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

Description

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.

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