Flexural-torsional buckling tests on beam-columns with sheeting-rail type restraints—II. Compression tests

1974 ◽  
Vol 16 (12) ◽  
pp. 893-912
Author(s):  
J.F. Dooley ◽  
J. Locke
2010 ◽  
Vol 136 (6) ◽  
pp. 787-800 ◽  
Author(s):  
Noël Challamel ◽  
Anísio Andrade ◽  
Dinar Camotim ◽  
Branko M. Milisavlevich

Nanomaterials ◽  
2021 ◽  
Vol 11 (8) ◽  
pp. 1936
Author(s):  
Masoumeh Soltani ◽  
Farzaneh Atoufi ◽  
Foudil Mohri ◽  
Rossana Dimitri ◽  
Francesco Tornabene

This paper addresses the flexural–torsional stability of functionally graded (FG) nonlocal thin-walled beam-columns with a tapered I-section. The material composition is assumed to vary continuously in the longitudinal direction based on a power-law distribution. Possible small-scale effects are included within the formulation according to the Eringen nonlocal elasticity assumptions. The stability equations of the problem and the associated boundary conditions are derived based on the Vlasov thin-walled beam theory and energy method, accounting for the coupled interaction between axial and bending forces. The coupled equilibrium equations are solved numerically by means of the differential quadrature method (DQM) to determine the flexural–torsional buckling loads associated to the selected structural system. A parametric study is performed to check for the influence of some meaningful input parameters, such as the power-law index, the nonlocal parameter, the axial load eccentricity, the mode number and the tapering ratio, on the flexural–torsional buckling load of tapered thin-walled FG nanobeam-columns, whose results could be used as valid benchmarks for further computational validations of similar nanosystems.


2013 ◽  
Vol 353-356 ◽  
pp. 3151-3154
Author(s):  
Jian Qin ◽  
Yong Jun Xia ◽  
Jin Miao Zhang ◽  
Chun Hua Hu

The flexural-torsional buckling of equal-leg angle member under compression is analyzed and calculated. Based on General bending theory and the section properties of angle, the governing equations of the spatial buckling are presented and the formula of Wagner effect coefficient is deduced. The method can also be used for beam-columns with any type section, and the computational efficiency is much higher than numerical methods. The critical buckling loads of equal-leg angle members with different sizes are calculated and the column curves of critical load and slenderness ratio are plotted which will guide efficiently the actual engineering design.


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