摘要
应用非线性有限元分析的理论,通过MSCDytran软件,对某航天器弹射装置中的缓冲装置进行仿真分析,得到缓冲装置的瞬态冲击下各物理量的分布曲线,初步验证模型的可行性,为今后模型进一步的优化和实验验证提供参考基础.
Applying the theory of non-linear finite element and transient dynamic analysis, the taper bumper device of certain aircraft ejecting device is simulated by MSC Dytran. The interrelated measures are provided within the transient impact. The analysis verifies the feasibility of the bumper and provides the basic for further test and optimization in the future.
出处
《计算机辅助工程》
2006年第B09期9-11,共3页
Computer Aided Engineering
