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Open Access

Predicting unsteady hydrodynamic performance of seaplanes based on diffusion models

Xinlong YUaMiao PENGbMingzhen WANGb,c( )Junlong ZHANGaJian YUaHongqiang LYUcXuejun LIUa( )
College of Artificial Intelligence, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China
Key Laboratory of High-Speed Hydrodynamics and Aviation Technology, China Institute of Special Aircraft, Jingmen 448035, China
College of Aeronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

Obtaining unsteady hydrodynamic performance is of great significance for seaplane design. Common methods for obtaining unsteady hydrodynamic performance data include tank test and Computational Fluid Dynamics (CFD) numerical simulation, which are costly and time-consuming. Therefore, it is necessary to obtain unsteady hydrodynamic performance in a low-cost and high-precision manner. Due to the strong nonlinearity, complex data distribution, and temporal characteristics of unsteady hydrodynamic performance, the prediction of it is challenging. This paper proposes a Temporal Convolutional Diffusion Model (TCDM) for predicting the unsteady hydrodynamic performance of seaplanes given design parameters. Under the framework of a classifier-free guided diffusion model, TCDM learns the distribution patterns of unsteady hydrodynamic performance data with the designed denoising module based on temporal convolutional network and captures the temporal features of unsteady hydrodynamic performance data. Using CFD simulation data, the proposed method is compared with the alternative methods to demonstrate its accuracy and generalization. This paper provides a method that enables the rapid and accurate prediction of unsteady hydrodynamic performance data, expecting to shorten the design cycle of seaplanes.

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Chinese Journal of Aeronautics

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Cite this article:
YU X, PENG M, WANG M, et al. Predicting unsteady hydrodynamic performance of seaplanes based on diffusion models. Chinese Journal of Aeronautics, 2025, 38(10). https://doi.org/10.1016/j.cja.2025.103628

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Received: 05 September 2024
Revised: 28 September 2024
Accepted: 23 October 2024
Published: 16 June 2025
© 2025 The Authors. Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).