1. 电子科技大学 航空航天学院,成都,611731
2. 中国空气动力研究与发展中心 旋翼空气动力学重点实验室,绵阳,621000
冯怡忆(2001—),湖北荆门人,硕士研究生,研究方向:航空智能计算. E-mail:1246093277@qq.com
张书俊*,河南内乡人,副研究员,研究方向:流体力学、飞行器多学科设计优化. E-mail:zhangsj@uestc.edu.cn
纸质出版:2026
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冯怡忆, 刘珊珊, 董守鸿, 等. 基于迁移学习的点云机翼气动性能预测[J]. 空气动力学学报, 2026, 44(2): 50−58.
Feng Yiyi, Liu Shanshan, Dong Shouhong, et al. Research on aerodynamic performance prediction of point cloud wings based on transfer learning[J]. 2026, 44(2): 50-58.
冯怡忆, 刘珊珊, 董守鸿, 等. 基于迁移学习的点云机翼气动性能预测[J]. 空气动力学学报, 2026, 44(2): 50−58. DOI: 10.7638/kqdlxxb-2024.0221
Feng Yiyi, Liu Shanshan, Dong Shouhong, et al. Research on aerodynamic performance prediction of point cloud wings based on transfer learning[J]. 2026, 44(2): 50-58. DOI: 10.7638/kqdlxxb-2024.0221.
当前机翼设计阶段获取大量机翼气动性能需要巨大成本,因此亟需发展一种可以高效且较为准确地获取机翼气动性能数据的方法。以低速双梯形机翼为研究对象,通过OpenVSP和CFD构建低亚声速飞行条件下的机翼数据集,基于此数据集设计了点云机翼气动性能耦合预测网络(PointNet-AP),并利用高低精度数据进行迁移学习。PointNet-AP以机翼点云数据、传统平面特征以及飞行条件为输入,预测机翼对应飞行条件下的 升力系数($C_L$)、阻力系数($C_D$)和俯仰力矩系数($C_m$)。实验结果表明,迁移学习后的PointNet-AP网络模型对机翼气动性能有较好的预测能力,$C_L$、$C_D$和$C_m$的平均相对预测误差分别为2.889%、4.728%和6.743%。本文所提出的预测网络可为后续气动性能预测大模型的开发提供数据特征提取和模型迁移的技术基础。
Acquiring extensive aerodynamic performance data in the current wing design phase incurs substantial costs
necessitating the development of efficient and accurate predictive methods. This study focused on a low-speed double-trapezoid wing. A dataset under subsonic flight conditions was constructed using OpenVSP and CFD simulations. Based on this dataset
a PointNet-based aerodynamic performance prediction network (PointNet-AP) was designed
which incorporated transfer learning utilizing multi-fidelity data. The PointNet-AP network took wing point cloud data
conventional planar geometric features
and flight conditions as inputs to predict the corresponding lift coefficient ($C_L$)
drag coefficient ($C_D$)
and pitching moment coefficient ($C_m$). Experimental results demonstrated that the PointNet-AP model with transfer learning achieved satisfactory predictive performance
with mean relative prediction errors of 2.88%
4.75%
and 6.74% for $C_L$
$C_D$
and $C_m$
respectively.The proposed network provides a technical foundation for developing large-scale aerodynamic performance prediction models by offering solutions for data feature extraction and model transfer.
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