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MEM 403 Gas Turbines & Jet Propulsion 3.0 Credits

Covers fundamentals of thermodynamics and aerothermodynamics, and application to propulsion engines; thermodynamic cycles and performance analysis of gas turbines and air-breathing propulsion systems, turbojet, turboprop, ducted fan, ramjet, and ducted rocket; theory and design of ramjets, liquid and solid rockets, air-augmented rockets, and hybrid rockets; aerodynamics of flames, including the thermodynamics and kinetics of combustion reactions; supersonic combustion technology and zero-g propulsion problems; and propulsion systems comparison and evaluation for space missions.

College/Department: College of Engineering
Repeat Status: Not repeatable for credit
Prerequisites: MEM 220 [Min Grade: D] and MEM 310 [Min Grade: D]

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