The University of Texas at Austin 3 credits Aerospace Engineering
Review of control volume analysis and quasi-one-dimensional compressible flow. Simple propeller theory. Analysis and design of rocket nozzles and air-breathing engines, including performance and cycle analysis; flow in nozzles, diffusers, compressor, and turbine stages; combustion chamber processes and propellants. Includes an introduction to chemical rocket propulsion. Three lecture hours a week for one semester. Pre/Corequisites: Aerospace Engineering 362K with a grade of at least C-.
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