3 credits
Spring 2026 Lecture Distance Learning Upper Division
Basic operating principles and analysis of performance characteristics of propulsion systems for air-breathing aerospace vehicles. Ramjet, turbojet, turbofan and turboprop cycle analysis. Propeller analysis and design. Analysis of flow through inlets, combustors, nozzles, compressors, and turbines. Component matching. Not open to students with credit in ME 43800.
Learning Outcomes1Determine the thrust and fuel consumption of gas turbine and turboprop engines.
2Understand advantages/disadvantages of turbojet, turboprop, turbofan, and ramjet air-breathing propulsion systems.
3Understand the thermodynamics of the Brayton cycle and how they contribute to overall propulsion system performance.
4Understand the role and fundamental performance of gas turbine components.
5Determine the basic performance and/or design of axial turbines and compressors.
6Determine the basic performance of air breathing combustors.
Prerequisites
made by Purdue students.