This document outlines a final project presentation for a mechanical engineering student. The project aims to investigate total pressure distortion patterns downstream of a distortion screen and identify the aerodynamic inlet plane ahead of a compressor. The methodology involves obtaining geometric details of an experimental facility, meshing the fluid domain, imposing boundary conditions from experiments, and obtaining flow solutions using simulation software. Results will be validated with experiments. The presentation covers the project objectives, literature review on distorted intake flows, validation studies, simulation design, solution procedure, results and discussions, conclusions, and suggestions for future work.