Determining pressure from velocity via physics-informed neural network

被引:0
|
作者
Cai, Zemin [1 ]
Lin, Xiangqi [1 ]
Liu, Tianshu [2 ]
Wu, Fan [3 ,4 ]
Wang, Shizhao [3 ,4 ]
Liu, Yun [5 ]
机构
[1] Shantou Univ, Dept Elect Engn, Shantou, Peoples R China
[2] Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA
[3] Chinese Acad Sci, Inst Mech, LNM, Beijing, Peoples R China
[4] Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China
[5] Purdue Univ Northwest, Dept Mech & Civil Engn, Westville, IN USA
基金
中国国家自然科学基金;
关键词
Pressure; Velocity; PINN; Machine learning; Neural network; Flow; Navier-Stokes equations; FLUID; FLOW; FIELDS; PIV; FORCES;
D O I
10.1016/j.euromechflu.2024.08.007
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper describes a physics-informed neural network (PINN) for determining pressure from velocity where the Navier-Stokes (NS) equations are incorporated as a physical constraint, but the boundary condition is not explicitly imposed. The exact solution of the NS equations for the oblique Hiemenz flow is utilized to evaluate the accuracy of the PINN and the effects of the relevant factors including the boundary condition, data noise, number of collocation points, Reynolds number and impingement angle. In addition, the PINN is evaluated in the twodimensional flow over a NACA0012 airfoil based on computational fluid dynamics (CFD) simulation. Further, the PINN is applied to the velocity data of a flying hawkmoth (Manduca) obtained in high-speed schlieren visualizations, revealing some interesting pressure features associated with the vortex structures generated by the flapping wings. Overall, the PINN offers an alternative solution for the problem of pressure from velocity with the reasonable accuracy and robustness.
引用
收藏
页码:1 / 21
页数:21
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