Alithea Fernandes
Don Bosco College of Engineering (DBCE), Goa
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Mridul Sharma
Indian Institute of Information Technology (IIIT), Bhopal
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11 Other formulas that you can solve using the same Inputs

Surface Area of a Rectangular Prism
Surface Area=2*(Length*Width+Length*Height+Width*Height) GO
Perimeter of a rectangle when diagonal and length are given
Perimeter=2*(Length+sqrt((Diagonal)^2-(Length)^2)) GO
Magnetic Flux
Magnetic Flux=Magnetic Field*Length*Breadth*cos(θ) GO
Diagonal of a Rectangle when length and area are given
Diagonal=sqrt(((Area)^2/(Length)^2)+(Length)^2) GO
Area of a Rectangle when length and diagonal are given
Area=Length*(sqrt((Diagonal)^2-(Length)^2)) GO
Diagonal of a Rectangle when length and breadth are given
Diagonal=sqrt(Length^2+Breadth^2) GO
Strain
Strain=Change In Length/Length GO
Surface Tension
Surface Tension=Force/Length GO
Perimeter of a rectangle when length and width are given
Perimeter=2*Length+2*Width GO
Volume of a Rectangular Prism
Volume=Width*Height*Length GO
Area of a Rectangle when length and breadth are given
Area=Length*Breadth GO

3 Other formulas that calculate the same Output

Euler's Formula for Critical Buckling Load when Area is Given
Critical Buckling Load=(Coefficient for Column End Conditions*(pi^2)*Modulus Of Elasticity*Cross sectional area)/((Length/Radius of gyration)^2) GO
Elastic Critical Buckling Load
Critical Buckling Load=(pi^2)*Young's Modulus*Cross sectional area/((Coefficient for Column End Conditions*Length/Radius of gyration)^2) GO
Euler's Formula for Critical Buckling Load
Critical Buckling Load=Coefficient for Column End Conditions*(pi^2)*Modulus Of Elasticity*Moment of Inertia/(Length^2) GO

Critical Buckling Load for Pin Ended Columns Formula

Critical Buckling Load=((pi^2)*Modulus of Elasticity of Column*Column Cross-Sectional Area)/((Length/Radius of Gyration of the Column)^2)
P<sub>c=((pi^2)*E*A)/((l/r)^2)
More formulas
Slenderness Ratio of when Critical Buckling Load for Pin Ended Columns is Given GO
Cross-Sectional Area when Critical Buckling Load for Pin Ended Columns is Given GO
Elastic Critical Buckling Load GO
Cross-Sectional Area when Elastic Critical Buckling Load is Given GO
Radius of Gyration of Column when Elastic Critical Buckling Load is Given GO
Torsional Buckling Load for Pin Ended Columns GO
Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given GO
Polar Moment of Inertia for Pin Ended Columns GO
Axial Buckling Load for a Warped Section GO
Cross-Sectional Area when Axial Buckling Load for a Warped Section is Given GO
Polar Moment of Inertia when Axial Buckling Load for a Warped Section is Given GO

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.

How to Calculate Critical Buckling Load for Pin Ended Columns?

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

How to calculate Critical Buckling Load for Pin Ended Columns using this online calculator? To use this online calculator for Critical Buckling Load for Pin Ended Columns, enter Modulus of Elasticity of Column (E), Column Cross-Sectional Area (A), Length (l) and Radius of Gyration of the Column (r) and hit the calculate button. Here is how the Critical Buckling Load for Pin Ended Columns calculation can be explained with given input values -> 0.109662 = ((pi^2)*100000000*1E-05)/((3/0.01)^2).

FAQ

What is Critical Buckling Load for Pin Ended Columns?
The Critical Buckling Load for Pin Ended Columns formula is defined as a function of slenderness ratio, elastic modulus of column and column cross-sectional area and is represented as Pc=((pi^2)*E*A)/((l/r)^2) or Critical Buckling Load=((pi^2)*Modulus of Elasticity of Column*Column Cross-Sectional Area)/((Length/Radius of Gyration of the Column)^2). Modulus of Elasticity of Column is the measure of the column's resistance to being deformed elastically when stress is applied, 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, Length is the measurement or extent of something from end to end and Radius of Gyration of the Column is the distance to a point which would have a moment of inertia the same as the body's actual distribution of mass, if the total mass were concentrated there.
How to calculate Critical Buckling Load for Pin Ended Columns?
The Critical Buckling Load for Pin Ended Columns formula is defined as a function of slenderness ratio, elastic modulus of column and column cross-sectional area is calculated using Critical Buckling Load=((pi^2)*Modulus of Elasticity of Column*Column Cross-Sectional Area)/((Length/Radius of Gyration of the Column)^2). To calculate Critical Buckling Load for Pin Ended Columns, you need Modulus of Elasticity of Column (E), Column Cross-Sectional Area (A), Length (l) and Radius of Gyration of the Column (r). With our tool, you need to enter the respective value for Modulus of Elasticity of Column, Column Cross-Sectional Area, Length and Radius of Gyration of the Column and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Critical Buckling Load?
In this formula, Critical Buckling Load uses Modulus of Elasticity of Column, Column Cross-Sectional Area, Length and Radius of Gyration of the Column. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Critical Buckling Load=Coefficient for Column End Conditions*(pi^2)*Modulus Of Elasticity*Moment of Inertia/(Length^2)
  • Critical Buckling Load=(Coefficient for Column End Conditions*(pi^2)*Modulus Of Elasticity*Cross sectional area)/((Length/Radius of gyration)^2)
  • Critical Buckling Load=(pi^2)*Young's Modulus*Cross sectional area/((Coefficient for Column End Conditions*Length/Radius of gyration)^2)
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