SE 260A
Aerospace 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: graduate standing.
Sources
- Course catalogue ↗2026-2027