Hypersonic Boundary-Layer Instability Characteristics on Sharp Cone with Porous Coating

No AccessTechnical NotesHypersonic Boundary-Layer Instability Characteristics on Sharp Cone with Porous CoatingYuteng Gui, Weizhang Wang, Rui Zhao, Jiaquan Zhao and Jie WuYuteng Gui https://orcid.org/0000-0001-8999-4483Huazhong University of Science and Technology, 430074 Wuhan, People’s Republic of China*Graduate Student, School of Aerospace Engineering.Search for more papers by this author, Weizhang WangBeijing Institute of Technology, 100081 Beijing, People’s Republic of China*Graduate Student, School of Aerospace Engineering.Search for more papers by this author, Rui ZhaoBeijing Institute of Technology, 100081 Beijing, People’s Republic of China†Associate Professor, School of Aerospace Engineering. Member AIAA.Search for more papers by this author, Jiaquan ZhaoHuazhong University of Science and Technology, 430074 Wuhan, People’s Republic of China‡Assistant Professor, School of Aerospace Engineering; (Co-Corresponding Author).Search for more papers by this author and Jie Wu https://orcid.org/0000-0001-7040-0817Huazhong University of Science and Technology, 430074 Wuhan, People’s Republic of China§Associate Professor, School of Aerospace Engineering; (Corresponding Author).Search for more papers by this authorPublished Online:16 May 2022https://doi.org/10.2514/1.J060930SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Fedorov A., “Transition and Stability of High-Speed Boundary Layers,” Annual Review of Fluid Mechanics, Vol. 43, No. 1, 2011, pp. 79–95. https://doi.org/10.1146/annurev-fluid-122109-160750 CrossrefGoogle Scholar[2] Reed H., Kimmel R., Schneider S., Arnal D., Reed H., Kimmel R., Schneider S. and Arnal D., “Drag Prediction and Transition in Hypersonic Flow,” 28th Fluid Dynamics Conference, AIAA Paper 1997-1818, 1997. https://doi.org/10.2514/6.1997-1818 LinkGoogle Scholar[3] Capriotti D., “Viscous Optimized Hypersonic Waveriders,” 25th AIAA Aerospace Sciences Meeting, AIAA Paper 1987-0272, 1987. https://doi.org/10.2514/6.1987-272 LinkGoogle Scholar[4] Mack L. 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TopicsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsBoundary LayersComputational Fluid DynamicsFinite Element MethodFlow RegimesFluid DynamicsFluid Flow PropertiesFluid MechanicsMesh GenerationVortex DynamicsWind Tunnels KeywordsBoundary Layer TransitionPower Spectral DensityShock TunnelsFlow ConditionsPiezoelectric SensorsLudwieg TubeDirect Numerical SimulationScanning Electron MicroscopeThermal Protection SystemSurface RoughnessAcknowledgmentsDr. Mi Zhao is specially acknowledged for providing the scanning electron microscope image of porous coating. This work was supported by the National Natural Science Foundation of China (grant number 92052301).PDF Received23 May 2021Accepted27 March 2022Published online16 May 2022