ME EN 5830 - Aero Propulsion

Institution:

University of Utah

Subject:

Mechanical Engineering

Description:

Introductions to compressible flow and combustion. Analysis of airbreathing propulsion systems including turbojets, turbofans, afterburners, and turboprops and analysis of chemical rocket propulsion systems including solid and liquid engines. Exploration into design considerations for components including inlets, nozzles, combustion chambers, turbines, and compressors. Prerequisites: 'C' or better in (ME EN 2300 OR ME EN 3600 OR ME EN 3610) AND (ME EN 3700 OR ME EN 3710) AND Full Major status in Mechanical Engineering

Credits:

3.00

Credit Hours:

Prerequisites:

Corequisites:

Exclusions:

Level:

Instructional Type:

Lecture

Notes:

Additional Information:

Historical Version(s):

Institution Website:

www.utah.edu

Phone Number:

(801) 581-7200

Regional Accreditation:

Northwest Commission on Colleges and Universities

Calendar System:

Semester

General Education

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