Effect of Freestream Noise on Hypersonic Crossflow-Induced Boundary-Layer Transition

No AccessTechnical NotesEffect of Freestream Noise on Hypersonic Crossflow-Induced Boundary-Layer TransitionAndrew N. Bustard, Thomas J. Juliano, Harrison B. Yates, Mark Noftz and Joseph S. JewellAndrew N. BustardUniversity of Notre Dame, Notre Dame, Indiana 46556-5684*Graduate Student, Department of Aerospace and Mechanical Engineering. Student Member AIAA.Search for more papers by this author, Thomas J. Juliano https://orcid.org/0000-0002-9362-6007University of Notre Dame, Notre Dame, Indiana 46556-5684†Associate Professor, Department of Aerospace and Mechanical Engineering. Associate Fellow AIAA.Search for more papers by this author, Harrison B. YatesJohns Hopkins University Applied Physics Laboratory, Laurel, Maryland 20723‡Senior Professional Staff. Member AIAA.Search for more papers by this author, Mark NoftzPurdue University, West Lafayette, Indiana 47907-2045§Graduate Student, School of Aeronautics and Astronautics. Student Member AIAA.Search for more papers by this author and Joseph S. Jewell https://orcid.org/0000-0002-4047-9998Purdue University, West Lafayette, Indiana 47907-2045¶Assistant Professor, School of Aeronautics and Astronautics. Associate Fellow AIAA.Search for more papers by this authorPublished Online:1 Nov 2022https://doi.org/10.2514/1.J060376SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Schuele C. Y., “Control of Stationary Crossflow Modes Using Stationary Patterned Roughness and DBD Plasma Actuators at Mach 3.5,” Ph.D. Thesis, Univ. of Notre Dame, Notre Dame, Indiana, Sept. 2011. Google Scholar[2] Li F., Choudhari M., Chang C. and White J., “Analysis of Instabilities in Non-Axisymmetric Hypersonic Boundary Layers over Cones,” AIAA Paper 2010-4643, June 2010. LinkGoogle Scholar[3] Saric W. S., Reed H. L. and White E. 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TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesBoundary LayersComputing, Information, and CommunicationFlow RegimesFluid DynamicsMaterial PropertiesMaterialsMaterials and Structural MechanicsPolymersSignal ProcessingSurface PropertiesVortex Dynamics KeywordsBoundary Layer TransitionFreestreamVorticesStanton NumberPSDAngle of AttackPolyether Ether KetoneSurface RoughnessTurbulent FlowNozzle WallsAcknowledgmentsThis work was supported by the Air Force Office of Scientific Research under award number FA9550-16-1-0320. Brandon Chynoweth had valuable thoughts that were helpful for the project.PDF Received19 December 2020Accepted28 August 2022Published online1 November 2022