Physics-informed neural networks for low Reynolds number flows over cylinder

Physics-informed neural network (PINN) architectures are recent developments that can act as surrogate models for fluid dynamics in order to reduce computational costs. PINNs make use of deep neural networks, where the Navier-Stokes equation and freestream boundary conditions are used as losses of t...

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Main Authors: Ang, Elijah Hao Wei, Wang, Guangjian, Ng, Bing Feng
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2023
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Online Access:https://hdl.handle.net/10356/171076
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1710762023-10-14T16:48:20Z Physics-informed neural networks for low Reynolds number flows over cylinder Ang, Elijah Hao Wei Wang, Guangjian Ng, Bing Feng School of Mechanical and Aerospace Engineering Engineering::Mechanical engineering Physics-Informed Neural Network Low Reynolds Number Physics-informed neural network (PINN) architectures are recent developments that can act as surrogate models for fluid dynamics in order to reduce computational costs. PINNs make use of deep neural networks, where the Navier-Stokes equation and freestream boundary conditions are used as losses of the neural network; hence, no simulation or experimental data in the training of the PINN is required. Here, the formulation of PINN for fluid dynamics is demonstrated and critical factors influencing the PINN design are discussed through a low Reynolds number flow over a cylinder. The PINN architecture showed the greatest improvement to the accuracy of results from the increase in the number of layers, followed by the increase in the number of points in the point cloud. Increasing the number of nodes per hidden layer brings about the smallest improvement in performance. In general, PINN is much more efficient than computational fluid dynamics (CFD) in terms of memory resource usage, with PINN requiring 5–10 times less memory. The tradeoff for this advantage is that it requires longer computational time, with PINN requiring approximately 3 times more than that of CFD. In essence, this paper demonstrates the direct formulation of PINN without the need for data, alongside hyperparameter design and comparison of computational requirements. Nanyang Technological University National Research Foundation (NRF) Published version This research was funded by Nanyang Technological University, Singapore under the Nanyang President’s Graduate Scholarship, and the Singapore Centre for 3D Printing, which is supported by the National Research Foundation, Prime Minister’s Office, Singapore under its Medium-Sized Centre funding Scheme. 2023-10-11T06:40:43Z 2023-10-11T06:40:43Z 2023 Journal Article Ang, E. H. W., Wang, G. & Ng, B. F. (2023). Physics-informed neural networks for low Reynolds number flows over cylinder. Energies, 16(12), 4558-. https://dx.doi.org/10.3390/en16124558 1996-1073 https://hdl.handle.net/10356/171076 10.3390/en16124558 2-s2.0-85163817679 12 16 4558 en Energies © 2023 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https:// creativecommons.org/licenses/by/ 4.0/). application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Mechanical engineering
Physics-Informed Neural Network
Low Reynolds Number
spellingShingle Engineering::Mechanical engineering
Physics-Informed Neural Network
Low Reynolds Number
Ang, Elijah Hao Wei
Wang, Guangjian
Ng, Bing Feng
Physics-informed neural networks for low Reynolds number flows over cylinder
description Physics-informed neural network (PINN) architectures are recent developments that can act as surrogate models for fluid dynamics in order to reduce computational costs. PINNs make use of deep neural networks, where the Navier-Stokes equation and freestream boundary conditions are used as losses of the neural network; hence, no simulation or experimental data in the training of the PINN is required. Here, the formulation of PINN for fluid dynamics is demonstrated and critical factors influencing the PINN design are discussed through a low Reynolds number flow over a cylinder. The PINN architecture showed the greatest improvement to the accuracy of results from the increase in the number of layers, followed by the increase in the number of points in the point cloud. Increasing the number of nodes per hidden layer brings about the smallest improvement in performance. In general, PINN is much more efficient than computational fluid dynamics (CFD) in terms of memory resource usage, with PINN requiring 5–10 times less memory. The tradeoff for this advantage is that it requires longer computational time, with PINN requiring approximately 3 times more than that of CFD. In essence, this paper demonstrates the direct formulation of PINN without the need for data, alongside hyperparameter design and comparison of computational requirements.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Ang, Elijah Hao Wei
Wang, Guangjian
Ng, Bing Feng
format Article
author Ang, Elijah Hao Wei
Wang, Guangjian
Ng, Bing Feng
author_sort Ang, Elijah Hao Wei
title Physics-informed neural networks for low Reynolds number flows over cylinder
title_short Physics-informed neural networks for low Reynolds number flows over cylinder
title_full Physics-informed neural networks for low Reynolds number flows over cylinder
title_fullStr Physics-informed neural networks for low Reynolds number flows over cylinder
title_full_unstemmed Physics-informed neural networks for low Reynolds number flows over cylinder
title_sort physics-informed neural networks for low reynolds number flows over cylinder
publishDate 2023
url https://hdl.handle.net/10356/171076
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