No AccessDigital Holographic Analysis of the Breakup of Aerated Liquid Jets in Supersonic CrossflowKhaled A. Sallam, Kuo-Cheng Lin, Stephen D. Hammack and Campbell D. CarterKhaled A. SallamOklahoma State UniversitySearch for more papers by this author, Kuo-Cheng LinTaitech, Inc.Search for more papers by this author, Stephen D. HammackAir Force Research LaboratorySearch for more papers by this author and Campbell D. CarterAir Force Research LaboratorySearch for more papers by this authorAIAA 2017-1957Session: Jets in Cross-FlowPublished Online:5 Jan 2017https://doi.org/10.2514/6.2017-1957SectionsPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byStudy on characteristics of fragment size distribution generated via droplet breakup by high-speed gas flowPhysics of Fluids, Vol. 34, No. 1Structures and Temporal Evolution of Liquid Jets in Supersonic CrossflowKuo-Cheng Lin, Ming-Chia Lai, Timothy Ombrello and Campbell D. Carter5 January 2017 What's Popular 55th AIAA Aerospace Sciences Meeting 9 - 13 January 2017Grapevine, Texashttps://doi.org/10.2514/6.2017-1957 CrossmarkInformationCopyright © 2017 by Khaled A. Sallam. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamicsAeronautical EngineeringAeronauticsAviationAvionicsFlow RegimesFluid DynamicsGuidance, Navigation, and Control SystemsIntegrated CircuitsMilitary AirbasesMilitary AviationSemiconductor DevicesWind Tunnels KeywordsStagnation TemperatureFreestream Mach NumberMicroscopySupersonic Wind TunnelsFlow ConditionsConvergent Divergent NozzlesTotal Mass Flow RateCharge Coupled DeviceAir Breathing Propulsion SystemAir Force Research Laboratory Topics Propellants and Combustion