Volume 41 Issue 8
Aug.  2026
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YOU Ruquan, LU Chunyuan, LIU Runzhou, et al. Flow field prediction method integrating residual learning and physics-informed neural network[J]. Journal of Aerospace Power, 2026, 41(8):20250324 doi: 10.13224/j.cnki.jasp.20250324
Citation: YOU Ruquan, LU Chunyuan, LIU Runzhou, et al. Flow field prediction method integrating residual learning and physics-informed neural network[J]. Journal of Aerospace Power, 2026, 41(8):20250324 doi: 10.13224/j.cnki.jasp.20250324

Flow field prediction method integrating residual learning and physics-informed neural network

doi: 10.13224/j.cnki.jasp.20250324
  • Received Date: 2025-07-11
    Available Online: 2026-01-24
  • A high-precision prediction method for flow field was developed by integrating residual neural network (ResNet) with physics-informed neural network (PINN). Based on numerical simulation data, a PINN model integrating residual neural network (Res-PINN) solved the cylinder flow problem. The model used velocity and pressure data from sampled flow-field points to predict flow-field and pressure distributions in different regions. The influences of network type, activation function, dataset size, network layers, number of neurons and loss function weight on the prediction results were also explored. Results demonstrated that the Res-PINN effectively reconstructed flow-field velocity and pressure distributions. Its prediction accuracy was highly consistent with the direct numerical simulation results. The relative error of physical quantities was less than 5%. Comparative analysis showed that compared with traditional PINN, Res-PINN reduced prediction errors by over 45%, significantly improving the prediction accuracy and stability. Furthermore, multiple network hyperparameters had a significant impact on prediction performance, and optimization should be made to comprehensively consider and balance these parameters.

     

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