AE 508 - Aerospace Structures II

Institution:

Washburn University

Subject:

Description:

Stress and deflection analysis of aerospace structures using the finite element method. Introduction to work-energy principles, including Castigliano's Theorems, for the analysis of statically indeterminate structures. Rod, beam, shaft, membrane, and plate finite elements. Prerequisite: AE 507. 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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