AE 112 - Aerospace Structural Analysis I

4 units
Aircraft loads, V-n diagram, safety factor; spacecraft boost loads. Stressed-skin wing sections. Shear force and bending moment diagrams for cantilevered wings. Strain gauges. Compression members: wing struts, landing gear, wing/fuselage skin. Shear flow and shear center in wing/tail sections.

Prerequisite(s): MATH 32, PHYS 50 or Graduate Standing
Corequisite(s): MATE 25, ENGR 100W OR Graduate Standing
Grading: Graded

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