Advanced Search
Volume 33 Issue 09
Sep.  2007
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2007  >  33(09): 1029-1032.
XIAO Yao, LI Yong, LI Dong-sheng, et al. Influence analysis of curing stress and stress relaxation on profile accuracy of carbon fiber reinforced composites tools[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023-0109(in Chinese)
Citation: Wang Kan, Cao Yihua, Yu Ziwen, et al. Numerical simulation of parachute fluid-solid coupling problem and flow analysis[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(09): 1029-1032. (in Chinese)
shu

Numerical simulation of parachute fluid-solid coupling problem and flow analysis

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 11 Sep 2006
  • Publish Date: 30 Sep 2007
    Abstract
  • A new numerical simulation method for predicting parachute fluid-solid coupling problem using semi-implicit method for pressure-linked equations (SIMPLE) algorithm is proposed. The both coupling computation and flow field analysis during terminal descent stage are proved efficient through sample analyses using this new simulation method. The simulations of a flat circle parachute and a cone-shaped parachute suggest a fine efficiency and good stability of the new method. The test problems for the new method are about the terminal descent stage, since the ordinary numerical simulation method(the parallel finite element method) is general used in this field. Comparing with the result gained by the parallel finite element method. The results of the new method are also proved accurate and reasonable. Flow field characteristics at various angles of attack are further simulated for the cone-shaped parachute model. The new method is an alternative and a complement to the ordinary numerical simulation method.

     

    • FullText(HTML)
    • References(1)
  • [1] Stein K R, Benney R, Kalro V, et al. Parallell computation of parachute fluid-structure interactions Proceedings of the 14th AIAA Aerodynamic Decelerator Technology Conference, San Francisco, 1997 [2] Stein K, Benney R, Kalro V, et al. Parachute fluid-structure interactions:3D computation[J]. Computer Methods in Applied Mechanics and Engineering, 2000,190:373-386 [3] Kalro V, Tezduyar T E. A parallel 3D computational method for fluid-structure interactions in parachute systems[J]. Computer Methods in Applied Mechanics and Engineering, 2000, 190:321-332 [4] Patankar S V. Numerical heat transfer and fluid flow[M]. New York:McGraw-Hill, 1980 [5] 朱侣蟾译.平面圆形伞充满时的力、应力和形状的近似计算[J].空降技术, 1983(1) :143- 177 Zhu Lüchan. An approximate approach to calculate drag, stress and deformation of inflated flat circular parachute [J]. Landing Technology, 1983(1):143-177(in Chinese) [6] Tezduyar T E. Finite element methods for flow problems with moving boundaries and interfaces[J]. Archives of Computational Methods in Engineering, 2001, 8:83-130 [7] Kalro V, Tezduyar T E. 3D computation of unsteady flow past a sphere with a parallel finite element method[J]. Oceanographic Literature Review, 1998, 45:602 [8] Tezduyar T E. Computational mechanics in modeling of airdrop systems Proceedings of the Israel Annual Conference on Aerospace Sciences, 2001:21-22 [9] Sahu J, Cooper G, Benney R. 3-D parachute descent analysis using coupled CFD and structural codes . AIAA-95-1580,1995 [10] Tezduyar T E, Behr M, Liou J. A new strategy for finite element computations involving moving boundaries and interfaces-the deforming-spatial-domain/space-time procedure:Ⅰ. the concept and the preliminary tests[J]. Computer Methods in Applied Mechanics and Engineering, 1994,94:339-351
    • Relative Articles

  • Relative Articles

    [1]LI T，ZHAO Y Q，XU T，et al. Stability control of vehicles powered by non-pneumatic wheels based on robust optimal sliding mode[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（4）：1342-1351 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0238.
    [2]WEI J R，WU Q，WU W，et al. Study on global stability of aluminum alloy honeycomb cylinder under axial compression[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（3）：962-972 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0135.
    [3]LYU Y Z，WAN H M，XU Y M. Dynamic stability analysis of a single-point hanging container[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：419-427 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0036.
    [4]WANG C S，ZHANG X Y，ZHAN Z X，et al. Analysis of compression stability and load capacity of thick composite plate structures[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（1）：94-101 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0991.
    [5]WANG F，ZHENG Q，YANG D K，et al. River parameter measurement research by GNSS-reflectometry[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3771-3779 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0912.
    [6]WU M P，LIU Y L，GUO Y，et al. A review of algorithms for multi-vector attitude synthesis of research[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1427-1437 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0325.
    [7]LI Wei, ZHAO Zhigang, ZHAO Xiangtang, LI Zixuan, GANG Zheng. Workspace stability evaluation of multi-engine suspension system based on EWM -TOPSIS[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0546
    [8]CHENG H J，YANG J F，LIU Z H，et al. Rule-based integrated stability control of multi-axle special vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1794-1805 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0569.
    [9]GAN W B，ZUO Z J，XIANG J W，et al. Research progress on dynamic stability of rotating variant wing opening and closing process for aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（4）：1053-1064 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0469.
    [10]WANG C，CHEN W J，CHEN W H，et al. Design of suspension weight-support rehabilitation system adapted to fluctuation of human center of gravity[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（7）：2322-2330 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0605.
    [11]ZHAI J D，LU G Q，CHEN F C. Effect analysis of automation levels on stabilization time of driving behaviors[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3477-3483 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0863.
    [12]YANG Hai-feng, LI Zhi-gang, TAN Yue-dong, XIAO Peng-hui, KONG Wei. Development of Ejection Seat-Dummy Model and Analysis of Seat Tip-off Stability[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0654
    [13]KONG D X，YIN Q Z，SONG J Y，et al. Research on turning directional stability of taxiing with changing speed for high-speed UAV[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3476-3488 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0159.
    [14]WANG W Z，ZHAO R，GUI Y T，et al. Stabilization effects of carbon foam surface on hypersonic boundary layers[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（10）：2741-2749 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0703.
    [15]YANG Jin-hui, WANG Xi-jie, XU Shi-yang, WANG Xiao-li. Study on flame stability of oxygen rich torch igniter[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0528
    [16]WANG X L，XU Y F，XUE Y C. Evaluation and optimization of departure flight schedule stability of airport group[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1331-1341 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0462.
    [17]GAO Yang, XU Guo-ning, WANG Sheng, LI Yong-xiang, CAI Rong, YANG Yan-chu. Stability analysis of stratospheric airship energy system[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0020
    [18]LIU S S，LUO L，HAN Q H，et al. Study on lateral-directional stability of a practical high lift-to-drag ratio hypersonic vehicle with momentum lift augmentation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3010-3021 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0035.
    [19]XIAO Y，CHEN X，YANG L Y，et al. Analysis of radome error on guidance loop stability[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3066-3074 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0780.
    [20]XING Yufeng, JI Yi, ZHANG Huimin. Advances and challenges in time integration methods[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1692-1701. doi: 10.13700/j.bh.1001-5965.2022.0288
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(3435) PDF downloads(1276) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return