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降落伞充满稳定阶段流场数值模拟
引用本文:刘巍,寇保华,葛健全,杨涛,张晓今,张青斌.降落伞充满稳定阶段流场数值模拟[J].中国空间科学技术,2007,27(1):61-64.
作者姓名:刘巍  寇保华  葛健全  杨涛  张晓今  张青斌
作者单位:国防科学技术大学航天与材料工程学院,长沙410073
摘    要:降落伞系统具有非常复杂的动力学特性,为了较精确的计算降落伞气动力,深入研究其流场特性,采用计算流体动力学方法,对某试验用降落伞充满稳定阶段流场进行数值模拟,计算结果与试验数据吻合较好,表明该数值模型可靠,具有较高精度。

关 键 词:计算流体动力学  数值模拟  降落伞
修稿时间:2005-12-26

Numerical Simulation of Flow Field of the Parachute Fully Developed
Liu Wei,Kou Baohua,Ge Jianquan,Yang Tao,Zhang Xiaojin,Zhang Qingbin.Numerical Simulation of Flow Field of the Parachute Fully Developed[J].Chinese Space Science and Technology,2007,27(1):61-64.
Authors:Liu Wei  Kou Baohua  Ge Jianquan  Yang Tao  Zhang Xiaojin  Zhang Qingbin
Institution:College of Aerospace and Material Engineering, NUDT, Changsha 410073
Abstract:The dynamic behavior of parachute system is an extremely complex phenomenon.By applying the Computational Fluid Dynamics(CFD),the flow field of the parachute fully developed is computed based on the three dimension Navier-Stodes equations closed with S-A turbulence model.The simulation results are agreement with the experiment dates,which verifies that the accuracy of the numerical simulation model is ensured.The methods used in this paper can also be used in the design of other parachute systems.
Keywords:Computational fluid dynamics Numerical simulation Parachute
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