Aircraft Structural Analysis
University of South Alabama
CourseAE 470
Introduction to elasticity. Torsion, bending and shearing of thin-walled skin-stringer structures. Failure mechanisms. Buckling of beams and plates. Introduction to finite element analysis and composite structural analysis.
Credits
3 credits
Course Code
AE 470
Related Courses
Prerequisites, corequisites, and courses that build on this one
Prerequisites
Complete these courses before enrolling