共 51 条
Comparative assessment for pressure field reconstruction based on physics-informed neural network
被引:13
作者:
Fan, Di
[1
]
Xu, Yang
[1
]
Wang, Hongping
[2
]
Wang, Jinjun
[1
]
机构:
[1] Beijing Univ Aeronaut & Astronaut, Fluid Mech Key Lab Educ Minist, Beijing 100191, Peoples R China
[2] Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China
基金:
中国国家自然科学基金;
关键词:
UNSTEADY;
SPHERE;
FLOW;
PIV;
VELOCITY;
FORCES;
LIFT;
D O I:
10.1063/5.0157753
中图分类号:
O3 [力学];
学科分类号:
08 ;
0801 ;
摘要:
In this paper, a physics-informed neural network (PINN) is used to determine pressure fields from the experimentally measured velocity data. As a novel method of data assimilation, PINN can simultaneously optimize velocity and solve pressure by embedding the Navier-Stokes equations into the loss function. The PINN method is compared with two traditional pressure reconstruction algorithms, i.e., spectral decomposition-based fast pressure integration and irrotation correction on pressure gradient and orthogonal-path integration, and its performance is numerically assessed using two kinds of flow motions, namely, Taylor's decaying vortices and forced isotropic turbulence. In the case of two-dimensional decaying vortices, critical parameters of PINN have been investigated with and without considering measurement errors. Regarding the forced isotropic turbulence, the influence of spatial resolution and out-of-plane motion on pressure reconstruction is assessed. Finally, in an experimental case of a synthetic jet impinging on a solid wall, the PINN is used to determine the pressure from the velocity fields obtained by the planar particle image velocimetry. All results show that the PINN-based pressure reconstruction is superior to other methods even if the velocity fields are significantly contaminated by the measurement errors.
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页数:13
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