Critical Buckling Load for Pin Ended Columns by Euler's Formula Calculator

✖The Modulus of Elasticity is the measure of the stiffness of a material. It is the slope of stress and strain diagram up to the limit of proportionality.ⓘ Modulus of Elasticity [E]			+10% -10%
✖Column Cross-Sectional Area is the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to some specified axis at a point.ⓘ Column Cross-Sectional Area [A]			+10% -10%
✖The Effective Length of Column can be defined as the length of an equivalent pin-ended column having the same load-carrying capacity as the member under consideration.ⓘ Effective Length of Column [L]			+10% -10%
✖The Radius of Gyration of Column about the axis of rotation is defined as the radial distance to a point which would have a moment of inertia the same as the body's actual distribution of mass.ⓘ Radius of Gyration of Column [r_gyration]			+10% -10%

✖The Buckling Load is the load at which the column starts buckling. The buckling load of a given material depends on the Slenderness ratio, Area of a cross-section, and Modulus of Elasticity.ⓘ Critical Buckling Load for Pin Ended Columns by Euler's Formula [P_{Buckling Load}]

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Critical Buckling Load for Pin Ended Columns by Euler's Formula Solution

STEP 0: Pre-Calculation Summary

Formula Used

Buckling Load = (pi^2*Modulus of Elasticity*Column Cross-Sectional Area)/((Effective Length of Column/Radius of Gyration of Column)^2)
P_{Buckling Load} = (pi^2*E*A)/((L/r_gyration)^2)
This formula uses 1 Constants, 5 Variables

Constants Used

pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288

Variables Used

Buckling Load - (Measured in Newton) - The Buckling Load is the load at which the column starts buckling. The buckling load of a given material depends on the Slenderness ratio, Area of a cross-section, and Modulus of Elasticity.
Modulus of Elasticity - (Measured in Megapascal) - The Modulus of Elasticity is the measure of the stiffness of a material. It is the slope of stress and strain diagram up to the limit of proportionality.
Column Cross-Sectional Area - (Measured in Square Millimeter) - Column Cross-Sectional Area is the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to some specified axis at a point.
Effective Length of Column - (Measured in Millimeter) - The Effective Length of Column can be defined as the length of an equivalent pin-ended column having the same load-carrying capacity as the member under consideration.
Radius of Gyration of Column - (Measured in Millimeter) - The Radius of Gyration of Column about the axis of rotation is defined as the radial distance to a point which would have a moment of inertia the same as the body's actual distribution of mass.

STEP 1: Convert Input(s) to Base Unit

Modulus of Elasticity: 50 Megapascal --> 50 Megapascal No Conversion Required
Column Cross-Sectional Area: 700 Square Millimeter --> 700 Square Millimeter No Conversion Required
Effective Length of Column: 3000 Millimeter --> 3000 Millimeter No Conversion Required
Radius of Gyration of Column: 26 Millimeter --> 26 Millimeter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

P_{Buckling Load} = (pi^2*E*A)/((L/r_gyration)^2) --> (pi^2*50*700)/((3000/26)^2)

Evaluating ... ...

P_{Buckling Load} = 25.9460933477527

STEP 3: Convert Result to Output's Unit

25.9460933477527 Newton --> No Conversion Required

FINAL ANSWER

25.9460933477527 ≈ 25.94609 Newton <-- Buckling Load

(Calculation completed in 00.020 seconds)

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Home » Engineering » Civil » Columns » Elastic Flexural Buckling of Columns » Pin Ended Columns » Critical Buckling Load for Pin Ended Columns by Euler's Formula

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Created by Alithea Fernandes

Don Bosco College of Engineering (DBCE), Goa

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< Pin Ended Columns Calculators

Radius of Gyration given Critical Buckling Load for Pin Ended Columns by Euler's Formula

LaTeX Go Radius of Gyration of Column = sqrt((Buckling Load*Effective Length of Column^2)/(pi^2*Modulus of Elasticity*Column Cross-Sectional Area))

Cross-Sectional Area given Critical Buckling Load for Pin Ended Columns by Euler's Formula

LaTeX Go Column Cross-Sectional Area = (Buckling Load*(Effective Length of Column/Radius of Gyration of Column)^2)/(pi^2*Modulus of Elasticity)

Critical Buckling Load for Pin Ended Columns by Euler's Formula

LaTeX Go Buckling Load = (pi^2*Modulus of Elasticity*Column Cross-Sectional Area)/((Effective Length of Column/Radius of Gyration of Column)^2)

Slenderness Ratio given Critical Buckling Load for Pin Ended Columns by Euler's Formula

LaTeX Go Slenderness Ratio = sqrt((pi^2*Modulus of Elasticity*Column Cross-Sectional Area)/Buckling Load)

Critical Buckling Load for Pin Ended Columns by Euler's Formula Formula

LaTeX Go

Buckling Load = (pi^2*Modulus of Elasticity*Column Cross-Sectional Area)/((Effective Length of Column/Radius of Gyration of Column)^2)
P_{Buckling Load} = (pi^2*E*A)/((L/r_gyration)^2)

What is Critical Buckling Load?

Buckling is a sudden lateral failure of an axially loaded member in compression, under a load value less than the compressive load-carrying capacity of that member. The axial compression load corresponding to this mode of failure is referred to as critical buckling load.

What does Buckling mean?

In structural engineering, buckling is the sudden change in shape (deformation) of a structural component under load, such as the bowing of a column under compression or the wrinkling of a plate under shear.

How to Calculate Critical Buckling Load for Pin Ended Columns by Euler's Formula?

Critical Buckling Load for Pin Ended Columns by Euler's Formula calculator uses Buckling Load = (pi^2*Modulus of Elasticity*Column Cross-Sectional Area)/((Effective Length of Column/Radius of Gyration of Column)^2) to calculate the Buckling Load, The Critical Buckling Load for Pin Ended Columns by Euler's Formula formula is defined as a function of slenderness ratio, elastic modulus of column and column cross-sectional area. Buckling Load is denoted by P_{Buckling Load} symbol.

How to calculate Critical Buckling Load for Pin Ended Columns by Euler's Formula using this online calculator? To use this online calculator for Critical Buckling Load for Pin Ended Columns by Euler's Formula, enter Modulus of Elasticity (E), Column Cross-Sectional Area (A), Effective Length of Column (L) & Radius of Gyration of Column (r_gyration) and hit the calculate button. Here is how the Critical Buckling Load for Pin Ended Columns by Euler's Formula calculation can be explained with given input values -> 2.6E+7 = (pi^2*50000000*0.0007)/((3/0.026)^2).

FAQ

What is Critical Buckling Load for Pin Ended Columns by Euler's Formula?

The Critical Buckling Load for Pin Ended Columns by Euler's Formula formula is defined as a function of slenderness ratio, elastic modulus of column and column cross-sectional area and is represented as P_{Buckling Load} = (pi^2*E*A)/((L/r_gyration)^2) or Buckling Load = (pi^2*Modulus of Elasticity*Column Cross-Sectional Area)/((Effective Length of Column/Radius of Gyration of Column)^2). The Modulus of Elasticity is the measure of the stiffness of a material. It is the slope of stress and strain diagram up to the limit of proportionality, Column Cross-Sectional Area is the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to some specified axis at a point, The Effective Length of Column can be defined as the length of an equivalent pin-ended column having the same load-carrying capacity as the member under consideration & The Radius of Gyration of Column about the axis of rotation is defined as the radial distance to a point which would have a moment of inertia the same as the body's actual distribution of mass.

How to calculate Critical Buckling Load for Pin Ended Columns by Euler's Formula?

The Critical Buckling Load for Pin Ended Columns by Euler's Formula formula is defined as a function of slenderness ratio, elastic modulus of column and column cross-sectional area is calculated using Buckling Load = (pi^2*Modulus of Elasticity*Column Cross-Sectional Area)/((Effective Length of Column/Radius of Gyration of Column)^2). To calculate Critical Buckling Load for Pin Ended Columns by Euler's Formula, you need Modulus of Elasticity (E), Column Cross-Sectional Area (A), Effective Length of Column (L) & Radius of Gyration of Column (r_gyration). With our tool, you need to enter the respective value for Modulus of Elasticity, Column Cross-Sectional Area, Effective Length of Column & Radius of Gyration of Column and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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