Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given Calculator

Category	Engineering ↺
Engineering	Civil ↺
Civil	Columns ↺
Columns	Elastic Flexural Buckling of Columns ↺

✖Torsional buckling load is an applied load causes both lateral displacement and twisting of a member.ⓘ Torsional buckling load [P_t]			+10% -10%
✖The Polar moment of Inertia is a shaft or beam's resistance to being distorted by torsion, as a function of its shape. ⓘ Polar moment of Inertia [J]			+10% -10%
✖Shear Modulus of Elasticity is one of the measures of mechanical properties of solids. Other elastic moduli are Young's modulus and bulk modulus.ⓘ Shear Modulus of Elasticity [G]			+10% -10%
✖Torsion constant is a geometrical property of a cross section of bar which is involved in the relationship between angle of twist and applied torque along the axis of the bar.ⓘ Torsion constant [J]			+10% -10%

✖Cross sectional area is the area of a two-dimensional shape that is obtained when a three dimensional shape is sliced perpendicular to some specifies axis at a point.ⓘ Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given [A]

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Rudrani Tidke

Cummins College of Engineering for Women (CCEW), Pune

Rudrani Tidke has created this Calculator and 100+ more calculators!

Mridul Sharma

Indian Institute of Information Technology (IIIT), Bhopal

Mridul Sharma has verified this Calculator and 200+ more calculators!

< 11 Other formulas that you can solve using the same Inputs

Constant for a particular shaft for torsion dynamometer

Constant for a particular shaft=(Modulus of rigidity*Polar moment of Inertia)/Length of Shaft GO

Strain Energy in Shear when Shear Deformation is Given

Strain Energy=(Shear Area*Shear Modulus of Elasticity*(Shear Deformation^2))/(2*Length) GO

Strain Energy in Torsion

Strain Energy=(Torque^2)*Length/(2*Polar moment of Inertia*Shear Modulus of Elasticity) GO

Total Angle of Twist

Total Angle of Twist=(Torque*Length of Shaft)/(Shear Modulus*Polar moment of Inertia) GO

torque acting on the shaft for torsion dynamometer

Torque=(Modulus of rigidity*Angle of Twist*Polar moment of Inertia)/Length of Shaft 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

Strain Energy if Torsion Moment Value is Given

Strain Energy=Torsion load*Length/(2*Shear Modulus*Polar moment of Inertia) GO

Torsional Shear Stress

Torsional Shear Stress=Torque*Radius of Shaft/Polar moment of Inertia GO

< 11 Other formulas that calculate the same Output

Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam

Cross sectional area=(Bending Moment /(Stress*Radius of Centroidal Axis))*(1+(Distance of Point from Centroidal Axis/(Cross-Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis)))) GO

Cross-Sectional Area when Axial Buckling Load for a Warped Section is Given

Cross sectional area=(Axial buckling Load*Polar moment of Inertia)/(Shear Modulus of Elasticity*Torsion constant+((pi^2)*Young's Modulus*Warping Constant/(Length^2))) GO

Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given

Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis))) GO

Cross-sectional area of the rod if stress induced in rod due to impact load is known

Cross sectional area=(2*Modulus Of Elasticity*Load Dropped(Impact Load)*Height through which load is dropped)/(Length of Rod*(Stress induced^2)) GO

Cross-Sectional Area when Elastic Critical Buckling Load is Given

Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus) GO

Cross-Sectional Area when Maximum Stress For Short Beams is Given

Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) GO

Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given

Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity) GO

Cross-Sectional Area when Critical Buckling Load for Pin Ended Columns is Given

Cross sectional area=Critical Buckling Load*(Slenderness Ratio^2)/((pi^2)*Young's Modulus) GO

Cross-sectional Area of Soil Conveying Flow when Rate of Flow of Water is Given

Cross sectional area=(Rate of flow/(Coefficient of permeability*Hydraulic gradient)) GO

Total Cross-Sectional Area of Tensile Reinforcing

Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam) GO

Area when water flow equation is given

Cross sectional area=water flow/flow velocity GO

Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given Formula

Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant)
A=P<sub>t</sub>*J/(G*J)

More formulas

Critical Buckling Load for Pin Ended Columns GO

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

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

When does Lateral torsional buckling occur?

Lateral torsional buckling may occur in an unrestrained beam. A beam is considered to be unrestrained when its compression flange is free to displace laterally and rotate. When an applied load causes both lateral displacement and twisting of a member lateral torsional buckling has occurred.

How to Calculate Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given?

Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given calculator uses Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant) to calculate the Cross sectional area, The Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given formula is defined as the area of a two-dimensional shape obtained when a Column is sliced perpendicular to its length axis at a point. Cross sectional area and is denoted by A symbol.

How to calculate Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given using this online calculator? To use this online calculator for Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given, enter Torsional buckling load (P_t), Polar moment of Inertia (J), Shear Modulus of Elasticity (G) and Torsion constant (J) and hit the calculate button. Here is how the Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given calculation can be explained with given input values -> 0.333333 = 10*50/(100*15).

FAQ

What is Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given?

The Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given formula is defined as the area of a two-dimensional shape obtained when a Column is sliced perpendicular to its length axis at a point and is represented as A=P_t*J/(G*J) or Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant). Torsional buckling load is an applied load causes both lateral displacement and twisting of a member, The Polar moment of Inertia is a shaft or beam's resistance to being distorted by torsion, as a function of its shape. , 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 Torsion constant is a geometrical property of a cross section of bar which is involved in the relationship between angle of twist and applied torque along the axis of the bar.

How to calculate Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given?

The Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given formula is defined as the area of a two-dimensional shape obtained when a Column is sliced perpendicular to its length axis at a point is calculated using Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant). To calculate Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given, you need Torsional buckling load (P_t), Polar moment of Inertia (J), Shear Modulus of Elasticity (G) and Torsion constant (J). With our tool, you need to enter the respective value for Torsional buckling load, Polar moment of Inertia, Shear Modulus of Elasticity and Torsion constant 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 Cross sectional area?

In this formula, Cross sectional area uses Torsional buckling load, Polar moment of Inertia, Shear Modulus of Elasticity and Torsion constant. We can use 11 other way(s) to calculate the same, which is/are as follows -

Cross sectional area=(Bending Moment /(Stress*Radius of Centroidal Axis))*(1+(Distance of Point from Centroidal Axis/(Cross-Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis))))
Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia))
Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis)))
Cross sectional area=Critical Buckling Load*(Slenderness Ratio^2)/((pi^2)*Young's Modulus)
Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus)
Cross sectional area=(Axial buckling Load*Polar moment of Inertia)/(Shear Modulus of Elasticity*Torsion constant+((pi^2)*Young's Modulus*Warping Constant/(Length^2)))
Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam)
Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity)
Cross sectional area=(2*Modulus Of Elasticity*Load Dropped(Impact Load)*Height through which load is dropped)/(Length of Rod*(Stress induced^2))
Cross sectional area=water flow/flow velocity
Cross sectional area=(Rate of flow/(Coefficient of permeability*Hydraulic gradient))

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