AE 167 - Aerospace Propulsion

3 unit(s)
Basic one-dimensional flows: isentropic, area change, heat addition. Overall performance characteristics of propellers, ramjets, turbojets, turbofans, rockets. Performance analysis of inlets, exhaust nozzles, compressors, burners, and turbines. Rocket flight performance, single-/multi-stage chemical rockets, liquid/solid propellants and design problems.

Prerequisite(s): C or better in AE 164, or graduate standing.
Grading: Letter Graded

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