Structural FEA and Design Optimization of an Aerospace Component

Project Overview

This project involved a comprehensive Finite Element Analysis (FEA) workflow to assess and optimize the structural performance of an aerospace component. The study began by defining material properties and applying relevant boundary conditions, including fixed constraints and distributed loads representing operational forces. Key analyses focused on predicting total deformation and identifying the fundamental modes of vibration. A critical aspect of the methodology was an iterative mesh refinement strategy, systematically improving element quality through techniques like face meshing and localized sizing. Multiple design iterations were evaluated, comparing their structural responses and material efficiency. This work demonstrated a robust FEA process for achieving design improvements, highlighting the impact of mesh quality on solution accuracy and showcasing a systematic approach to structural optimization for enhanced component integrity and performance.