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首页> 外文期刊>Journal of Spacecraft and Rockets >improving Metallic Thermal Protection System Hypervelocity Impact Resistance Through Numerical Simulations
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improving Metallic Thermal Protection System Hypervelocity Impact Resistance Through Numerical Simulations

机译:通过数值模拟改善金属热保护系统的超高速抗冲击性

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摘要

A design of experiments approach has been implemented using computational hypervelocity impact simulations. The purpose of this study is to determine the most effective place to make minor design changes to an existing metallic thermal protection system to improve hypervelocity impact protection provided to underlying components. Simulations are performed using axisymmetric models in a shock-physics hydrodynamics code and compared with existing experimental data. The axisymmetric models are then used in a statistical sensitivity analysis to determine the influence of design parameters on degree of protection. Several damage metrics are identified and evaluated. Damage metrics related to the extent of substructure damage produce misleading results; however, damage metrics related to the degree of dispersion of the hypervelocity projectile produce results that correspond to physical intuition. Based on analysis of variance results, it is concluded that increasing the spacing between the outer surface and the substructure is the most effective way to increase hypervelocity impact resistance. The second most effective design change is to increase the thickness of the outer foil layer. When design considerations are taken into account for the system in this study, it is explained that increasing the thickness of the outer foil layer is the most practical design change.
机译:实验方法的设计已经使用计算超高速冲击模拟来实现。本研究的目的是确定最有效的方法,以对现有的金属热保护系统进行较小的设计更改,以改善对基础组件提供的超高速冲击保护。仿真是在冲击物理流体力学代码中使用轴对称模型进行的,并与现有的实验数据进行了比较。然后,将轴对称模型用于统计敏感性分析中,以确定设计参数对防护等级的影响。确定并评估了几个损坏指标。与子结构损坏程度有关的损坏度量产生误导性结果;但是,与超高速弹丸的分散程度有关的损伤度量会产生与物理直觉相对应的结果。通过对方差结果的分析,可以得出结论,增加外表面和下部结构之间的间距是增加超高速冲击阻力的最有效方法。第二个最有效的设计更改是增加外箔层的厚度。在本研究中,将系统设计考虑在内时,可以解释为增加外箔层的厚度是最实际的设计更改。

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