Rudrani Tidke
Cummins College of Engineering for Women (CCEW), Pune
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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

Critical Buckling Load for Pin Ended Columns
Critical Buckling Load=((pi^2)*Modulus of Elasticity of Column*Column Cross-Sectional Area)/((Length/Radius of Gyration of the Column)^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

Euler's Formula for Critical Buckling Load when Area is Given Formula

Critical Buckling Load=(Coefficient for Column End Conditions*(pi^2)*Modulus Of Elasticity*Cross sectional area)/((Length/Radius of gyration)^2)
P<sub>c=(n*(pi^2)*E*A)/((l/k<sub>G</sub>)^2)
More formulas
Euler's Formula for Critical Buckling Load GO
Smallest Moment of Inertia Allowable at Worst Section for Cast Iron GO
Smallest Moment of Inertia Allowable at Worst Section for Wrought Iron GO
Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel GO
Smallest Moment of Inertia Allowable at Worst Section for Medium Carbon Steel GO
Maximum Stress For a Rectangular Cross Section GO
Maximum Stress For a Circular Cross Section GO
Theoretical Maximum Stress for ANC Code Alloy Steel Tubing GO
Theoretical Maximum Stress for ANC Code 2017ST Aluminium GO
Theoretical Maximum Stress for ANC Code Spruce GO
Theoretical Maximum Stress for Johnson Code Steels GO
Theoretical Maximum Stress for Secant Code Steels GO
Length of a Rectangular Section Under Compression GO
Maximum Stress For a Circular Section Under Compression GO
Maximum Stress For a Rectangular Section Under Compression GO
Radius of the Kern for a Circular Ring GO
Radius of the Kern for a Hollow Square GO
Critical Slenderness Ratio for Cast Iron Columns GO
Ultimate Load per Area for Cast Iron Columns GO
Ultimate Load per Area for Aluminium Columns GO
Ultimate Load per Area for Aluminium Columns GO
Critical Slenderness Ratio for Aluminium Columns GO
Specified Compressive Strength of Concrete when Nominal Bearing Strength is Given GO
Nominal Bearing Strength of the Concrete GO
Area of the Base Plate when Nominal Bearing Strength is Given GO
Area of the Supporting Concrete when Nominal Bearing Strength is Given GO
Required Area of a Base Plate for a Factored Load GO
Factored Load when Base Plate Area is Given GO
Width Parallel to the Flanges GO
Base Plate Thickness when Projection of Base Plate Beyond the Flange and Parallel to Web is Given GO
Base Plate Thickness when Projection of Base Plate Beyond Flange and Perpendicular to Web is Given GO
Projection of Base Plate Beyond the Flange and Parallel to Web GO
Projection of Base Plate Beyond the Flange and Perpendicular to Web GO
Thickness of Wall for a Hollow Octagon GO
Area of foundation of the Lowest Column of a Structure GO
Load when Area of Lowest Column of a Structure is Given GO
Allowable Bearing Pressure when Area of Lowest Column of a Structure is Given GO
Allowable Bearing Pressure when Full Area of Support is Occupied by Base Plate GO
Equivalent Cantilever Dimension GO
Base Plate Thickness GO
Design Strength of an Axially Loaded Composite Column GO
Gross Area of Steel Core when Design Strength of Axially Loaded Composite Column is Given GO
Design Strength of Concrete for Direct Bearing GO
Loaded Area when Design Strength of Concrete for Direct Bearing is Given GO
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
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
Radius of Gyration of Column when Allowable Compressive Stress for Aluminium Columns is Given GO
Length of Column when Allowable Compressive Stress for Aluminium Columns is Given GO
Allowable Compressive Stress for Aluminium Columns GO
Allowable Compressive Stress for Aluminium Columns when Column Yield Stress is Given GO
Transition from Long to Short Column Range GO
Column Ultimate Strength with Zero Eccentricity of Load GO
Yield Strength of Reinforcing Steel when Column Ultimate Strength is Given GO
28-day Concrete Compressive Strength when Column Ultimate Strength is Given GO
Axial-Load Capacity of Short Rectangular Members GO
Tensile Stress in Steel when Axial-Load Capacity of Short Rectangular Members is Given GO
Tension Reinforcement Area when Axial-Load Capacity of Short Rectangular Members is Given GO
Compressive Reinforcement Area when Axial-Load Capacity of Short Rectangular Members is Given GO
Balanced Moment when Load and Eccentricity is Given GO
Balanced Moment when Φ is Given GO
Ultimate Strength for Symmetrical Reinforcement GO
Ultimate Strength for No Compression Reinforcement GO
Ultimate Strength for Symmetrical Reinforcement in Single Layers GO
Ultimate Strength for Short, Circular Members when Controlled by Tension GO
Ultimate Strength for Short, Circular Members when Governed by Compression GO
Eccentricity for Balanced Condition for Short, Circular Members GO
Ultimate Strength for Short, Square Members when Governed by Compression GO
Ultimate Strength for Short, Square Members when Controlled by Tension GO
Magnified Moment when Eccentricity of Slender Columns is Given GO
Eccentricity of Slender Columns GO
LRFD Strength for a Compression Member GO
LRFD Design Strength of Member GO
Slenderness Ratio that Demarcates Between Inelastic from Elastic Buckling GO
Allowable Compression Stress when Slenderness Ratio is less than Cc GO
Allowable Compression Stress when Slenderness Ratio is Greater than Cc GO

Column End Conditions

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 = 2; when both ends are fixed, n = 4; and when one end is fixed and the other is free, n = 0.25. The slenderness ratio separating long columns from short columns depends on the modulus of elasticity and the yield strength of the column material.

How to Calculate Euler's Formula for Critical Buckling Load when Area is Given?

Euler's Formula for Critical Buckling Load when Area is Given calculator uses Critical Buckling Load=(Coefficient for Column End Conditions*(pi^2)*Modulus Of Elasticity*Cross sectional area)/((Length/Radius of gyration)^2) to calculate the Critical Buckling Load, The Euler's Formula for Critical Buckling Load when Area is Given formula is defined as the compressive load at which a slender column will suddenly bend or buckle. Critical Buckling Load and is denoted by Pc symbol.

How to calculate Euler's Formula for Critical Buckling Load when Area is Given using this online calculator? To use this online calculator for Euler's Formula for Critical Buckling Load when Area is Given, enter Coefficient for Column End Conditions (n), Modulus Of Elasticity (E), Cross sectional area (A), Length (l) and Radius of gyration (kG) and hit the calculate button. Here is how the Euler's Formula for Critical Buckling Load when Area is Given calculation can be explained with given input values -> 986960.4 = (1*(pi^2)*10000*10)/((3/3)^2).

FAQ

What is Euler's Formula for Critical Buckling Load when Area is Given?
The Euler's Formula for Critical Buckling Load when Area is Given formula is defined as the compressive load at which a slender column will suddenly bend or buckle and is represented as Pc=(n*(pi^2)*E*A)/((l/kG)^2) or Critical Buckling Load=(Coefficient for Column End Conditions*(pi^2)*Modulus Of Elasticity*Cross sectional area)/((Length/Radius of gyration)^2). Coefficient for Column End Conditions is defined as the multiplicative factor for different column end conditions, Modulus Of Elasticity is a quantity that measures an object or substance's resistance to being deformed elastically when a stress is applied to it, 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, Length is the measurement or extent of something from end to end and 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.
How to calculate Euler's Formula for Critical Buckling Load when Area is Given?
The Euler's Formula for Critical Buckling Load when Area is Given formula is defined as the compressive load at which a slender column will suddenly bend or buckle is calculated using Critical Buckling Load=(Coefficient for Column End Conditions*(pi^2)*Modulus Of Elasticity*Cross sectional area)/((Length/Radius of gyration)^2). To calculate Euler's Formula for Critical Buckling Load when Area is Given, you need Coefficient for Column End Conditions (n), Modulus Of Elasticity (E), Cross sectional area (A), Length (l) and Radius of gyration (kG). With our tool, you need to enter the respective value for Coefficient for Column End Conditions, Modulus Of Elasticity, Cross sectional area, Length and Radius of gyration 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 Coefficient for Column End Conditions, Modulus Of Elasticity, Cross sectional area, Length and Radius of gyration. 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=((pi^2)*Modulus of Elasticity of Column*Column Cross-Sectional Area)/((Length/Radius of Gyration of the Column)^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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