Passive control of shock-boundary layer interaction |
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| Institution: | 1. State Key Laboratory of High Performance Ceramics and Superfine Microstructure and CAS Key Laboratory of Materials for Energy Conversion, Shanghai Institute of Ceramics, Chinese Academy of Sciences, Shanghai 200050, PR China;2. University of Chinese Academy of Sciences, 19 Yuquan Road, Beijing 100049, PR China;3. Beijing National Laboratory for Molecular Sciences and State Key Laboratory of Rare Earth Materials Chemistry and Applications, College of Chemistry and Molecular Engineering, Peking University, 202 Chengfu Road, Beijing 100871, PR China;1. Kirchhoff Institute of Physics, Heidelberg University, INF 227, 69120 Heidelberg, Germany;2. Institute of Solid State Chemistry, Ural Division, Russian Academy of Sciences, Pervomaiskaya ul. 91, Yekaterinburg, 620990 Russia;3. State Key Laboratory of Advanced Technology for Materials Synthesis and Processing, School of Material Science and Engineering, Wuhan University of Technology, Wuhan 430070, China;4. M.N. Mikheev Institute of Metal Physics, Ural Division, Russian Academy of Sciences, S. Kovalevskaya ul. 18, Yekaterinburg, 620137 Russia;5. Centre for Advanced Materials (CAM), Heidelberg University, INF 225, 69120 Heidelberg, Germany;1. School of Physics, Beijing Institute of Technology, Beijing 100081, China;2. Science and Technology on Electromagnetic Scattering Laboratory, Beijing 100854, China;1. Department of Mechanical and Aerospace Engineering, The Hong Kong University of Science and Technology, Clear Water Bay, Kowloon, Hong Kong, China;2. HKUST Shenzhen Research Institute, Shenzhen 518057, China;1. Indian Institute of Technology Kanpur, Uttar Pradesh 208016, India;2. National Aerospace Laboratories, Bengaluru 560017, India;1. Physics Department, University of Chemical Technology and Metallurgy, Sofia 1000, Bulgaria;2. Physics Department, Faculty of Science, Sohag University, Sohag 82524, Egypt |
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| Abstract: | Passive control shock-boundary layer studies, both theoretical and experimental, are reviewed in this paper. The first paper in this area was published in 1983. Since then there have been programmes of research in U.S.A., Germany and U.K. to understand the concept of passive shock wave boundary layer control and to predict the effect of such a control on the aerodynamic forces on an aerofoil. This review shows that the application of passive control in transonic flow can reduce drag, increase lift and reduce unsteady pressures on an aerofoil. |
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