主管部门: 中国航天科技集团有限公司
主办单位: 中国航天空气动力技术研究院
中国宇航学会
中国宇航出版有限责任公司

基于IB-LBFS和绝对节点坐标法的降落伞柔性结构流固耦合数值模拟

Fluid-Structure Interaction Simulation of Parachute Based on IB-LBFS and Absolute Nodal Coordinate Formulation

  • 摘要: 在空气动力学、水动力学和生物流体力学领域中,大变形柔性结构的流固耦合现象是一个重要的非线性力学问题.对该系统的数值模拟是分析这一问题的有效手段.将近年提出的一种Descartes流场求解器,即浸润边界-格子Boltzmann通量求解器(immersed boundary-lattice Boltzmann flux solver,IB-LBFS)作为流场求解方法,并引入绝对节点坐标法(absolute nodal coordinate formulation,ANCF)作为大变形结构分析手段,构建了流固耦合求解器以模拟三维流场中的大变形柔性体运动.使用三维来流中的旗帜摆动算例对该流固耦合求解器进行了验证计算.基于该流固耦合求解器对三维不可压流场中的矩形降落伞和十字形降落伞的展开过程进行了非定常流固耦合数值模拟.

     

    Abstract: Fluid-structure interaction (FSI) for structures with large deformation is a crucial problem in aerodynamics, hydrodynamics and bio-fluid mechanics. An efficient numerical method is needed in FSI modeling and analyzing flow over elastic structures. A new FSI solver, which adopts the recent developed Cartesian flow solver called immersed boundary-lattice Boltzmann flux solver (IB-LBFS) and the structure solver of finite element absolute nodal coordinate formulation (ANCF), was developed and validated. Acceleration techniques of the IB-LBFS were applied and a parallel computation framework was implemented. The dynamic behaviors of a square parachute and a cross parachute during inflation were performed with the current IB-LBFS/ANCF FSI solver. Aerodynamic characteristics and the elastic configuration were obtained for different material Young's modulus.

     

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