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中文核心期刊

飞行器热流固耦合数据驱动建模研究进展

RESEARCH PROGRESS IN DATA-DRIVEN MODELING OF THERMAL-FLUID-SOLID COUPLING OF FLIGHT VEHICLE

  • 摘要: 热流固耦合是指飞行过程中流场、温度场与结构场相互作用、动态反馈所形成的复杂多物理场耦合过程, 其研究对于高超声速飞行器、空天往返飞行器及再入返回器的气动布局设计、热防护分析、结构安全评估和轨迹控制具有重要意义. 传统风洞试验、理论分析与高保真数值模拟能够较为准确地刻画相关物理机制, 但在复杂构型、宽域工况和多场强耦合条件下, 仍普遍面临试验成本高、计算周期长、参数覆盖有限以及难以支撑快速迭代与在线应用等问题. 近年来, 数据驱动方法通过融合风洞试验、数值模拟、飞行试验及多源异构数据, 为热流固耦合问题提供了新的建模范式. 现有研究已围绕复杂气动力快速预测、局部气动热高效重构、非线性结构响应建模以及多场耦合条件下的降阶分析与代理建模等关键问题展开探索, 在提高计算效率、增强数据利用能力、支撑快速优化、飞行控制和虚拟试验等方面展现出重要潜力. 现有研究仍以单场预测和跨场映射为主, 同时描述流场、温度场与结构场动态反馈的统一模型较少. 基于此, 本文围绕气动力、气动热和结构响应的数据驱动建模及其向热流固耦合发展的研究, 依次从气动力智能建模、气动热智能建模、结构力学智能建模以及基于数据驱动的热流固耦合应用四个方面, 对相关研究进展、典型方法、关键挑战与发展趋势进行系统梳理, 区分单场代理、跨场映射与反馈耦合模型, 比较其输入输出、数据需求、物理信息利用方式和验证结果, 并讨论多时间尺度、界面守恒、跨场误差传播、长期稳定性及跨工况泛化等问题, 以期为复杂飞行器多物理场耦合建模与智能化分析提供参考.

     

    Abstract: Thermal-fluid-solid coupling refers to a complex multiphysics process involving the mutual interaction and dynamic feedback among the flow field, thermal field, and structural field during flight. It is of great significance to aerodynamic configuration design, thermal protection analysis, structural safety assessment, trajectory optimization, and flight control of hypersonic vehicles, aerospace planes, and reentry vehicles. Traditional approaches, including wind tunnel testing, theoretical analysis, and high-fidelity numerical simulation, can describe the underlying physical mechanisms with relatively high accuracy. However, under complex configurations, wide-range flight conditions, and strongly coupled multiphysics environments, these approaches still suffer from high experimental cost, long computational cycle, limited parameter coverage, and insufficient capability for rapid design iteration and online application. In recent years, data-driven methods have provided a new modeling paradigm for thermal-fluid-solid coupling by integrating wind tunnel data, numerical simulations, flight tests, and multi-source heterogeneous data. Existing studies have explored several key issues, including rapid prediction of complex aerodynamic characteristics, efficient reconstruction of local aerothermal loads, modeling of nonlinear structural responses, and reduced-order or surrogate modeling under multiphysics coupling conditions. These methods have shown great potential in improving computational efficiency, enhancing data utilization, and supporting rapid optimization, flight control, and virtual flight testing. Existing studies still mainly address single-field prediction and cross-field mapping, while unified models describing dynamic feedback among the flow, temperature, and structural fields remain limited. Based on this background, this review focuses on data-driven modeling of aerodynamic, aerothermal, and structural responses and their development toward thermal-fluid-solid coupling and systematically summarizes recent progress, typical methods, key challenges, and future trends from four aspects: intelligent aerodynamic modeling, intelligent aerothermal modeling, intelligent structural mechanics modeling, and data-driven applications of thermal-fluid-solid coupling. It distinguishes single-field surrogates, cross-field mappings, and feedback-coupled models, comparing their inputs and outputs, data requirements, use of physical information, and validation results. It also discusses multiple time scales, interface conservation, cross-field error propagation, long-term stability, and generalization across operating conditions. This review aims to provide a reference for multiphysics coupling modeling and intelligent analysis of complex flight vehicles.

     

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