A method for the closed-form evaluation of critical buckling loads for planar strongly curved bars (Q1067842)
From MaRDI portal
| This is the item page for this Wikibase entity, intended for internal use and editing purposes. Please use this page instead for the normal view: A method for the closed-form evaluation of critical buckling loads for planar strongly curved bars |
scientific article; zbMATH DE number 3930465
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | A method for the closed-form evaluation of critical buckling loads for planar strongly curved bars |
scientific article; zbMATH DE number 3930465 |
Statements
A method for the closed-form evaluation of critical buckling loads for planar strongly curved bars (English)
0 references
1985
0 references
The calculation of critical buckling loads of planar curved bars, subjected to a general co-planar continuous external load (or a general co-planar terminal loading), leads to the solution of transcendental (nonlinear) equations. In this investigation a new method for the closed- form solution of such types of equations is presented. In particular, the transcendental equation \(u \tan \gamma \cot u \gamma =1\), corresponding to the buckling problem of a cantilever circular bar of high curvature loaded by two co-planar forces acting along its chord, is solved in a closed-form. Finally, several numerical results are presented, based on the Gauss integration rule.
0 references
critical buckling loads
0 references
planar curved bars
0 references
general co-planar continuous external load
0 references
general co-planar terminal loading
0 references
transcendental (nonlinear) equations
0 references
closed-form solution
0 references
u tan \(\gamma \) cot u\(\gamma \) \(=1,\)
0 references
cantilever circular bar
0 references
high curvature
0 references
loaded by two co-planar forces
0 references
Gauss integration rule
0 references
0.8544705
0 references
0.8517628
0 references
0.84409004
0 references
0.8434732
0 references
0.84297705
0 references
0.8406111
0 references
0.8391676
0 references