自编码
翼型
空气动力学
非线性系统
计算机科学
稀疏逼近
算法
跨音速
稀疏矩阵
人工神经网络
流量(数学)
编码器
压缩传感
集合(抽象数据类型)
人工智能
不确定度量化
直升机旋翼
稀疏网格
计算机模拟
模式识别(心理学)
作者
Rui Huang,Zhijie Peng,Xiangjie Yao,Haiyan Hu,Haojie Liu
出处
期刊:AIAA Journal
[American Institute of Aeronautics and Astronautics]
日期:2025-12-02
卷期号:64 (1): 501-518
摘要
Reconstruction of unsteady fluid–structure interaction flows from sparse measurements taken at the interface can facilitate data-driven modeling or real-time control; however, current methods often lead to nonoptimal sparse measurement placement and hinder insights into underlying physics and mechanisms. This paper proposes an embedded methodology whereby a concrete autoencoder is used to simultaneously optimize the sparse measurement placement and the flow reconstruction process. The concrete autoencoder uses a concrete selector layer as an encoder such that a low-dimensional state is indicated by concrete sparse measurements rather than abstract latent variables. The decoder can then be set up with any reasonable neural network depending on the problem of the fluid–structural interaction problem to be solved. The proposed method is applied to the sparse sensing and reconstruction of unsteady pressure distributions for an airfoil and a swept wing. In addition, the data-driven aerodynamic models based on sparse measurements are coupled with the structural models to efficiently predict the problem of transonic aeroelasticity. The numerical results demonstrate that the proposed method outperforms the conventional sparse sensing based on proper orthogonal decomposition.
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