The goal of the project was to theoretically determine the normal stress and deflection of a pull up bar being subjected to a concentrated load in the middle. We then compared the results to the ones found through our SolidWorks FEA of the same bar. We strengthened our understanding of superposition and the flexure formula, as well as how normal stress and deflection change under load.

Ran FEA on SolidWorks Simulation on a variety of SEDS rocketry components to analyze deformation under high launch stresses.

Highlighted simulations from Atlas internship and Jetson chassis. Performed thermal and deformation FEA to analyze heat management and structural performance, optimizing designs for reliability and efficiency.