ideal pinned column buckling calculation and equation - engineers edge
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7/27/2019 Ideal Pinned Column Buckling Calculation and Equation - Engineers Edge
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8/8/13 Ideal Pinned Column Buckling Calculation and Equation - Engineers Edge
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Ideal Pinned Column Buckling Equation and Calculation, Euler's Formula
Mechanics of Materials Menu
For the ideal pinned column shown in below, the critical buckling load can be
calculated using Euler's formula:
Open: Ideal Pinned Column Buckling Calculator
Where:
E = Modulus of elasticity of the material
I = Minimum moment of inertia
L = Unsupported length of the column (see picture below)
Note that regardless of the end condition, the critical load depends not on the material
strength, but rather the flexural rigidity, EI. Buckling resistance can be increased by
increasing the moment of inertia.
When a column buckles, it maintains its deflected shape after the application of the
critical load. In most applications, the critical load is usually regarded as the maximum
load sustainable by the column. Theoretically, any buckling mode is possible, but the
column will ordinarily deflect into the first mode. A column will buckle when the load
P reaches a critical level, called the critical load, Pcr .
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7/27/2019 Ideal Pinned Column Buckling Calculation and Equation - Engineers Edge
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8/8/13 Ideal Pinned Column Buckling Calculation and Equation - Engineers Edge
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Ideal Pinned Column (Pinned - Pinned)
For columns with different types of support, Euler's formula may still be used if the
distance L is replaced with the distance between the zero moment points. See
"Effective Length Constant Table" below.
This length is called the effective length Le and is illustrated in below. Thus the critical
load equation becomes:
The slenderness ratio is an important parameter in the classification of compression
members, and is represented by the equation:
Where:
r = Radius of gyration
I = Moment of inertia
A = Area cross section
If the slenderness ratio > (greater than) critical slenderness ratio, then the column is
treated as a long column and the Euler buckling formula is applicable.
If slenderness ratio is < (less than) the critical slenderness ratio, the column is treated
as a short column.
In short columns, failure may occur by compression without significant buckling and at
stresses exceeding the proportional limit. For this condition, Johnson's formula is
applicable:
7/27/2019 Ideal Pinned Column Buckling Calculation and Equation - Engineers Edge
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8/8/13 Ideal Pinned Column Buckling Calculation and Equation - Engineers Edge
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For columns that fail subsequent to the onset of inelastic behavior, the constant of
proportionality must be used rather than the modulus of elasticity (Engesser formula).
The constant of proportionality, Et, is the slope of the stress-strain diagram beyond
the proportional limit, termed the tangent modulus. Note within the linearly elastic
range, E = Et.
Effective Length Constant Table
Column BoundaryEffective Length Constant **
C = Le / L
Free - Free 1.0
Fixed - Free 2.0
Fixed - Pinned .707
Fixed - Guided 1.0
Fixed - Fixed .5
Guide - Free 2.0
Guided - Pinned 2.0
Guided - Guided 1.0
Pinned - Free 1.0
Pinned - Pinned 1.0
** In practice, the Effective Length Constant is increased by a factor approximately
10 - 20 %
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