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| ME 43400 - Gas Turbines For Power And Propulsion |
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Credit Hours: 3.00. Basic operating principles and analysis of performance characteristics of gas turbine engines for aircraft and vehicular propulsion and stationary power. Turbojet, turbofan, turboshaft cycle analysis. Analysis of flow through compressors, turbines, combustors, inlets, nozzles, and regenerators. Component matching and off-design performance. Coursework in thermodynamics and fluid mechanics. Typically offered Spring.
3.000 Credit hours Syllabus Available Levels: Undergraduate, Graduate, Professional Schedule Types: Distance Learning, Lecture Offered By: School of Mechanical Engr Department: Mechanical Engineering Course Attributes: Upper Division May be offered at any of the following campuses: West Lafayette Learning Outcomes: 1. Apply basic performance characteristics of shaft power gas turbin engines. 2. Apply basic performance characteristics of gas turbines for aircraft propulsion. 3. Apply cycle analysis. 4. Apply component performance analysis. 5. Apply design and off-design operation. Prerequisites: Undergraduate level ME 30000 Minimum Grade of D- and Undergraduate level ME 30900 Minimum Grade of D- |
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