用多网格分层学习加速大型飞机三维流场模拟,提升效率3至8倍。
Full-field prediction for engineering-scale three-dimensional aircraft with multigrid-hierarchical learning

- 构建多网格分层框架,捕捉不同区域流场差异。
- 在马赫数0.15至6.0下实现3至8倍收敛加速。
- 适合需要高保真三维流场预测的航空设计工程师。
高保真计算流体力学对航空航天设计至关重要,但实际三维飞机的工程规模模拟仍计算成本高昂。基于学习的流场初始化可减少初始解与收敛解之间的数值距离,提升效率,然而现有深度学习方法难以扩展到具有多尺度区域异质性的大尺寸三维飞机流动。多数先前研究集中于二维问题、表面量或简化三维案例,且网格分辨率有限。本文提出MHLF——一种用于加速工程级飞机流场模拟的多网格分层学习框架,结合拓扑一致的几何多网格表示与分层策略,同时捕捉预测与后续CFD修正中的区域流场异质性。在三个涵盖马赫数0.15至6.0、覆盖亚音速、跨音速和超音速状态的工程级飞机案例中,MHLF在不牺牲流场精度的前提下实现收敛加速,相比传统初始化提升3至8倍效率。结果证明了在CFD领域内对大型三维飞机实现完整流场预测的可行性,并为高保真飞机流场模拟的数据驱动加速提供了基础。
原文摘要 · Abstract (English)
High-fidelity computational fluid dynamics is essential for aerospace design, but engineering-scale simulations of practical three-dimensional aircraft remain computationally expensive. Learning-based flow-field initialization can improve efficiency by reducing the numerical distance between the initial and converged solutions, yet existing deep learning approaches remain difficult to scale to large three-dimensional aircraft flows with multiscale regional heterogeneity. Most prior studies therefore focus on two-dimensional problems, surface quantities, integral aerodynamic coefficients, or simplified three-dimensional cases with limited grid resolution.Here we propose MHLF, a multigrid-hierarchical learning framework for accelerating engineering-scale aircraft flow simulations while preserving high-fidelity numerical accuracy. MHLF combines a topologically consistent geometric multigrid representation with a hierarchical strategy that captures regional flow heterogeneity during both prediction and subsequent CFD correction. Across three engineering-scale aircraft cases spanning Mach 0.15 to 6.0 and covering subsonic, transonic and supersonic regimes, MHLF accelerates convergence without sacrificing flow-field accuracy, achieving a 3 to 8 times efficiency improvement over conventional initialization. These results demonstrate practical full-flow-field prediction for large three-dimensional aircraft within the CFD domain and provide a foundation for data-driven acceleration of high-fidelity aircraft flow simulation.
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