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
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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

5 Other formulas that calculate the same Output

Allowable Compressive Stress for Aluminium Columns when Column Yield Stress is Given
Compressive Stress=Yield stress*(1-(Aluminum Alloy Constant K*((Length/Radius of gyration)/(pi*sqrt(End Fixity Coefficient*Modulus Of Elasticity/Yield stress)))^Aluminum Alloy Constant n)) GO
Compressive Stress Of Spigot
Compressive Stress=Tensile Force on Rods/(Thickness of Cotter *Diameter of Spigot) GO
Compressive stress if the modulus of elasticity and compressive strain are known
Compressive Stress=(Modulus Of Elasticity*Compressive strain) GO
Compressive stress if resisting force is known
Compressive Stress=Resistance Force/Cross sectional area GO
Compressive stress if axial push acting on body is known
Compressive Stress=Axial Push/Cross sectional area GO

Allowable Compressive Stress for Aluminium Columns Formula

Compressive Stress=End Fixity Coefficient*(pi^2)*Young's Modulus/((Length/Radius of gyration)^2)
σ<sub>c=c*(pi^2)*E/((l/k<sub>G</sub>)^2)
More formulas
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 when Column Yield Stress is Given GO
Transition from Long to Short Column Range GO

End Fixity Coefficient

The end fixity coefficient is defined as the ratio of the moment at one end to the moment at the same end when both the ends are ideally fixed. c=2, both ends pivoted; c=2.86, one pivoted, other fixed; c=1.25 to 1.50,Restraining bulkhead partially fixed; c=4, both ends fixed; c=1 one fixed, one free.

How to Calculate Allowable Compressive Stress for Aluminium Columns?

Allowable Compressive Stress for Aluminium Columns calculator uses Compressive Stress=End Fixity Coefficient*(pi^2)*Young's Modulus/((Length/Radius of gyration)^2) to calculate the Compressive Stress, The Allowable Compressive Stress for Aluminium Columns formula is defined as the maximum stress (tensile, compressive or bending) that can be applied on a structural material such as Aluminium Columns without any deformation. Compressive Stress and is denoted by σc symbol.

How to calculate Allowable Compressive Stress for Aluminium Columns using this online calculator? To use this online calculator for Allowable Compressive Stress for Aluminium Columns, enter End Fixity Coefficient (c), Young's Modulus (E), Length (l) and Radius of gyration (kG) and hit the calculate button. Here is how the Allowable Compressive Stress for Aluminium Columns calculation can be explained with given input values -> 9.870E+11 = 1*(pi^2)*100000000000/((3/3)^2).

FAQ

What is Allowable Compressive Stress for Aluminium Columns?
The Allowable Compressive Stress for Aluminium Columns formula is defined as the maximum stress (tensile, compressive or bending) that can be applied on a structural material such as Aluminium Columns without any deformation and is represented as σc=c*(pi^2)*E/((l/kG)^2) or Compressive Stress=End Fixity Coefficient*(pi^2)*Young's Modulus/((Length/Radius of gyration)^2). The end fixity coefficient is defined as the ratio of the moment at one end to the moment at the same end when both the ends are ideally fixed, 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), 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 Allowable Compressive Stress for Aluminium Columns?
The Allowable Compressive Stress for Aluminium Columns formula is defined as the maximum stress (tensile, compressive or bending) that can be applied on a structural material such as Aluminium Columns without any deformation is calculated using Compressive Stress=End Fixity Coefficient*(pi^2)*Young's Modulus/((Length/Radius of gyration)^2). To calculate Allowable Compressive Stress for Aluminium Columns, you need End Fixity Coefficient (c), Young's Modulus (E), Length (l) and Radius of gyration (kG). With our tool, you need to enter the respective value for End Fixity Coefficient, Young's Modulus, 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 Compressive Stress?
In this formula, Compressive Stress uses End Fixity Coefficient, Young's Modulus, Length and Radius of gyration. We can use 5 other way(s) to calculate the same, which is/are as follows -
  • Compressive Stress=Tensile Force on Rods/(Thickness of Cotter *Diameter of Spigot)
  • Compressive Stress=Yield stress*(1-(Aluminum Alloy Constant K*((Length/Radius of gyration)/(pi*sqrt(End Fixity Coefficient*Modulus Of Elasticity/Yield stress)))^Aluminum Alloy Constant n))
  • Compressive Stress=Resistance Force/Cross sectional area
  • Compressive Stress=Axial Push/Cross sectional area
  • Compressive Stress=(Modulus Of Elasticity*Compressive strain)
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