A Computational Framework for Parachute Inflation Based on Immersed Boundary/Finite Element Approach

被引：0

作者：

Huang, Yunyao ^{[1
]}

Zhang, Yang ^{[1
,2
]}

Pu, Tianmei ^{[3
]}

Jia, He ^{[2
,4
]}

Wu, Shiqing ^{[2
,4
]}

Zhou, Chunhua ^{[5
]}

机构：

[1] College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing,211106, China

[2] Laboratory of Aerospace Entry，Descent and Landing Technology, CASC, Beijing,100094, China

[3] College of Electrical，Energy and Power Engineering, Yangzhou University, Yangzhou,225127, China

[4] Beijing Institute of Space Mechanics and Electricity, Beijing,100096, China

[5] College of Aeronautics, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China

来源：

Transactions of Nanjing University of Aeronautics and Astronautics | 2024年 / 41卷 / 04期

关键词：

Dynamic response - Parachutes;

D O I：

10.16356/j.1005-1120.2024.04.007

中图分类号：

学科分类号：

摘要：

A computational framework for parachute inflation is developed based on the immersed boundary/finite element approach within the open-source IBAMR library. The fluid motion is solved by Peskin’s diffuse-interface immersed boundary（IB）method，which is attractive for simulating moving-boundary flows with large deformations. The adaptive mesh refinement technique is employed to reduce the computational cost while retain the desired resolution. The dynamic response of the parachute is solved with the finite element approach. The canopy and cables of the parachute system are modeled with the hyperelastic material. A tether force is introduced to impose rigidity constraints for the parachute system. The accuracy and reliability of the present framework is validated by simulating inflation of a constrained square plate. Application of the present framework on several canonical cases further demonstrates its versatility for simulation of parachute inflation. © 2024 Nanjing University of Aeronautics an Astronautics. All rights reserved.

引用

页码：502 / 514