3 credits
Fall 2026 Distance Learning Lecture Upper Division
This course applies the foundational principles of thermodynamics, heat transfer, and fluid mechanics to propulsion systems. Students will develop a deeper understanding of these fundamental concepts as they are applied to both airbreathing and rocket propulsion systems.
Learning Outcomes1Model isentropic flow, normal shock waves, and flow with heat addition or friction, particularly in the context of inlets, nozzles, and combustors.
2Calculate adiabatic flame temperatures, analyze equilibrium combustion using chemical equilibrium constants, and explain the role of combustion in both airbreathing and rocket engines.
3Apply thermodynamic principles such as enthalpy and isentropic efficiency to analyze system performance of turbojets, turbofans, ramjets, and turboprops engines.
4Model the performance of solid and liquid rocket engines using simplified models.
5Use principles of conduction and convection to analyze thermal problems related to propulsion systems.
Prerequisites
Restrictions
GPA by professor
made by Purdue students.