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一种基于任意拉格朗日-欧拉方法的降落伞充气展开数值模型
引用本文:陈晨,郭琪磊.一种基于任意拉格朗日-欧拉方法的降落伞充气展开数值模型[J].科学技术与工程,2021,21(2):801-807.
作者姓名:陈晨  郭琪磊
作者单位:中国民用航空飞行学院,广汉618307;中国民用航空飞行学院,广汉618307
基金项目:四川省教育厅科研项目(APS折叠展开失效机理研究(18ZB0688))
摘    要:降落伞充气展开过程是一个典型时变非线性流构耦合问题,大多研究所建立的数值计算模型未考虑织物透气性和初始投放速度的影响.为修正模型,基于任意拉格朗日-欧拉(arbitrary Lagrange-Euler,ALE)方法和动网格技术,考虑织物透气性并预设初始投放速度,建立了降落伞充气展开的有限元模型.计算了充气过程中,有限质量情况下C-9伞的开伞力,并与实验数据对比,验证了该模型的正确性与合理性.随后分析了其开伞过程中伞衣应力分布特征与气动减速特性,为降落伞数值建模和结构设计提供一定参考.

关 键 词:任意拉格朗日-欧拉  降落伞  充气展开  有限质量
收稿时间:2020/3/22 0:00:00
修稿时间:2020/10/20 0:00:00

A numerical model of parachute deployment inflation process based on ALE method
Chen Chen,Guo Qilei.A numerical model of parachute deployment inflation process based on ALE method[J].Science Technology and Engineering,2021,21(2):801-807.
Authors:Chen Chen  Guo Qilei
Institution:Civil Aviation Flight University of China
Abstract:Parachute inflation-deployment process is a typical time-varying nonlinear fluid-structure coupling problem. The influence of fabric permeability and initial airdrop velocity was ignored in most numerical models. To modify the calculation model, a finite element model of parachute inflation process was established based on ALE (Arbitrary Lagrange Euler) method and dynamic mesh technology, while permeability and initial airdrop speed preseted. The parachute opening load of C-9 canopy was calculated under finite mass condition and compared to experimental data. While the correctness and rationality of the model verified, the stress distribution and aerodynamic deceleration characteristics was analyzed. Which provided some reference for parachute numerical modeling and structural design.
Keywords:ALE      parachute      inflation      finite mass
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