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SE 260A

Aerospace Structural Mechanics I

4 credits

Aircraft and spacecraft flight loads and operational envelopes, three-dimensional stress/strain relations, metallic and composite materials, failure theories, three-dimensional space trusses and stiffened shear panels, combined extension-bend-twist behavior of thin-walled multicell aircraft and space vehicle structures, modulus-weighted section properties, shear center. Prerequisites: graduate standing.

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