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AE 112

Aerospace Structural Analysis I

Description
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. Prerequisites: MATH 32, PHYS 50 or Graduate Standing Corequisites: MatE 25, Engr 100W OR Graduate Standing

Grading
Normal Grade Rules

Units
4