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降落伞流固耦合问题的数值模拟和流场分析
引用本文:王侃,曹义华,于子文,潘星.降落伞流固耦合问题的数值模拟和流场分析[J].北京航空航天大学学报,2007,33(9):1029-1032.
作者姓名:王侃  曹义华  于子文  潘星
作者单位:北京航空航天大学 航空科学与工程学院, 北京 100083
基金项目:国家自然科学基金,航空基础科学基金
摘    要:提出了基于压力耦合的半隐式算法,即SIMPLE (Semi-Implicit Method for Pressure-Linked Equations)算法和生成阶梯网格方法的对稳定下降阶段的降落伞进行数值模拟的新方法.此方法在降落伞流固耦合计算中具有较好的稳定性和较高的效率.对降落伞稳定下降阶段的流固耦合问题进行了数值模拟.降落伞模型分别采用了圆形伞和锥形伞稳定下降时的结构数据,并对锥形伞模型进行了不同来流攻角情形下的模拟.与平行有限元方法相比,采用SIMPLE算法的新方法得到了更准确和更合理的结果.此新方法可以作为传统数值模拟方法的一个可靠替代和重要补充.    

关 键 词:降落伞    流固耦合    数值模拟    流场分析
文章编号:1001-5965(2007)09-1029-04
收稿时间:2006-09-11
修稿时间:2006-09-11

Numerical simulation of parachute fluid-solid coupling problem and flow analysis
Wang Kan,Cao Yihua,Yu Ziwen,Pan Xing.Numerical simulation of parachute fluid-solid coupling problem and flow analysis[J].Journal of Beijing University of Aeronautics and Astronautics,2007,33(9):1029-1032.
Authors:Wang Kan  Cao Yihua  Yu Ziwen  Pan Xing
Institution:School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
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.
Keywords:parachutes  fluid-solid coupling  numerical methods  flow field analysis
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