Study of velocity effects on parachute inflation performance based on fluid-structure interaction method

doi:10.1007/s10483-014-1852-6

Applied Mathematics and Mechanics (English Edition) ›› 2014, Vol. 35 ›› Issue (9): 1177-1188.doi: https://doi.org/10.1007/s10483-014-1852-6

Study of velocity effects on parachute inflation performance based on fluid-structure interaction method

程涵¹, 张鑫华², 余莉¹, 陈猛²

1. College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P. R. China;
2. Aviation Key Laboratory of Science and Technology on Aeronautical Life-Support, AVIC Aerospace Life-Support Industries Ltd., Xiangyang 441000, Hubei Province, P. R. China

收稿日期:2013-03-06 修回日期:2013-09-19 出版日期:2014-09-01 发布日期:2014-09-01
通讯作者: Li YU, yuli_happy@163.com E-mail:yuli_happy@163.com
基金资助:
Project supported by the National Natural Science Foundation of China (No. 11172137) and the Aeronautical Science Foundation of China (No. 20122910001)

Study of velocity effects on parachute inflation performance based on fluid-structure interaction method

Han CHENG¹, Xin-hua ZHANG², Li YU¹, Meng CHEN²

1. College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P. R. China;
2. Aviation Key Laboratory of Science and Technology on Aeronautical Life-Support, AVIC Aerospace Life-Support Industries Ltd., Xiangyang 441000, Hubei Province, P. R. China

Received:2013-03-06 Revised:2013-09-19 Online:2014-09-01 Published:2014-09-01
Supported by:
Project supported by the National Natural Science Foundation of China (No. 11172137) and the Aeronautical Science Foundation of China (No. 20122910001)

摘要/Abstract

摘要： The inflation of a five-ring cone parachute with the airflow velocity of 18 m/s is studied based on the simplified arbitrary Lagrange Euler (SALE)/fluid-structure interaction (FSI) method. The numerical results of the canopy shape, stability, opening load, and drag area are obtained, and they are well consistent with the experimental data gained from wind tunnel tests. The method is then used to simulate the opening process under different velocities. It is found that the first load shock affected by the velocity often occurs at the end of the initial inflation stage. For the first time, the phenomena that the inflation distance proportion coefficient increases and the dynamic load coefficient decreases, respectively, with the increase in the velocity are revealed. The above proposed method is competent to solve the large deformation problem without empirical coefficients, and can collect more space-time details of fluid-structure-motion information when it is compared with the traditional method.

关键词: empirical coefficient, opening shock load, parachute, inflation performance, fluid-structure interaction (FSI), velocity

Abstract: The inflation of a five-ring cone parachute with the airflow velocity of 18 m/s is studied based on the simplified arbitrary Lagrange Euler (SALE)/fluid-structure interaction (FSI) method. The numerical results of the canopy shape, stability, opening load, and drag area are obtained, and they are well consistent with the experimental data gained from wind tunnel tests. The method is then used to simulate the opening process under different velocities. It is found that the first load shock affected by the velocity often occurs at the end of the initial inflation stage. For the first time, the phenomena that the inflation distance proportion coefficient increases and the dynamic load coefficient decreases, respectively, with the increase in the velocity are revealed. The above proposed method is competent to solve the large deformation problem without empirical coefficients, and can collect more space-time details of fluid-structure-motion information when it is compared with the traditional method.

Key words: fluid-structure interaction (FSI), inflation performance, parachute, empirical coefficient, opening shock load, velocity

中图分类号:

V244.21

程涵;张鑫华;余莉;陈猛. Study of velocity effects on parachute inflation performance based on fluid-structure interaction method[J]. Applied Mathematics and Mechanics (English Edition), 2014, 35(9): 1177-1188.

Han CHENG;Xin-hua ZHANG;Li YU;Meng CHEN. Study of velocity effects on parachute inflation performance based on fluid-structure interaction method[J]. Applied Mathematics and Mechanics (English Edition), 2014, 35(9): 1177-1188.

参考文献

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Study of velocity effects on parachute inflation performance based on fluid-structure interaction method

Study of velocity effects on parachute inflation performance based on fluid-structure interaction method

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