NASA - Mech.E. Senior Capstone

Below is our proposed URI's NASA 21H Proof of Concept models from design, analysis and to experiments.
We plan on finalizing a full scaled model to accurately meet our criteria and outcomes for Spring 2024.

Introduction: Proof of Concept, led by myself . Working on reaching our 7k RPM goal, using a windtunnel at half scaled turbine and engine geometry.