersonic Wind TunnelsCFDFlow CharacteristicsBoeingArnold Engineering Development ComplexQuiet Flow FacilityData AcquisitionAcknowledgmentsFunding was provided by Sandia National Laboratories under award no. 1975861. Sandia National Laboratories is a multimission laboratory managed and operated by National Technology and Engineering Solutions of Sandia, LLC, which is a wholly owned subsidiary of Honeywell International, Inc., for the U.S. Department of Energy's National Nuclear Security Administration under contract DE-NA0003525.PDF Received10 June 2020Accepted10 November 2020Published online8 January 2021