Numerical simulation of parachute Fluid-Structure Interaction in terminal descent

被引：8
|
作者：
Cao YiHua [1 ]
Wan Kan [1 ]
Song QianFu [1 ]
Sheridan, John [2 ]
机构：
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
[2] Monash Univ, Dept Mech & Aerosp Engn, Fac Engn, Clayton, Vic 3800, Australia
来源：
SCIENCE CHINA-TECHNOLOGICAL SCIENCES | 2012年 / 55卷 / 11期
基金：
中国国家自然科学基金;
关键词：
parachute; Fluid-Structure Interaction (FSI); Semi-Implicit Method for Pressure-Linked Equations (SIMPLE) algorithm; vortex structure; flowfield topological analysis; SPACE-TIME PROCEDURE; FINITE-ELEMENT; INCOMPRESSIBLE FLOWS; MOVING BOUNDARIES; COMPUTATIONS; WAKE; INTERFACES; CYLINDERS; STRATEGY;
D O I：
10.1007/s11431-012-4998-z
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
A numerical simulation method for parachute Fluid-Structure Interaction (FSI) problem using Semi-Implicit Method for Pressure-Linked Equations (SIMPLE) algorithm is proposed. This method could be used in both coupling computation of parachute FSI and flow field analysis. Both flat circular parachute and conical parachute are modeled and simulated by this new method. Flow field characteristics at various angles of attack are further simulated for the conical parachute model. Comparison with the space-time FSI technique shows that this method also provides similar and reasonable results.
引用
收藏
页码：3131 / 3141
页数：11
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