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A direct random sampling method for the Fourier amplitude sensitivity test of nonuniformly distributed uncertainty inputs and its application in C/C nozzles

机译:非均匀分布不确定性输入的傅立叶振幅灵敏度测试的直接随机采样方法及其在C / C喷嘴中的应用

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摘要

In this paper, the applicability of the conventional random balanced design method for the Fourier amplitude sensitivity test (RBD-FAST) is extended to uncertainty parameters with nonuniform distributions. The latter is a more general premise in real-world applications. The Halton low discrepancy sequence is proposed for direct random sampling (DRS) in RBD-FAST. The correctness of the method is verified with two benchmark problems, i.e., the G function and the flood model. DRS can alleviate the cumbersome mathematical derivation of sampling functions in the conventional FAST, and a higher accuracy level is observed with the DRS-RBD-FAST. The proposed method is employed in the global sensitivity analysis (GSA) of a C/C nozzle where 24 input parameters with normal distributions are considered. The key uncertainties contributing to the transient thermal stress of the C/C nozzle are identified, including the coefficient of thermal expansion, the wall thickness of the nozzle, the coefficient of thermal conductivity, the Poisson's ratios, and Young's moduli. The Poisson's ratios are identified as more sensitive parameters than the Young's moduli, which would not be identified without the higher accuracy level of the proposed DRS method. The proposed method can be used for widespread applications. (C) 2020 Elsevier Masson SAS. All rights reserved.
机译:在本文中,将常规随机平衡设计方法用于傅立叶振幅灵敏度测试(RBD-FAST)的适用性扩展到具有非均匀分布的不确定性参数。后者是实际应用中的更一般的前提。提出将Halton低差异序列用于RBD-FAST中的直接随机采样(DRS)。该方法的正确性通过两个基准问题验证,即G函数和洪水模型。 DRS可以减轻传统FAST中采样函数的繁琐数学推导,并且使用DRS-RBD-FAST可以观察到更高的准确性。该方法用于C / C喷嘴的全局灵敏度分析(GSA),其中考虑了24个具有正态分布的输入参数。确定了导致C / C喷嘴瞬态热应力的关键不确定因素,包括热膨胀系数,喷嘴壁厚,导热系数,泊松比和杨氏模量。泊松比被确定为比杨氏模量更敏感的参数,没有提出的DRS方法的更高准确度,就无法确定泊松比。所提出的方法可以用于广泛的应用。 (C)2020年Elsevier Masson SAS。版权所有。

著录项

  • 来源
    《Aerospace science and technology》 |2020年第5期|105830.1-105830.8|共8页
  • 作者

  • 作者单位

    Harbin Inst Technol Natl Key Lab Sci & Technol Adv Composites Special Harbin 150001 Heilongjiang Peoples R China;

    Harbin Inst Technol Natl Key Lab Sci & Technol Adv Composites Special Harbin 150001 Heilongjiang Peoples R China|Harbin Inst Technol Postdoctoral Res Ctr Mat Sci & Engn Harbin 150001 Heilongjiang Peoples R China;

    THU Inst Flexible Elect Technol Jiaxing Zhejiang Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Global sensitivity analysis; Fourier amplitude sensitivity test; Nonuniform distribution; Sampling; Rocket nozzle;

    机译:全局敏感性分析;傅里叶振幅灵敏度测试;分布不均匀;采样;火箭喷嘴;

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