The aim of the project:
1) To develop and implement URANS/VLES-based high-fidelity concurrent aerodynamic design optimization
2) To develop and implement the discrete 2-way FSI based on ALE and OM methods and VLES for the concurrent transient design optimization
3) To develop and implement 3H (high disciplinary, fidelity and dimensionality) concurrent transient multidisciplinary design optimization.
4) This project aims to evaluate the impact of the optimization of the blade design on the performance and structural integrity by analyzing the fluid-structure interaction of HAWTs, specifically focusing on NREL 5MW and NREL Phase VI.