| Citation: | Yang Jinheng, Li Yingkun, Wu Yan, et al. Rapid prediction of flow field in rocket engine nozzles based on U-Net[J]. Journal of Aerospace Power, 2026, 41（7）：20250158 doi: 10.13224/j.cnki.jasp.20250158
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A prediction model of the flow field in a rocket engine nozzle based on the U-net architecture was proposed to solve the problem of the time-consuming computation of the flow field in the nozzle using conventional computational fluid dynamics (CFD) methods. By changing the temperature and pressure of the nozzle inlet gas over a certain range,
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