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Finite element analysis of large rocket launcher

机译:大火箭发射器的有限元分析

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摘要

By taking a certain type of rocket launcher structure as the research object, its loading analysis was carried out. By applying the ANSYS as a tool and by combining a typical working condition to carry out finite element analysis (FEA), the deformation and the stress values under the work condition were obtained, and the rocket launcher's strength and rigidity were analyzed. The results show that the research is based on the application of finite element software ANSYS calculation method on the launch pad is feasible, cost savings at the same time, the calculation result of finite element analysis can provide a theoretical basis for the subsequent upgrading of equipment.
机译:通过采用某种类型的火箭发射器结构作为研究对象,进行了其装载分析。通过将ANSYS作为工具应用并且通过组合典型的工作条件来执行有限元分析(FEA),获得了工作条件下的变形和应力值,并分析了火箭发射器的强度和刚性。结果表明,该研究基于应用有限元软件的应用ANSYS计算方法在发射垫上是可行的,成本节约同时,有限元分析的计算结果可以为随后的设备提供理论依据。

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