No AccessCoherence Analysis of the Noise from a Simulated Highly-heated Laboratory-scale JetKevin M. Leete, Kent L. Gee, Junhui Liu and Alan T. WallKevin M. LeeteBrigham Young UniversitySearch for more papers by this author, Kent L. GeeBrigham Young UniversitySearch for more papers by this author, Junhui LiuNaval Research LaboratorySearch for more papers by this author and Alan T. WallAir Force Research LaboratorySearch for more papers by this authorAIAA 2019-2633Session: Jet Aeroacoustics XPublished Online:18 May 2019https://doi.org/10.2514/6.2019-2633SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for references What's Popular 25th AIAA/CEAS Aeroacoustics Conference 20-23 May 2019Delft, The Netherlandshttps://doi.org/10.2514/6.2019-2633 CrossmarkInformationCopyright © 2019 by The Authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAeroacousticsAerodynamicsAirspeedBoundary LayersComputational Fluid DynamicsFlow RegimesFluid DynamicsNumerical AnalysisNumerical InterpolationShock WavesVortex Dynamics KeywordsFlux Corrected TransportHigh Performance Military AircraftJet NoiseAfterburnerShear LayersTemperature RatioSound Pressure LevelMach WavesMach NumberConvergent Divergent NozzlesPDF Topics Aeroacoustics