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| ME 531 - Aerospace Propulsion |
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ME 531 - Gas Turbine Analysis for Engineering
The performance analysis of stationary gas turbine systems and aircraft gas turbine engines. Ideal shaft power gas turbine cycles; cycle losses; the ideal amjet, turbojet, and turbofan engines; aircraft engine losses; diffusers and nozzles; centrifugal and axial flow compressors; axial flow turbines.
Prerequisite(s): ME 530 .
3.000 Credit hours Levels: Undergraduate, Graduate Schedule Types: Lecture Mechanical Engineering Department Course Attributes: College 06 - Fee Assess Restrictions: Must be enrolled in one of the following Levels: Graduate Undergraduate Must be enrolled in one of the following Colleges: College of Eng, Tech and Arch Prerequisites: Undergraduate level ME 530 Minimum Grade of C- or Graduate level ME 530 Minimum Grade of C- |
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