3 credits
Spring 2026 Lecture Distance Learning Upper DivisionData from last updated 2/24/2026
Spring 2026
Spring 2026 Instructors: ,
This course introduces aerospace engineering students to properties of wing and fuselage sections, basic concepts in elasticity, torsion of single and multi-cell thin-walled and skin stringer sections, bending and flexural shear in open and closed thin-walled and skin-stringer sections, flexural shear flow in thin-walled sections, and failure criteria for isotropic materials.
Learning Outcomes1Predict the distribution of load (or displacement) in typical aerospace components using analytical and/or empirical tools.
2Implement the procedures for relating applied loads (or displacements) to component "failure."
3Select materials to resist structural failure.
Prerequisites
GPA by professor
Wate...(Summer 2019)
Vika...(Fall 2019)
Jame...(Spring 2019)
Hash...(Fall 2021)
Kawa...(Fall 2024)
Wenb...(Fall 2023)
Lisa...(Spring 2019)
No grades available
Juli...(Spring 2019)
No grades available
Goon...(Spring 2020)
No grades available
Jame...(Fall 2021)
No grades available
Kare...(Fall 2023)
No grades available
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