SE 260AAerospace Structural Mechanics I
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
From the catalog: “graduate standing.”
Courses that list SE 260A as a prerequisite (1)
- SE 260B Aerospace Structural Mechanics II