The second part of a two course series (see AA240A for the first part) on the analysis of aircraft structures with an emphasis on computational methods as well as failure of materials and structures. These techniques and others covered are essential for the structure design and sizing of aeronautical products.
Acquire basic knowledge and experience with light-weight aerospace structures and apply these skills broadly to the creation of a stable and functional aircraft.
- Debbie Senesky Assistant Professor, Aeronautics and Astronautics
- Introduction to the finite element method (FEM)
- Energy methods
- Structural buckling
- Plasticity and fracture
- Commercial FEM software and additive manufacturing (3D printing)
Note on Course Availability
The course schedule is displayed for planning purposes – courses can be modified, changed, or cancelled. Course availability will be considered finalized on the first day of open enrollment. For quarterly enrollment dates, please refer to our graduate certificate homepage.
Analysis of Structures (Stanford Course: AA240A) or consent of instructor. Students should be familiar with the basic mechanics of materials.