Mridul Sharma
Indian Institute of Information Technology (IIIT), Bhopal
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Kethavath Srinath
Osmania University (OU), Hyderabad
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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
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
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
Time period of Rolling
Time period of rolling=2*pi*(sqrt(((Radius of gyration)^(2))/(Acceleration Due To Gravity*Metacentric height))) 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
Strain Energy in Bending
Strain Energy=(Bending moment^2)*Length/(2*Modulus Of Elasticity*Moment of Inertia) GO
Minimum periodic time of SHM for compound pendulum
Time Period SHM=2*pi*sqrt(2*Radius of gyration/Acceleration Due To Gravity) 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 of Circular Cross Section
Allowable Unit Stress=(0.22*Modulus Of Elasticity)/((unsupported length of column/least dimension)^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 for a Single Member Formula

Allowable Unit Stress=(3.619*Modulus Of Elasticity)/((unsupported length of column/Radius of gyration)^2)
P/A=(3.619*E)/((l/k<sub>G</sub>)^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 of Square or Rectangular Cross Section GO
Elasticity Modulus when Allowable Unit Stress of Square or Rectangular Timber Columns is Given GO
Allowable Unit Stress on Timber Columns of Circular Cross Section 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 for a Single Member?

Allowable Unit Stress on Timber Columns for a Single Member calculator uses Allowable Unit Stress=(3.619*Modulus Of Elasticity)/((unsupported length of column/Radius of gyration)^2) to calculate the Allowable Unit Stress, The Allowable Unit Stress on Timber Columns for a Single Member formula calculates the maximum stress or load allowed per unit area for timber columns . Allowable Unit Stress and is denoted by P/A symbol.

How to calculate Allowable Unit Stress on Timber Columns for a Single Member using this online calculator? To use this online calculator for Allowable Unit Stress on Timber Columns for a Single Member, enter Modulus Of Elasticity (E), unsupported length of column (l) and Radius of gyration (kG) and hit the calculate button. Here is how the Allowable Unit Stress on Timber Columns for a Single Member calculation can be explained with given input values -> 325710 = (3.619*10000)/((0.001/3)^2).

FAQ

What is Allowable Unit Stress on Timber Columns for a Single Member?
The Allowable Unit Stress on Timber Columns for a Single Member formula calculates the maximum stress or load allowed per unit area for timber columns and is represented as P/A=(3.619*E)/((l/kG)^2) or Allowable Unit Stress=(3.619*Modulus Of Elasticity)/((unsupported length of column/Radius of gyration)^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 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 Unit Stress on Timber Columns for a Single Member?
The Allowable Unit Stress on Timber Columns for a Single Member formula calculates the maximum stress or load allowed per unit area for timber columns is calculated using Allowable Unit Stress=(3.619*Modulus Of Elasticity)/((unsupported length of column/Radius of gyration)^2). To calculate Allowable Unit Stress on Timber Columns for a Single Member, you need Modulus Of Elasticity (E), unsupported length of column (l) and Radius of gyration (kG). With our tool, you need to enter the respective value for Modulus Of Elasticity, unsupported length of column 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 Allowable Unit Stress?
In this formula, Allowable Unit Stress uses Modulus Of Elasticity, unsupported length of column and Radius of gyration. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Allowable Unit Stress=(0.3*Modulus Of Elasticity)/((unsupported length of column/least dimension)^2)
  • Allowable Unit Stress=(0.22*Modulus Of Elasticity)/((unsupported length of column/least dimension)^2)
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