Extension of a sharp-interface immersed-boundary method for simulating parachute inflation

被引:0
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作者
Yang Zhang
Tianmei Pu
He Jia
Shiqing Wu
Chunhua Zhou
机构
[1] Nanjing University of Aeronautics and Astronautics,College of Astronautics
[2] CASC,Laboratory of Aerospace Entry, Descent and Landing Technology
[3] Yangzhou University,College of Electrical, Energy and Power Engineering
[4] Nanjing University of Aeronautics and Astronautics,College of Aeronautics
[5] Beijing Institute of Space Mechanics and Electricity,undefined
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关键词
Parachute inflation; Immersed boundary method; Fluid-structure interaction; preCICE; CalculiX;
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摘要
In this work, the sharp-interface immersed boundary (IB) method proposed by Mittal et al. (J Comput Phys 227(10):4825–4852, 2008) is extended to fluid-structure-interaction (FSI) simulation of parachute inflation by utilizing several open-source tools. The method employs a Cartesian-grid ghost-cell methodology to accurately represent the immersed boundary, and it is suitable for solving moving-boundary flows with arbitrarily complex geometries. The finite-element code CalculiX is employed to solve the structural dynamics of the parachute system. The IB flow solver is coupled with CalculiX in a minimally-invasive manner using the multi-physics coupling library preCICE. The implicit fluid-structure coupling together with the Aitken adaptive under-relaxation scheme is considered to improve the numerical accuracy and stability. The developed approach is validated by a benchmark FSI case. Numerical experiments on the inflation process of several typical parachutes are further conducted. The breathing process, flow structure, canopy displacement and drag coefficient are analyzed to demonstrate the applicability of the present approach for simulating parachute inflation.
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