Chandana P Dev
NSS College of Engineering (NSSCE), Palakkad
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Ishita Goyal
Meerut Institute of Engineering and Technology (MIET), Meerut
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11 Other formulas that you can solve using the same Inputs

Torsional Buckling Load for Pin Ended Columns
Torsional buckling load=Shear Modulus of Elasticity*Torsion constant*Cross sectional area/Polar moment of Inertia GO
Strain Energy in Torsion when Angle of Twist is Given
Strain Energy=(Polar moment of Inertia*Shear Modulus of Elasticity*Angle of Twist^2)/(2*Length) GO
Length over which Deformation Takes Place when Strain Energy in Torsion is Given
Length=sqrt(2*Strain Energy*Polar moment of Inertia*Shear Modulus of Elasticity/Torque^2) GO
Polar Moment of Inertia when Strain Energy in Torsion is Given
Polar moment of Inertia=(Torque^2)*Length/(2*Strain Energy*Shear Modulus of Elasticity) GO
Strain Energy in Shear when Shear Deformation is Given
Strain Energy=(Shear Area*Shear Modulus of Elasticity*(Shear Deformation^2))/(2*Length) GO
Torque when Strain Energy in Torsion is Given
Torque=sqrt(2*Strain Energy*Polar moment of Inertia*Shear Modulus of Elasticity/Length) GO
Strain Energy in Torsion
Strain Energy=(Torque^2)*Length/(2*Polar moment of Inertia*Shear Modulus of Elasticity) GO
Shear Load when Strain Energy in Shear is Given
Shear Force=sqrt(2*Strain Energy*Shear Area*Shear Modulus of Elasticity/Length) GO
Shear Area when Strain Energy in Shear is Given
Shear Area=(Shear Force^2)*Length/(2*Strain Energy*Shear Modulus of Elasticity) GO
Strain Energy in Shear
Strain Energy=(Shear Force^2)*Length/(2*Shear Area*Shear Modulus of Elasticity) GO
Length over which Deformation Takes Place when Strain Energy in Shear is Given
Length=2*Strain Energy*Shear Area*Shear Modulus of Elasticity/(Shear Force^2) GO

Beam Buckling Factor 2 Formula

Beam buckling factor 2=(4*Warping Constant/Moment of Inertia about Y-axis)*((Section modulus about major axis)/(Shear Modulus of Elasticity*Torsional constant))^2
X<sub>2</sub>=(4*C<sub>w/I<sub>y)*((S<sub>x</sub>)/(G*J))^2
More formulas
Maximum Laterally Unbraced Length for Plastic Analysis GO
Maximum Laterally Unbraced Length for Plastic Analysis in Solid Bars and Box Beams GO
Plastic Moment GO
Limiting Laterally Unbraced Length for Full Plastic Bending Capacity for I and Channel Sections GO
Limiting Laterally Unbraced Length for Full Plastic Bending Capacity for Solid Bar and Box Beams GO
Limiting Laterally Unbraced Length for Inelastic Lateral Buckling GO
Specified Minimum Yield Stress for Web if Lr is Given GO
Beam Buckling Factor 1 GO
Limiting Buckling Moment GO
Limiting Laterally Unbraced Length for Inelastic Lateral Buckling for Box Beams GO
Critical Elastic Moment GO
Critical Elastic Moment for Box Sections and Solid Bars GO

Why is beam buckling factor used?

Since the buckling failure can cause serious catastrophic results, a high factor of safety will be used for design purpose. Here, for calculating the limiting unbraced length two different safety factors are considered, among which one of them is evaluated using the above formula.

How to Calculate Beam Buckling Factor 2?

Beam Buckling Factor 2 calculator uses Beam buckling factor 2=(4*Warping Constant/Moment of Inertia about Y-axis)*((Section modulus about major axis)/(Shear Modulus of Elasticity*Torsional constant))^2 to calculate the Beam buckling factor 2, The Beam Buckling Factor 2 is considered as the safety factor value against buckling failure due to load acting on the member. . Beam buckling factor 2 and is denoted by X2 symbol.

How to calculate Beam Buckling Factor 2 using this online calculator? To use this online calculator for Beam Buckling Factor 2, enter Warping Constant (Cw), Moment of Inertia about Y-axis (Iy), Section modulus about major axis (Sx), Shear Modulus of Elasticity (G) and Torsional constant (J) and hit the calculate button. Here is how the Beam Buckling Factor 2 calculation can be explained with given input values -> 2.000E-21 = (4*10/50)*((5E-08)/(100*10))^2.

FAQ

What is Beam Buckling Factor 2?
The Beam Buckling Factor 2 is considered as the safety factor value against buckling failure due to load acting on the member. and is represented as X2=(4*Cw/Iy)*((Sx)/(G*J))^2 or Beam buckling factor 2=(4*Warping Constant/Moment of Inertia about Y-axis)*((Section modulus about major axis)/(Shear Modulus of Elasticity*Torsional constant))^2. The Warping Constant is often referred to as the warping moment of inertia. It is a quantity derived from a cross-section, Moment of Inertia about Y-axis is defined as the moment of inertia of cross-section about YY, Section modulus about major axis is the ratio between second moment of area to distance from neutral axis to extreme fiber about the major axis. , Shear Modulus of Elasticity is one of the measures of mechanical properties of solids. Other elastic moduli are Young's modulus and bulk modulus and The Torsional constant is a geometrical property of a bar's cross-section which is involved in the relationship between the angle of twist and applied torque along the axis of the bar.
How to calculate Beam Buckling Factor 2?
The Beam Buckling Factor 2 is considered as the safety factor value against buckling failure due to load acting on the member. is calculated using Beam buckling factor 2=(4*Warping Constant/Moment of Inertia about Y-axis)*((Section modulus about major axis)/(Shear Modulus of Elasticity*Torsional constant))^2. To calculate Beam Buckling Factor 2, you need Warping Constant (Cw), Moment of Inertia about Y-axis (Iy), Section modulus about major axis (Sx), Shear Modulus of Elasticity (G) and Torsional constant (J). With our tool, you need to enter the respective value for Warping Constant, Moment of Inertia about Y-axis, Section modulus about major axis, Shear Modulus of Elasticity and Torsional constant 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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