EG 330

Propulsion

This course provides a basic understanding of, and analysis tools for, various aerospace propulsion systems. Students apply the fundamentals of thermodynamics and fluid mechanics to complex propulsion systems. Subjects included are: analysis of various common aircraft propulsion systems with emphasis on jet engines (turbojet, turbofan, and turboprop) and their subsystems (including afterburners and exhaust nozzles). Reciprocating engines (including propeller momentum and blade element theories and propeller efficiency analysis) and rocket engines (both solid and liquid propellants) are covered.

Units: 3.0