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
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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 (Pt), 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=Pt*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 (Pt), 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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