Physics-Informed Neural Network for Solving a One-Dimensional Solid Mechanics Problem

Our objective in this work is to demonstrate how physics-informed neural networks, a type of deep learning technology, can be utilized to examine the mechanical properties of a helicopter blade. The blade is regarded as a one-dimensional prismatic cantilever beam that is exposed to triangular loading, and comprehending its mechanical behavior is of utmost importance in the aerospace field. PINNs utilize the physical information, including differential equations and boundary conditions, within the loss function of the neural network to approximate the solution. Our approach determines the overall loss by aggregating the losses from the differential equation, boundary conditions, and data. We employed a physics-informed neural network (PINN) and an artificial neural network (ANN) with equivalent hyperparameters to solve a fourth-order differential equation. By comparing the performance of the PINN model against the analytical solution of the equation and the results obtained from the ANN model, we have conclusively shown that the PINN model exhibits superior accuracy, robustness, and computational efficiency when addressing high-order differential equations that govern physics-based problems. In conclusion, the study demonstrates that PINN offers a superior alternative for addressing solid mechanics problems with applications in the aerospace industry.

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Publication Details

Journal
Modelling—International Open Access Journal of Modelling in Engineering Science
Published
2024-10-18
DOI
https://doi.org/10.3390/modelling5040080
Citations
15
Primary Topic
Model Reduction and Neural Networks
Type
article
Field-Weighted Citation Impact
4.22

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Physics-Informed Neural Network for Solving a One-Dimensional Solid Mechanics Problem

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15 citations
Modelling—International Open Access Journal of Modelling in Engineering Science
Model Reduction and Neural Networks
4.22
article

Physics-Informed Neural Network for Solving a One-Dimensional Solid Mechanics Problem

Dineshkumar Harursampath, Sahaj Saxena, Rajnish Mallick, Manoj Sahni, Sharanjeet Dhawan, Vishal Singh
article en
15 citations

Abstract

Our objective in this work is to demonstrate how physics-informed neural networks, a type of deep learning technology, can be utilized to examine the mechanical properties of a helicopter blade. The blade is regarded as a one-dimensional prismatic cantilever beam that is exposed to triangular loading, and comprehending its mechanical behavior is of utmost importance in the aerospace field. PINNs utilize the physical information, including differential equations and boundary conditions, within the loss function of the neural network to approximate the solution. Our approach determines the overall loss by aggregating the losses from the differential equation, boundary conditions, and data. We employed a physics-informed neural network (PINN) and an artificial neural network (ANN) with equivalent hyperparameters to solve a fourth-order differential equation. By comparing the performance of the PINN model against the analytical solution of the equation and the results obtained from the ANN model, we have conclusively shown that the PINN model exhibits superior accuracy, robustness, and computational efficiency when addressing high-order differential equations that govern physics-based problems. In conclusion, the study demonstrates that PINN offers a superior alternative for addressing solid mechanics problems with applications in the aerospace industry.

Modelling—International Open Access Journal of Modelling in Engineering ScienceVol. 5(4)
Thapar Institute of Engineering & Technology (IN), Chaudhary Charan Singh Haryana Agricultural University (IN), Pandit Deendayal Energy University (IN), Indian Institute of Science Bangalore (IN)
Arthritis National Research Foundation, National Research Foundation, Department of Science and Technology, Ministry of Science and Technology, India, Science and Engineering Research Board
Industry, innovation and infrastructure
Openalex Percentile: Top 5%
Model Reduction and Neural Networks
4.22
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