Cross-Sectional Area when Elastic Critical Buckling Load is Given Calculator

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✖Critical Buckling Load is defined as the greatest load that will not cause lateral deflection.ⓘ Critical Buckling Load [P_c]			+10% -10%
✖Coefficient for Column End Conditions is defined as the multiplicative factor for different column end conditions.ⓘ Coefficient for Column End Conditions [n]			+10% -10%
✖Length is the measurement or extent of something from end to end.ⓘ Length [l]			+10% -10%
✖Radius of gyration or gyradius of a body about an 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, if the total mass of the body were concentrated there.ⓘ Radius of gyration [k_G]			+10% -10%
✖Young's Modulus which can also be called elastic modulus is a mechanical property of linear elastic solid substances. It describes the relationship between stress (force per unit area) and strain (proportional deformation in an object).ⓘ Young's Modulus [E]			+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 Elastic Critical Buckling Load is Given [A]

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Cross-Sectional Area when Elastic Critical Buckling Load is Given

Rudrani Tidke

Cummins College of Engineering for Women (CCEW), Pune

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

Alithea Fernandes

Don Bosco College of Engineering (DBCE), Goa

Alithea Fernandes has verified this Calculator and 100+ more calculators!

< 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

< 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 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 Torsional Buckling Load for Pin Ended Columns is Given

Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant) 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 Elastic Critical Buckling Load is Given Formula

Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus)
A=(P<sub>c*((n*l/k<sub>G</sub>)^2))/((pi^2)*E)

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

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

Column End Conditions for effective length of column

In this formula, the coefficient n accounts for end conditions. When the column is pivoted at both ends, n = 1; when one end is fixed and the other end is rounded, n = 0.7; when both ends are fixed, n = 0.5; and when one end is fixed and the other is free, n = 2.

How to Calculate Cross-Sectional Area when Elastic Critical Buckling Load is Given?

Cross-Sectional Area when Elastic Critical Buckling Load is Given calculator uses Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus) to calculate the Cross sectional area, The Cross-Sectional Area when Elastic Critical Buckling Load 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 Elastic Critical Buckling Load is Given using this online calculator? To use this online calculator for Cross-Sectional Area when Elastic Critical Buckling Load is Given, enter Critical Buckling Load (P_c), Coefficient for Column End Conditions (n), Length (l), Radius of gyration (k_G) and Young's Modulus (E) and hit the calculate button. Here is how the Cross-Sectional Area when Elastic Critical Buckling Load is Given calculation can be explained with given input values -> 5.066E-11 = (50*((1*3/3)^2))/((pi^2)*100000000000).

FAQ

What is Cross-Sectional Area when Elastic Critical Buckling Load is Given?

The Cross-Sectional Area when Elastic Critical Buckling Load 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_{c*((n*l/k_G)^2))/((pi^2)*E)} or Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus). Critical Buckling Load is defined as the greatest load that will not cause lateral deflection, Coefficient for Column End Conditions is defined as the multiplicative factor for different column end conditions, Length is the measurement or extent of something from end to end, Radius of gyration or gyradius of a body about an 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, if the total mass of the body were concentrated there and Young's Modulus which can also be called elastic modulus is a mechanical property of linear elastic solid substances. It describes the relationship between stress (force per unit area) and strain (proportional deformation in an object).

How to calculate Cross-Sectional Area when Elastic Critical Buckling Load is Given?

The Cross-Sectional Area when Elastic Critical Buckling Load 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=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus). To calculate Cross-Sectional Area when Elastic Critical Buckling Load is Given, you need Critical Buckling Load (P_c), Coefficient for Column End Conditions (n), Length (l), Radius of gyration (k_G) and Young's Modulus (E). With our tool, you need to enter the respective value for Critical Buckling Load, Coefficient for Column End Conditions, Length, Radius of gyration and Young's Modulus 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 Critical Buckling Load, Coefficient for Column End Conditions, Length, Radius of gyration and Young's Modulus. 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=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant)
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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