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Centerline instabilities on the hypersonic international flight research experimentation HIFiRE-5 elliptic cone model
Institution:1. University of Genova 1 via Montallegro, Italy;2. Monash University, Australia;3. Monash University, Australia;4. Institut de Mécanique des Fluides de Toulouse, France;1. Universidade de São Paulo, Departamento de Engenharia Aeronautica, Av. João Dagnone, 1100, São Carlos-SP, CEP 13563120, Brazil;2. Universidade Estadual Paulista (UNESP), Câmpus de Sãao João da boa Vista - SP, Brazil;1. Science and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, Hunan, 410073, People''s Republic of China;2. Institute of Systems Engineering, Academy of Military Sciences PLA China, Beijing, 100071, People''s Republic of China;1. Sorbonne Université, CNRS, Institut Jean Le Rond d''Alembert, F-75005 Paris, France;2. DynFluid Laboratory - Arts et Métiers - 151, Bd. de l''Hôpital, 75013, Paris, France;3. Aix Marseille Univ., CNRS, Centrale Marseille, M2P2 UMR 7340, 13451, Marseille, France;1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;2. Department of Mechanical Engineering, The Hong Kong Polytechnic University, Kowloon, Hong Kong Special Administrative Region;3. Supercomputing Center, Computer Network Information Center, Chinese Academy of Sciences, Beijing 100190, China
Abstract:
Keywords:Elliptic cone  Hypersonic flow  Linear modal instability  Spatial BiGlobal analysis
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