基于适当正交分解的热保护系统概率分析参数化降序模型

Kun Zhang, Jianyao Yao, Wenxiang Zhu, Zhifu Cao, Teng Li, Jianqiang Xin
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引用次数: 0

摘要

热保护系统(TPS)是飞行器重返大气层最关键的子系统之一。然而,由于热负荷、材料特性和制造偏差等方面的不确定性,TPS 的热响应表现出显著的随机性,给工程设计和可靠性评估带来了相当大的挑战。鉴于不确定的空气动力热负荷随着时间的推移表现为随机场,通常接受标量随机变量作为输入的传统代用模型在对其建模时面临限制。因此,本文介绍了一种有效的表征方法,利用适当的正交分解(POD)来表示空气动力加热的不确定性。利用增强快照矩阵,通过独立空间和时间基础的解耦方法来降低随机场的维度。描述材料属性和几何厚度的随机变量也被用作概率分析的输入。然后建立了一个非耦合 POD 高斯过程回归(UPOD-GPR)模型,以实现瞬态热传导的高精度求解。该模型将随机热通量场作为输入,将热响应场作为输出。以典型的多层 TPS 和热结构为例,进行了概率分析。典型多层 TPS 的均方相对误差小于 4%。对于热结构,当最大温度达到 1200 ℃ 和 150 ℃ 时,辐射层和隔热层的平均绝对误差分别小于 25 ℃ 和 6 ℃。在输入热通量场和结构参数的情况下,这种方法可以准确、快速地预测 TPS 和热结构在整个工作时间内的热响应。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Parameterized Reduced-Order Models for Probabilistic Analysis of Thermal Protection System Based on Proper Orthogonal Decomposition
The thermal protection system (TPS) represents one of the most critical subsystems for vehicle re-entry. However, due to uncertainties in thermal loads, material properties, and manufacturing deviations, the thermal response of the TPS exhibits significant randomness, posing considerable challenges in engineering design and reliability assessment. Given that uncertain aerodynamic heating loads manifest as a stochastic field over time, conventional surrogate models, typically accepting scalar random variables as inputs, face limitations in modeling them. Consequently, this paper introduces an effective characterization approach utilizing proper orthogonal decomposition (POD) to represent the uncertainties of aerodynamic heating. The augmented snapshots matrix is used to reduce the dimension of the random field by the decoupling method of independently spatial and temporal bases. The random variables describing material properties and geometric thickness are also employed as inputs for probabilistic analyses. An uncoupled POD Gaussian process regression (UPOD-GPR) model is then established to achieve highly accurate solutions for transient heat conduction. The model takes random heat flux fields as inputs and thermal response fields as outputs. Using a typical multi-layer TPS and thermal structure as two examples, probabilistic analyses are conducted. The mean square relative error of a typical multi-layer TPS is less than 4%. For the thermal structure, the averaged absolute error of the radiation and insulation layer is less than 25 ∘C and 6 ∘C when the maximum reaches 1200 ∘C and 150 ∘C, respectively. This approach can provide accurate and rapid predictions of thermal responses for TPS and thermal structures throughout their entire operating time when furnished with input heat flux fields and structural parameters.
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