基于迁移学习的点云机翼气动性能预测

Research on aerodynamic performance prediction of point cloud wings based on transfer learning

  • 摘要: 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2.88%、4.75%和6.74%。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。

     

    Abstract: In the current wing design phase, acquiring extensive aerodynamic performance data of wings incurs substantial costs. To address this challenge, there is an urgent need to develop an efficient and relatively accurate method for obtaining wing aerodynamic performance data. The research focused on a low-speed double-trapezoid wing, establishing a wing dataset under subsonic flight conditions using OpenVSP and CFD simulations. Based on this dataset, a PointNet-based aerodynamic performance prediction network (PointNet-AP) was developed. 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, yielding mean relative errors of 2.88%, 4.75%, and 6.74% for C_L, C_D, and C_m predictions, respectively.In the current stage of wing design, obtaining large amounts of aerodynamic performance data is costly. This study focuses on a low-speed, double-delta wing and constructs a wing dataset for subsonic flight conditions using OpenVSP and CFD. Based on this dataset, a PointNet-based aerodynamic performance prediction network (PointNet-AP) is designed. The network predicts the lift coefficient (C_L), drag coefficient (C_D), and pitching moment coefficient (C_m) for the wing under given flight conditions, using wing point cloud data, traditional geometric features, and flight conditions as inputs. Experimental results show that the PointNet-AP model, after transfer learning, offers good prediction accuracy, with average relative errors of 2.88%, 4.75%, and 6.74% for C_L, C_D, and C_m, respectively. The prediction network proposed in this paper can lay a technical foundation for the development of large-scale aerodynamic performance prediction models by providing capabilities for data feature extraction and model transfer.

     

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