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REFINEMENT OF A HYPERVELOCITY GOUGING MODEL FOR THE ROCKET SLED TEST

机译:火箭滑动试验的超高速气钻模型的完善

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摘要

In an effort to improve the accuracy of current numerical models of the hypervelocity gouging impact phenomenon at the Holloman Air Force Base High Speed Test Track (HHSTT), several investigations were conducted. First, a metallurgical study of a gouged rail section is summarized that quantifies the nature of the non-equilibrium thermodynamic event. Second, the current CTH model of the sled/rail interaction is scaled mathematically to determine the feasibility of a laboratory experiment to generate gouging. Additionally, the various material contact schemes in CTH are evaluated to determine the most accurate approach in the gouging impact problem. Next, the absence of specific constitutive models for 1080 steel and VascoMax 300 (which are the materials of interest in the HHSTT gouging problem) is addressed with Split Hopkinson Bar characterization. These models are validated by comparison to Taylor Impact Tests conducted on the same materials. Finally, the two coatings used at the HHSTT to mitigate gouging are experimentally compared using the Taylor test. Conclusions are drawn from the experimentation and numerical modeling efforts with regard to the gouging phenomenon.
机译:为了提高Holloman空军基地高速试验场(HHSTT)的超高速气刨冲击现象的当前数值模型的准确性,进行了一些研究。首先,总结了对刨槽截面的冶金研究,以量化非平衡热力学事件的性质。其次,对雪橇/轨道相互作用的当前CTH模型进行数学缩放,以确定实验室实验产生气刨的可行性。此外,对CTH中的各种材料接触方案进行了评估,以确定在气刨冲击问题中最准确的方法。接下来,通过Split Hopkinson Bar表征解决了缺乏针对1080钢和VascoMax 300(这是HHSTT气刨问题中的重要材料)的特定本构模型的问题。通过与在相同材料上进行的泰勒冲击试验进行比较,可以验证这些模型。最后,使用泰勒测试对HHSTT上用于减轻气刨的两种涂料进行了实验比较。从气刨现象的实验和数值建模工作中得出结论。

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