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Spatial Structure Similarity Analysis of Aero-Optical Wavefront Induced by Supersonic Film Cooling

2021; American Institute of Aeronautics and Astronautics; Volume: 59; Issue: 9 Linguagem: Inglês

10.2514/1.j060517

1533-385X

Haolin Ding, Shihe Yi, Yao Xu, Xinhai Zhao, Lin He,

Advanced Image Processing Techniques

No AccessTechnical NotesSpatial Structure Similarity Analysis of Aero-Optical Wavefront Induced by Supersonic Film CoolingHaolin Ding, Shihe Yi, Yao Xu, Xinhai Zhao and Lin HeHaolin DingNational University of Defense Technology, 410073 Changsha, People's Republic of China, Shihe YiNational University of Defense Technology, 410073 Changsha, People's Republic of China, Yao XuNational University of Defense Technology, 410073 Changsha, People's Republic of China, Xinhai ZhaoNational University of Defense Technology, 410073 Changsha, People's Republic of China and Lin HeNational University of Defense Technology, 410073 Changsha, People's Republic of ChinaPublished Online:7 May 2021https://doi.org/10.2514/1.J060517SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Fu J., Yi S.-H., Wang X. -H., He L. and Ge Y., "Experimental Study on Supersonic Film Cooling on the Surface of a Blunt Body in Hypersonic Flow," Chinese Physics B, Vol. 23, No. 10, 2014, Paper 104702. https://doi.org/10.1088/1674-1056/23/10/104702 Google Scholar[2] Ding H., Yi S., Zhao X. and Xu Y., "Experimental Investigation on Aero-Optical Effects of a Hypersonic Optical Dome Under Different Exposure Times," Applied Optics, Vol. 59, No. 13, 2020, pp. 3842–3850. https://doi.org/10.1364/AO.387513 CrossrefGoogle Scholar[3] Guo G., Liu H. and Zhang B., "Aero-Optical Effects of an Optical Seeker with a Supersonic Jet for Hypersonic Vehicles in Near Space," Applied Optics, Vol. 55, No. 17, 2016, pp. 4741–4751. https://doi.org/10.1364/AO.55.004741 CrossrefGoogle Scholar[4] Yang-Zhu Z., Shi-He Y., Lin H., Li-Feng T. and Yong-Wei Z., "Instantaneous and Time-Averaged Flow Structures Around a Blunt Double-Cone with or Without Supersonic Film Cooling Visualized via Nano-Tracer Planar Laser Scattering," Chinese Physics B, Vol. 22, No. 1, 2013, pp. 368–373. https://doi.org/10.1088/1674-1056/22/1/014702 Google Scholar[5] Xu L. and Cai Y., "Influence of Altitude on Aero-Optic Imaging Deviation," Applied Optics, Vol. 50, No. 18, 2011, pp. 2949–2957. https://doi.org/10.1364/AO.50.002949 CrossrefGoogle Scholar[6] Babcock H. 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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 EngineeringAeronauticsAerothermodynamicsAirspeedCooling TechnologyFluid DynamicsFluid Flow PropertiesFluid MechanicsIdeal GasThermal Control and ProtectionThermal InsulationThermodynamicsThermophysics and Heat Transfer KeywordsFilm CoolingCharge Coupled DeviceStatic PressureMach NumberBackground Oriented SchlierenGas ConstantViscosityAerodynamic HeatingHypersonic AircraftThermal InsulationAcknowledgmentThis work was supported by the National Natural Science Foundation of China (Grant Nos. 11527802 and 91752102) and Hunan Provincial Innovation Foundation for Postgraduate (CX20190010).PDF Received5 January 2021Accepted22 March 2021Published online7 May 2021