Mridul Sharma
Indian Institute of Information Technology (IIIT), Bhopal
Mridul Sharma has created this Calculator and 100+ more calculators!
Kethavath Srinath
Osmania University (OU), Hyderabad
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11 Other formulas that you can solve using the same Inputs

Maximum and Center Deflection of Cantilever Beam carrying Point Load at any point
Deflection=(Point Load acting on the Beam*(Distance from end A^2)*(3*Length-Distance from end A))/(6*Modulus Of Elasticity*Area Moment of Inertia) GO
Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length
Deflection=(5*Uniformly Distributed Load*(Length^4))/(384*Modulus Of Elasticity*Area Moment of Inertia) GO
Maximum and Center Deflection of Simply Supported Beam carrying Point Load at Center
Deflection=(Point Load acting on the Beam*(Length^3))/(48*Modulus Of Elasticity*Area Moment of Inertia) GO
Maximum and Center Deflection of Cantilever Beam carrying Point Load at Free End
Deflection=(Point Load acting on the Beam*(Length^3))/(3*Modulus Of Elasticity*Area Moment of Inertia) GO
Maximum and Center Deflection of Cantilever Beam with Couple Moment at Free End
Deflection=(Couple Moment*(Length^2))/(2*Modulus Of Elasticity*Area Moment of Inertia) GO
Bending Moment when Strain Energy in Bending is Given
Bending moment=sqrt(Strain Energy*(2*Modulus Of Elasticity*Moment of Inertia)/Length) GO
Strain Energy in Bending when Angle Through which One Beam Rotates wrt Other End is Given
Strain Energy=Modulus Of Elasticity*Moment of Inertia*(Angle of Twist^2)/(2*Length) GO
Length over which Deformation Takes Place when Strain Energy in Bending is Given
Length=Strain Energy*(2*Modulus Of Elasticity*Moment of Inertia)/(Bending moment^2) GO
Moment of Inertia when Strain Energy in Bending is Given
Moment of Inertia=Length*(Bending moment^2)/(2*Strain Energy*Modulus Of Elasticity) GO
Strain Energy in Bending
Strain Energy=(Bending moment^2)*Length/(2*Modulus Of Elasticity*Moment of Inertia) GO
Stress using Hook's Law
Stress=Modulus Of Elasticity*Engineering strain GO

2 Other formulas that calculate the same Output

Allowable Unit Stress on Timber Columns for a Single Member
Allowable Unit Stress=(3.619*Modulus Of Elasticity)/((unsupported length of column/Radius of gyration)^2) GO
Allowable Unit Stress on Timber Columns of Square or Rectangular Cross Section
Allowable Unit Stress=(0.3*Modulus Of Elasticity)/((unsupported length of column/least dimension)^2) GO

Allowable Unit Stress on Timber Columns of Circular Cross Section Formula

Allowable Unit Stress=(0.22*Modulus Of Elasticity)/((unsupported length of column/least dimension)^2)
P/A=(0.22*E)/((l/d)^2)
More formulas
Elasticity Modulus when Allowable Unit Stress on Timber Columns for a Single Member is Given GO
Allowable Unit Stress on Timber Columns for a Single Member GO
Allowable Unit Stress on Timber Columns of Square or Rectangular Cross Section GO
Elasticity Modulus when Allowable Unit Stress of Square or Rectangular Timber Columns is Given GO
Elasticity Modulus when Allowable Unit Stress of Circular Timber Columns is Given GO

What is Allowable Unit Stress?

Allowable Unit Stress is the maximum stress per unit area (tensile, compressive or bending) that is allowed to be applied on a structural material.

How to Calculate Allowable Unit Stress on Timber Columns of Circular Cross Section?

Allowable Unit Stress on Timber Columns of Circular Cross Section calculator uses Allowable Unit Stress=(0.22*Modulus Of Elasticity)/((unsupported length of column/least dimension)^2) to calculate the Allowable Unit Stress, The Allowable Unit Stress on Timber Columns of Circular Cross Section formula calculates the maximum stress per unit area for timber columns whose cross section shape is circular. Allowable Unit Stress and is denoted by P/A symbol.

How to calculate Allowable Unit Stress on Timber Columns of Circular Cross Section using this online calculator? To use this online calculator for Allowable Unit Stress on Timber Columns of Circular Cross Section, enter Modulus Of Elasticity (E), unsupported length of column (l) and least dimension (d) and hit the calculate button. Here is how the Allowable Unit Stress on Timber Columns of Circular Cross Section calculation can be explained with given input values -> 0.0088 = (0.22*10000)/((0.001/0.002)^2).

FAQ

What is Allowable Unit Stress on Timber Columns of Circular Cross Section?
The Allowable Unit Stress on Timber Columns of Circular Cross Section formula calculates the maximum stress per unit area for timber columns whose cross section shape is circular and is represented as P/A=(0.22*E)/((l/d)^2) or Allowable Unit Stress=(0.22*Modulus Of Elasticity)/((unsupported length of column/least dimension)^2). 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, unsupported length of column is the distance between the end supports of a beam and least dimension is the measure of the shortest side of the column.
How to calculate Allowable Unit Stress on Timber Columns of Circular Cross Section?
The Allowable Unit Stress on Timber Columns of Circular Cross Section formula calculates the maximum stress per unit area for timber columns whose cross section shape is circular is calculated using Allowable Unit Stress=(0.22*Modulus Of Elasticity)/((unsupported length of column/least dimension)^2). To calculate Allowable Unit Stress on Timber Columns of Circular Cross Section, you need Modulus Of Elasticity (E), unsupported length of column (l) and least dimension (d). With our tool, you need to enter the respective value for Modulus Of Elasticity, unsupported length of column and least dimension 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 Allowable Unit Stress?
In this formula, Allowable Unit Stress uses Modulus Of Elasticity, unsupported length of column and least dimension. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Allowable Unit Stress=(3.619*Modulus Of Elasticity)/((unsupported length of column/Radius of gyration)^2)
  • Allowable Unit Stress=(0.3*Modulus Of Elasticity)/((unsupported length of column/least dimension)^2)
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