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Rigid-Flexible Coupling Model and Dynamic Analysis of Rocket Sled

机译:刚性柔性耦合模型及火箭雪橇动力学分析

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The Dynamics Analysis & Simulation of the Rocket Sled were done based on Multibody System Dynamics and Finite Element Analysis Theory. The most difficult work in the analysis was establishing the boundary conditions of the rocket sled. The paper made this kind of attempt. Then the relevant post processing figures and data were obtained, thereby providing the designer and manufacturer with detailed and reliable data. The conclusion is the simulation method is more effective than those before and the boundary conditions is correct and acceptable.
机译:基于多体系系统动态和有限元分析理论,完成了火箭雪橇的动态分析和仿真。分析中最困难的工作是建立火箭雪橇的边界条件。本文制作了这种尝试。然后获得相关的后处理数据和数据,从而为设计者和制造商提供详细和可靠的数据。结论是模拟方法比之前的模拟方法更有效,边界条件是正确可接受的。

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