Data availability for the work entitled "A simulation-based optimization approach for poultry axial exhaust fans to fulfill aerodynamic and mechanical service constraints".

The following data is provided to replicate the results: NACA-6 and NACA-4 airfoil coordinates (with 5% width fraction), CFD background and volume mesh configuration files, and FEM volume mesh configuration files. Using the NACA-6 airfoil file along with the blade configuration available in Table 8 (Section 5.2) of the manuscript, the 3D parametric model of the blade can be constructed with SALOME or any other CAD software. Subsequently, the CFD and FEM meshes can be constructed with the mesh configuration files provided. The boundary condition information provided in Section 4 of the manuscript can be used to create the CFD and FEM simulations and replicate the results.本数据集提供以下数据以复现研究结果：NACA-6与NACA-4翼型坐标（含5%宽度分数）、计算流体动力学（Computational Fluid Dynamics，CFD）背景与体网格配置文件，以及有限元法（Finite Element Method，FEM）体网格配置文件。 结合本文手稿第5.2节表8中给出的叶片构型，使用NACA-6翼型文件即可通过SALOME或其他任意计算机辅助设计（Computer-Aided Design，CAD）软件构建该叶片的三维参数化模型。随后可依托所提供的网格配置文件生成CFD与FEM网格。 可利用本文手稿第4节中给出的边界条件信息开展CFD与FEM仿真，进而复现相关研究结果。