Eccentricity to Maintain Stress as Wholly Compressive Solution

STEP 0: Pre-Calculation Summary
Formula Used
Eccentricity of Load = Section Modulus for Eccentric Load on Beam/Area of Cross-Section
e' = Z/A
This formula uses 3 Variables
Variables Used
Eccentricity of Load - (Measured in Meter) - Eccentricity of Load is the distance from point of application of resultant to center of base.
Section Modulus for Eccentric Load on Beam - (Measured in Cubic Meter) - Section Modulus for Eccentric Load on Beam is a geometric property for a given cross-section used in the design of beams or flexural members.
Area of Cross-Section - (Measured in Square Meter) - Area of Cross-section is a cross-sectional area which we obtain when the same object is cut into two pieces. The area of that particular cross-section is known as the cross-sectional area.
STEP 1: Convert Input(s) to Base Unit
Section Modulus for Eccentric Load on Beam: 1120000 Cubic Millimeter --> 0.00112 Cubic Meter (Check conversion here)
Area of Cross-Section: 5600 Square Millimeter --> 0.0056 Square Meter (Check conversion here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
e' = Z/A --> 0.00112/0.0056
Evaluating ... ...
e' = 0.2
STEP 3: Convert Result to Output's Unit
0.2 Meter -->200 Millimeter (Check conversion here)
FINAL ANSWER
200 Millimeter <-- Eccentricity of Load
(Calculation completed in 00.004 seconds)

Credits

Created by Rithik Agrawal
National Institute of Technology Karnataka (NITK), Surathkal
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7 Strain Energy Calculators

Eccentricity in Column for Hollow Circular Section when Stress at Extreme Fibre is Zero
Go Eccentricity of Load = (Outer Depth^2+Inner Depth^2)/(8*Outer Depth)
Section Modulus to Maintain Stress as Wholly Compressive given Eccentricity
Go Section Modulus for Eccentric Load on Beam = Eccentricity of Load*Area of Cross-Section
Area to Maintain Stress as Wholly Compressive given Eccentricity
Go Area of Cross-Section = Section Modulus for Eccentric Load on Beam/Eccentricity of Load
Eccentricity to Maintain Stress as Wholly Compressive
Go Eccentricity of Load = Section Modulus for Eccentric Load on Beam/Area of Cross-Section
Eccentricity for Solid Circular Sector to Maintain Stress as Wholly Compressive
Go Eccentricity of Load = Diameter of Circular Shaft/8
Eccentricity for Rectangular Section to maintain Stress as Wholly Compressive
Go Eccentricity of Load = Dam Thickness/6
Breadth for Rectangular Section to Maintain Stress as Wholly Compressive
Go Dam Thickness = 6*Eccentricity of Load

11 Structural Analysis of Beams Calculators

Beam Depth of Uniform Strength for Simply Supported Beam when Load is at Centre
Go Effective Depth of Beam = sqrt((3*Point Load*Distance from A end)/(Width of Beam Section*Stress of Beam))
Beam Breadth of Uniform Strength for Simply Supported Beam when Load is at Centre
Go Width of Beam Section = (3*Point Load*Distance from A end)/(Stress of Beam*Effective Depth of Beam^2)
Loading of Beam of Uniform Strength
Go Point Load = (Stress of Beam*Width of Beam Section*Effective Depth of Beam^2)/(3*Distance from A end)
Stress of Beam of Uniform Strength
Go Stress of Beam = (3*Point Load*Distance from A end)/(Width of Beam Section*Effective Depth of Beam^2)
Eccentricity in Column for Hollow Circular Section when Stress at Extreme Fibre is Zero
Go Eccentricity of Load = (Outer Depth^2+Inner Depth^2)/(8*Outer Depth)
Section Modulus to Maintain Stress as Wholly Compressive given Eccentricity
Go Section Modulus for Eccentric Load on Beam = Eccentricity of Load*Area of Cross-Section
Area to Maintain Stress as Wholly Compressive given Eccentricity
Go Area of Cross-Section = Section Modulus for Eccentric Load on Beam/Eccentricity of Load
Eccentricity to Maintain Stress as Wholly Compressive
Go Eccentricity of Load = Section Modulus for Eccentric Load on Beam/Area of Cross-Section
Eccentricity for Solid Circular Sector to Maintain Stress as Wholly Compressive
Go Eccentricity of Load = Diameter of Circular Shaft/8
Eccentricity for Rectangular Section to maintain Stress as Wholly Compressive
Go Eccentricity of Load = Dam Thickness/6
Breadth for Rectangular Section to Maintain Stress as Wholly Compressive
Go Dam Thickness = 6*Eccentricity of Load

Eccentricity to Maintain Stress as Wholly Compressive Formula

Eccentricity of Load = Section Modulus for Eccentric Load on Beam/Area of Cross-Section
e' = Z/A

What is Eccentric Loading?

A load, whose line of action does not coincide with the axis of a column or a strut, is known as an eccentric load.

How to Calculate Eccentricity to Maintain Stress as Wholly Compressive?

Eccentricity to Maintain Stress as Wholly Compressive calculator uses Eccentricity of Load = Section Modulus for Eccentric Load on Beam/Area of Cross-Section to calculate the Eccentricity of Load, The Eccentricity to Maintain Stress as Wholly Compressive formula is defined as the distance of the line of action from the center axis given is the maximum limit. Eccentricity of Load is denoted by e' symbol.

How to calculate Eccentricity to Maintain Stress as Wholly Compressive using this online calculator? To use this online calculator for Eccentricity to Maintain Stress as Wholly Compressive, enter Section Modulus for Eccentric Load on Beam (Z) & Area of Cross-Section (A) and hit the calculate button. Here is how the Eccentricity to Maintain Stress as Wholly Compressive calculation can be explained with given input values -> 200000 = 0.00112/0.0056.

FAQ

What is Eccentricity to Maintain Stress as Wholly Compressive?
The Eccentricity to Maintain Stress as Wholly Compressive formula is defined as the distance of the line of action from the center axis given is the maximum limit and is represented as e' = Z/A or Eccentricity of Load = Section Modulus for Eccentric Load on Beam/Area of Cross-Section. Section Modulus for Eccentric Load on Beam is a geometric property for a given cross-section used in the design of beams or flexural members & Area of Cross-section is a cross-sectional area which we obtain when the same object is cut into two pieces. The area of that particular cross-section is known as the cross-sectional area.
How to calculate Eccentricity to Maintain Stress as Wholly Compressive?
The Eccentricity to Maintain Stress as Wholly Compressive formula is defined as the distance of the line of action from the center axis given is the maximum limit is calculated using Eccentricity of Load = Section Modulus for Eccentric Load on Beam/Area of Cross-Section. To calculate Eccentricity to Maintain Stress as Wholly Compressive, you need Section Modulus for Eccentric Load on Beam (Z) & Area of Cross-Section (A). With our tool, you need to enter the respective value for Section Modulus for Eccentric Load on Beam & Area of Cross-Section 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 Eccentricity of Load?
In this formula, Eccentricity of Load uses Section Modulus for Eccentric Load on Beam & Area of Cross-Section. We can use 6 other way(s) to calculate the same, which is/are as follows -
  • Eccentricity of Load = (Outer Depth^2+Inner Depth^2)/(8*Outer Depth)
  • Eccentricity of Load = Dam Thickness/6
  • Eccentricity of Load = Diameter of Circular Shaft/8
  • Eccentricity of Load = Diameter of Circular Shaft/8
  • Eccentricity of Load = Dam Thickness/6
  • Eccentricity of Load = (Outer Depth^2+Inner Depth^2)/(8*Outer Depth)
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