1.College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, P.R. China;2.Laboratory of Aerospace Entry, Descent and Landing Technology, CASC, Beijing 100094, P.R. China;3.College of Electrical, Energy and Power Engineering, Yangzhou University, Yangzhou 225127, P.R. China;4.Beijing Institute of Space Mechanics and Electricity, Beijing 100096, P.R. China;5.College of Aeronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R. China
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This work was supported by the Open Project of Key Laboratory of Aerospace EDLA, CASC (No.EDL19092208).
HUANG Yunyao, ZHANG Yang, PU Tianmei, JIA He, WU Shiqing, ZHOU Chunhua. A Computational Framework for Parachute Inflation Based on Immersed Boundary/Finite Element Approach[J]. Transactions of Nanjing University of Aeronautics & Astronautics,2024,(4):502-514
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