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MECH 590 - Aerospace Propulsion

Description
Aspects of one-dimensional compressible flow, including isentropic flow and normal shocks; effects of friction and combustion; analysis and design of and air-breathing and rocket engines, including performance and cycle analysis; flow in nozzles, diffusers, compressors, and turbines; combustion chamber processes and propellants.
Credits
3
Attributes
Taught 1n Person Only, Lecture, Primary Course
Recent Professors
Open Seat Checker
Schedule Planner
Recent Semesters
Fall 2021, Fall 2020, Fall 2019
Offered
MWF
Avg. Class Size
49
Avg. Sections
1