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

Periodic time of SHM for compound pendulum in terms of radius of gyration
Periodic time for compound pendulum=2*pi*sqrt(((Radius of gyration^2)+(Distance of point of suspension of pendulum from the center of gravity^2))/(Acceleration Due To Gravity*Distance of point of suspension of pendulum from the center of gravity)) GO
Velocity ratio of belt in terms of creep of belt
Velocity ratio=(Diameter of the driver*(Young's Modulus+sqrt(Stress in the belt on the slack side of belt)))/(Diameter of the follower*(Young's Modulus+sqrt(Stress in the belt on the tight side of belt))) GO
Euler's Formula for Critical Buckling Load when Area is Given
Critical Buckling Load=(Coefficient for Column End Conditions*(pi^2)*Modulus Of Elasticity*Cross sectional area)/((Length/Radius of gyration)^2) GO
Total Unit Stress in Eccentric Loading when Radius of Gyration is Given
Total Unit Stress=(Axial Load/Cross sectional area)*(1+(Outermost Fiber Distance*Distance_from Load Applied/(Radius of gyration^2))) GO
Thermal stress of a material
Thermal stress=(Young's Modulus*Coefficient of Linear Thermal expansion*Temperature Difference)/(Initial length) GO
Time period of Rolling
Time period of rolling=2*pi*(sqrt(((Radius of gyration)^(2))/(Acceleration Due To Gravity*Metacentric height))) GO
Theoretical Maximum Stress for ANC Code Alloy Steel Tubing
Critical stress=135000-(15.9/End Fixity Coefficient)*((Length/Radius of gyration)^2) GO
Critical stress for crack propagation
Critical stress=sqrt(2*Young's Modulus*Specific surface energy/(pi*Crack Length)) GO
Minimum periodic time of SHM for compound pendulum
Time Period SHM=2*pi*sqrt(2*Radius of gyration/Acceleration Due To Gravity) GO
Modulus of resilience
Modulus of resilience=Yield Strength^2/(2*Young's Modulus) GO
Strain Energy if applied tension load is given
Strain Energy=Force^2*Length/(2*Area*Young's Modulus) GO

11 Other formulas that calculate the same Output

Length over which Deformation Takes Place when Strain Energy in Torsion is Given
Length=sqrt(2*Strain Energy*Polar moment of Inertia*Shear Modulus of Elasticity/Torque^2) 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
Length of rectangle when diagonal and breadth are given
Length=sqrt(Diagonal^2-Breadth^2) GO
Length of rectangle when perimeter and breadth are given
Length=(Perimeter-2*Breadth)/2 GO
Length of rectangle when diagonal and angle between two diagonal are given
Length=Diagonal*sin(sinϑ/2) GO
Length of a rectangle in terms of diagonal and angle between diagonal and breadth
Length=Diagonal*sin(sinϑ) GO
Length of rectangle when area and breadth are given
Length=Area/Breadth GO
Length of the major axis of an ellipse (b>a)
Length=2*Major axis GO
Length of major axis of an ellipse (a>b)
Length=2*Major axis GO
Length of minor axis of an ellipse (a>b)
Length=2*Minor axis GO
Length of minor axis of an ellipse (b>a)
Length=2*Minor axis GO

Length of Column when Allowable Compressive Stress for Aluminium Columns is Given Formula

Length=sqrt(End Fixity Coefficient*(pi^2)*Young's Modulus/(Compressive Stress/(Radius of gyration)^2))
l=sqrt(c*(pi^2)*E/(σ<sub>c/(k<sub>G</sub>)^2))
More formulas
Radius of Gyration 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

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 Length of Column when Allowable Compressive Stress for Aluminium Columns is Given?

Length of Column when Allowable Compressive Stress for Aluminium Columns is Given calculator uses Length=sqrt(End Fixity Coefficient*(pi^2)*Young's Modulus/(Compressive Stress/(Radius of gyration)^2)) to calculate the Length, The Length of Column when Allowable Compressive Stress for Aluminium Columns is Given formula is defined as the distance between two points where a column gets its fixidty of support so its movement is restrained in all directions. Length and is denoted by l symbol.

How to calculate Length of Column when Allowable Compressive Stress for Aluminium Columns is Given using this online calculator? To use this online calculator for Length of Column when Allowable Compressive Stress for Aluminium Columns is Given, enter End Fixity Coefficient (c), Young's Modulus (E), Compressive Stress c) and Radius of gyration (kG) and hit the calculate button. Here is how the Length of Column when Allowable Compressive Stress for Aluminium Columns is Given calculation can be explained with given input values -> 421488.9 = sqrt(1*(pi^2)*100000000000/(50/(3)^2)).

FAQ

What is Length of Column when Allowable Compressive Stress for Aluminium Columns is Given?
The Length of Column when Allowable Compressive Stress for Aluminium Columns is Given formula is defined as the distance between two points where a column gets its fixidty of support so its movement is restrained in all directions and is represented as l=sqrt(c*(pi^2)*E/(σc/(kG)^2)) or Length=sqrt(End Fixity Coefficient*(pi^2)*Young's Modulus/(Compressive Stress/(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), Compressive Stress is the force that is responsible for the deformation of the material such that the volume of the material reduces 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 Length of Column when Allowable Compressive Stress for Aluminium Columns is Given?
The Length of Column when Allowable Compressive Stress for Aluminium Columns is Given formula is defined as the distance between two points where a column gets its fixidty of support so its movement is restrained in all directions is calculated using Length=sqrt(End Fixity Coefficient*(pi^2)*Young's Modulus/(Compressive Stress/(Radius of gyration)^2)). To calculate Length of Column when Allowable Compressive Stress for Aluminium Columns is Given, you need End Fixity Coefficient (c), Young's Modulus (E), Compressive Stress c) and Radius of gyration (kG). With our tool, you need to enter the respective value for End Fixity Coefficient, Young's Modulus, Compressive Stress 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 Length?
In this formula, Length uses End Fixity Coefficient, Young's Modulus, Compressive Stress and Radius of gyration. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Length=sqrt(Diagonal^2-Breadth^2)
  • Length=Area/Breadth
  • Length=(Perimeter-2*Breadth)/2
  • Length=Diagonal*sin(sinϑ)
  • Length=Diagonal*sin(sinϑ/2)
  • Length=2*Major axis
  • Length=2*Major axis
  • Length=2*Minor axis
  • Length=2*Minor axis
  • Length=2*Strain Energy*Shear Area*Shear Modulus of Elasticity/(Shear Force^2)
  • Length=sqrt(2*Strain Energy*Polar moment of Inertia*Shear Modulus of Elasticity/Torque^2)
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