ENGR 3613 - Aero Propulsion

Credits: 3

The course covers airbreathing, rocket propulsion systems, one-dimensional compressible internal flows; cycle and performance analysis of ramjets, turbojets, and turbofans; propellers; reacting flows and chemical equilibrium, main components of gas turbine engines and rockets, including inlets, turbomachinery, thrust chambers, and nozzles.

Prerequisites: ENGR 3603