一种高速激波风洞实验数据与CFD仿真智能同化方法

By constructing a deep reinforcement learning agent to interact with the CFD simulation environment and automatically adjusting the CFD model parameters, the problem of sparse and noisy experimental data for high-speed aircraft is solved, achieving efficient and accurate CFD model assimilation, which is applicable to different wind tunnel equipment and aircraft.

CN122133530BActive Publication Date: 2026-07-17NORTHWESTERN POLYTECHNICAL UNIV

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
NORTHWESTERN POLYTECHNICAL UNIV
Filing Date
2026-05-07
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In existing high-speed aircraft research, experimental time is extremely short, measurement data is sparse and noisy, sensor data is difficult to obtain, and CFD model parameters are difficult to determine. There is a need for a method that can automatically and efficiently solve this problem.

Method used

We construct a deep reinforcement learning agent, extract steady-state features through a temporal adversarial network, build an interactive CFD simulation environment, define a reward function, enable the agent to train interactively with the CFD environment, automatically adjust the CFD model parameters, and achieve data assimilation.

Benefits of technology

It achieves efficient utilization of sparse experimental data, automatically adjusts CFD model parameters, reduces the computational load of traditional methods, provides uncertainty quantification, is applicable to different wind tunnel equipment and aircraft shapes, and improves the accuracy of simulation results.

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Abstract

本发明涉及高速空气动力学、实验流体力学与人工智能交叉技术领域,尤其涉及一种高速激波风洞实验数据与CFD仿真智能同化方法,包括:获取激波风洞实验原始信号,利用时序对抗网络提取稳态特征,获得传感器位置上的实验真值;构建可交互的CFD仿真环境;构建深度强化学习智能体,定义奖励函数;将智能体与CFD环境交互训练,智能体根据当前状态输出动作,CFD环境执行动作并返回新状态和奖励,存储经验并更新网络,直至收敛;固化训练后的智能体,输出最优CFD参数,并对未测量区域进行误差预测及不确定性量化,本发明使仿真结果最大程度复现实验测量值,同时实现未测量区域的流场预测和不确定性量化。
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