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Dec 22, 2024
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MAE 4316 - Propulsion3 Credits (Minimum) 3 Credits (Maximum)
Basic concepts of aerospace propulsion. Foundational concepts of thermodynamics, compressible flow, and boundary layer theory. Characteristics, operation and analysis of turbine engines. Characteristics, operation and analysis of rocket engines. Prer., MAE 2301, MATH 3130, MATH 3400; College of Engineering students only.
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