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Nov 04, 2024
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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 160 and AE 164 . Allowed Declared Majors: Engineering, Aerospace Engineering, Mechanical Engineering. Grading: Letter Graded
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