Stress Analysis II: L-18 Stability - Crippling of Thin-Flanged Sections

This video explains how to evaluate crippling for a thin-flanged sections.

This is perhaps the most common failure mode in lightweight structures such as aircraft, therefore it is critical that aerospace, mechanical and civil engineers master these concepts.

Be sure to systematically review the following stability topics in order:
- L-17 Buckling of Columns
- L-17 Buckling of Flat Plates
- L-18 Crippling of Thin-Flanged sections
- L-19 Effective Sheet Widths & Inter-Rivet Buckling
- L-20 Euler Johnson's Equation
- L-21 Buckling of Cylinders
- L-22 Buckling of Curved Panels

By Dr. Todd Coburn
Recorded: 07 April 2021.

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Enjoy.

Keywords:
##stability #stabilityofflatplates #stabilityofcolumns #buckling #bucklingopfflatplates
#bifurcation #flatplates #euler #criticalload