Ramjet Engine Design

https://github.com/z-devin/Ramjet_Engine_Design

Designed a supersonic ramjet engine operating between Mach 2.75-3.25 at 50,000 ft, producing 1,582-5,028 N thrust depending on flight speed.

Built a multi-stage oblique shock inlet to compress incoming air, used Method of Characteristics to design the supersonic nozzle, and modeled heat addition in the combustor with Rayleigh flow.

Analyzed the complete engine using control volume momentum balance and mapped out flow properties (Mach, pressure, temperature) through each component.

Final Project of a Master's Level Rocket Science Independent Study.