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Open Access

Fast prediction of high-speed missile flow field characteristics under transverse jet control based on deep learning

Zhenwei DINGZhenbing LUO( )Qiang LIU( )Yan ZHOUWei XIEZhijie ZHAO
College of Aeronautics and Astronautics, National University of Defense Technology, Changsha 410073, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

The complex flow characteristics of transverse jet in high-speed crossflow involve several separation regions and multiple shock waves, which make it difficult to capture and precisely predict the flow field state in real time merely by relying on traditional approaches. With the rapid advancement of deep learning technology, its powerful data processing capability offers a fast method for the prediction of the transverse jet flow field. Consequently, a prediction model based on deep learning is established, with the aim of obtaining the flow characteristics of a transverse jet under different freestream and jet conditions. This study segments the complex grid into several individual grids and trains them independently. The trained model can successfully establish the nonlinear mapping relationship between the transverse jet flow field and the input parameters. The prediction accuracy of the established model for the wall pressure under different conditions exceeds 99%, and the established model is also capable of reproducing structures such as shock waves and recirculation zones in the overall flow field, thereby achieving highly precise and efficient prediction of the jet structure and flow information. The results suggest that in contrast to the traditional numerical simulation, this deep learning model demonstrates greater efficiency in predicting the transverse jet flow field.

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Chinese Journal of Aeronautics

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Cite this article:
DING Z, LUO Z, LIU Q, et al. Fast prediction of high-speed missile flow field characteristics under transverse jet control based on deep learning. Chinese Journal of Aeronautics, 2025, 38(8). https://doi.org/10.1016/j.cja.2025.103447

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Received: 15 July 2024
Revised: 01 September 2024
Accepted: 08 September 2024
Published: 27 February 2025
© 2025 The Author(s). 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/).