AE 670 - Aerospace Propulsion III

Institution:

Washburn University

Subject:

Description:

Advanced theory of turbojet, fanjet (multispool), variable cycle engines, ramjet and bypass air breathing propulsion systems. Theory and design of inlets, compressors, burners and turbines. Component matching, cooling, regenerative systems, test methods and corrections. Prerequisite: AE 572. LEC

Credits:

3.00

Credit Hours:

Prerequisites:

Corequisites:

Exclusions:

Level:

Instructional Type:

Lecture

Notes:

Additional Information:

Historical Version(s):

Institution Website:

www.washburn.edu

Phone Number:

(785) 670-1010

Regional Accreditation:

North Central Association of Colleges and Schools

Calendar System:

Semester

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