Buckling loads of linearly tapered columns laterally restrained by multiple elastic springs

2003 ◽  
Vol 7 (3) ◽  
pp. 305-311 ◽  
Author(s):  
Byoung Koo Lee ◽  
Guangfan Li ◽  
Suk Ki Kim ◽  
Dae Soon Ahn
Keyword(s):  
Buckling Loads ◽  
Tapered Columns

Critical Buckling Loads for Tapered Columns

1963 ◽  
Vol 128 (2) ◽  
pp. 736-746
Author(s):  
James M. Gere ◽  
Winifred O. Carter
Keyword(s):  
Buckling Loads ◽  
Tapered Columns

Closure to “Critical Buckling Loads for Tapered Columns”

1963 ◽  
Vol 89 (2) ◽  
pp. 223-224
Author(s):  
James M. Gere ◽  
Winfred O. Carter
Keyword(s):  
Buckling Loads ◽  
Tapered Columns

Discussion of “Critical Buckling Loads for Tapered Columns”

1962 ◽  
Vol 88 (3) ◽  
pp. 343-345
Author(s):  
Larry A. Colbert
Keyword(s):  
Buckling Loads ◽  
Tapered Columns

ELASTICAS AND BUCKLING LOADS OF SHEAR DEFORMABLE TAPERED COLUMNS

2005 ◽  
Vol 05 (03) ◽  
pp. 317-335 ◽  
Author(s):  
BYOUNG KOO LEE ◽  
ATHOL J. CARR ◽  
TAE EUN LEE ◽  
DAE SOON AHN
Keyword(s):  
Differential Equations ◽  
Shear Deformation ◽  
Experimental Studies ◽  
Nonlinear Analyses ◽  
Buckling Loads ◽  
Nonlinear Responses ◽  
Geometrical Nonlinear ◽  
Tapered Columns ◽  
Shear Deformable ◽  
Theoretical Results

This paper deals with the geometrical nonlinear analyses of buckled columns. Differential equations governing the elasticas of buckled columns are derived, in which both the effects of taper type and shear deformation are included. Three kinds of taper types are considered, i.e. breadth, depth and square tapers. Differential equations are solved numerically to obtain the deflection of elasticas and the buckling loads of such columns. Both clamped ends and hinged ends are considered. The effects of shear deformation on the deflection of elasticas of buckled columns and on the buckling loads of columns are investigated extensively. The buckling load equations for uniform columns are expressed as a function of the implicit shear effect. Experimental studies are presented that complement the theoretical results of nonlinear responses of the elasticas.

Discussion of “Critical Buckling Loads for Tapered Columns”

1962 ◽  
Vol 88 (5) ◽  
pp. 185-186
Author(s):  
Donald J. Butler
Keyword(s):  
Buckling Loads ◽  
Tapered Columns

Critical Buckling Loads for Tapered Columns

1962 ◽  
Vol 88 (1) ◽  
pp. 1-12
Author(s):  
James M. Gere ◽  
Winfred O. Carter
Keyword(s):  
Buckling Loads ◽  
Tapered Columns

Stability of tapered columns under end-concentrated and variably distributed follower forces

AIAA Journal ◽  
2002 ◽  
Vol 40 ◽  
pp. 1250-1252
Author(s):  
H. Qiao ◽  
Q. S. Li
Keyword(s):  
Follower Forces ◽  
Tapered Columns

Flexural-Torsional Buckling of Pultruded Fiber-Reinforced Polymer Angle Beams under Eccentric Loading

2020 ◽  
Vol 982 ◽  
pp. 201-206
Author(s):  
Jaksada Thumrongvut ◽  
Natthawat Pakwan ◽  
Samaporn Krathumklang
Keyword(s):  
Buckling Load ◽  
Fiber Reinforced Polymer ◽  
Width Ratio ◽  
Fiber Reinforced ◽  
Torsional Buckling ◽  
Eccentric Load ◽  
Buckling Loads ◽  
Reinforced Polymer ◽  
Cross Sectional Dimension ◽  
Flexural Torsional Buckling

In this paper, the experimental study on the pultruded fiber-reinforced polymer (pultruded FRP) angle beams subjected to transversely eccentric load are presented. A summary of critical buckling load and buckling behavior for full-scale flexure tests with various span-to-width ratios (L/b) and eccentricities are investigated, and typical failure mode are identified. Three-point flexure tests of 50 pultruded FRP angle beams are performed. The E-glass fibre/polyester resin angle specimens are tested to examine the effect of span-to-width ratio of the beams on the buckling responses and critical buckling loads. The angle specimens have the cross-sectional dimension of 76x6.4 mm with span-to-width ratios, ranging from 20 to 40. Also, four different eccentricities are investigated, ranging from 0 to ±2e. Eccentric loads are applied below the horizontal flange in increments until beam buckling occurred. Based upon the results of this study, it is found that the load and mid-span vertical deflection relationships of the angle beams are linear up to the failure. In contrast, the load and mid-span lateral deflection relationships are geometrically nonlinear. The general mode of failure is the flexural-torsional buckling. The eccentrically loaded specimens are failed at critical buckling loads lower than their concentric counterparts. Also, the quantity of eccentricity increases as buckling load decreases. In addition, it is noticed that span-to-width ratio increases, the buckling load is decreased. The eccentric location proved to have considerable influence over the buckling load of the pultruded FRP angle beams.

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