Inline Turbojet

Description

This fully student-designed turbojet features a radial compressor, diffuser, turbine, and combustion chamber engineered from the ground up. Using SolidWorks, Ansys, Mathcad, and Starccm+, we’re optimizing for airflow, heat, and stability. We’re also developing custom circuits and microcontroller systems to monitor performance and keep it balanced under real conditions.

Team Members