AE 112 - Aerospace Structural Analysis I
Aircraft loads, V-n diagram; spacecraft boost loads. Free-body diagrams, 2-D and 3-D force and moment equilibrium. Centroid and area moment of inertia. Shear force and bending moment diagrams; cantilevered wings & internal support structures; stress/strain relationships; Mohr’s Circle. Experimental strain measurement.
Prerequisite(s): “C” or better in PHYS 50 and (MATH 31 or MATH 31X) or graduate standing.
Grading: Letter Graded
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