Torsion formulas: Difference between revisions
Jump to navigation
Jump to search
(Created page with '== Torsion of Solid Sections == == Torsion of Closed Thin-Walled Sections == Shear stress due to torsion in a thin-walled noncircular shell can be calculated as follows (Lindeb…') |
m (Text replacement - "<tex>" to "<math>") |
||
| Line 5: | Line 5: | ||
Shear stress due to torsion in a thin-walled noncircular shell can be calculated as follows (Lindeburg 2003): | Shear stress due to torsion in a thin-walled noncircular shell can be calculated as follows (Lindeburg 2003): | ||
< | <math>\tau = \frac{T}{2At}</tex> | ||
where | where | ||
* < | * <math>\tau</tex> ... shear stress | ||
* < | * <math>T</tex> ... applied torsion | ||
* < | * <math>A</tex> ... area enclosed by the centerline of the shell | ||
* < | * <math>t</tex> ... sheel thickness | ||
== Torsion of Open Thin-Walled Sections == | == Torsion of Open Thin-Walled Sections == | ||
{{Torsion}} | {{Torsion}} | ||
Revision as of 02:13, 22 October 2024
Torsion of Solid Sections
Torsion of Closed Thin-Walled Sections
Shear stress due to torsion in a thin-walled noncircular shell can be calculated as follows (Lindeburg 2003):
<math>\tau = \frac{T}{2At}</tex>
where
- <math>\tau</tex> ... shear stress
- <math>T</tex> ... applied torsion
- <math>A</tex> ... area enclosed by the centerline of the shell
- <math>t</tex> ... sheel thickness
Torsion of Open Thin-Walled Sections
| Home > Topics > Traditional Analysis Methods > Torsion e | |
| Overview | Torsion · Saint Venant torsion theory · Vlasov torsion theory · Torsion formulas |
| Topics | Warping · Bimoment |