Bending Stress for Hollow Circular Section using Eccentric Load and Eccentricity Solution

STEP 0: Pre-Calculation Summary
Formula Used
Bending Stress in Column = (Eccentricity of Loading*Eccentric load on column)/Section Modulus
σb = (eload*P)/S
This formula uses 4 Variables
Variables Used
Bending Stress in Column - (Measured in Pascal) - Bending Stress in Column is the normal stress that is induced at a point in a body subjected to loads that cause it to bend.
Eccentricity of Loading - (Measured in Meter) - Eccentricity of Loading is the distance between the actual line of action of loads and the line of action that would produce a uniform stress over the cross section of the specimen.
Eccentric load on column - (Measured in Newton) - Eccentric load on column is the load that causes direct stress as well as bending stress.
Section Modulus - (Measured in Cubic Meter) - Section Modulus is a geometric property for a given cross-section used in the design of beams or flexural members.
STEP 1: Convert Input(s) to Base Unit
Eccentricity of Loading: 25 Millimeter --> 0.025 Meter (Check conversion here)
Eccentric load on column: 7 Kilonewton --> 7000 Newton (Check conversion here)
Section Modulus: 1200000 Cubic Millimeter --> 0.0012 Cubic Meter (Check conversion here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
σb = (eload*P)/S --> (0.025*7000)/0.0012
Evaluating ... ...
σb = 145833.333333333
STEP 3: Convert Result to Output's Unit
145833.333333333 Pascal -->0.145833333333333 Megapascal (Check conversion here)
FINAL ANSWER
0.145833333333333 0.145833 Megapascal <-- Bending Stress in Column
(Calculation completed in 00.004 seconds)

Credits

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National Institute Of Technology (NIT), Hamirpur
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Indian Institute of Information Technology, Design and Manufacturing (IIITDM), Jabalpur
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13 Kernel of Hollow Circular Section Calculators

Bending Stress for Hollow Circular section given Diameter
Go Bending Stress in Column = Moment due to eccentric load/((pi/(32*Outer Diameter of Hollow Circular Section))*((Outer Diameter of Hollow Circular Section^4)-(Hollow Circular Section Inner Diameter^4)))
Internal Diameter given Maximum Eccentricity of Load for Hollow Circular Section
Go Hollow Circular Section Inner Diameter = sqrt((Eccentricity of Loading*8*Outer Diameter of Hollow Circular Section)-(Outer Diameter of Hollow Circular Section^2))
Section modulus hollow circular section
Go Section Modulus = (pi/(32*Outer Diameter of Hollow Circular Section))*((Outer Diameter of Hollow Circular Section^4)-(Hollow Circular Section Inner Diameter^4))
Inner Diameter of Hollow Circular Section given Diameter of kernel
Go Hollow Circular Section Inner Diameter = sqrt((4*Outer Diameter of Hollow Circular Section*Diameter of kernel)-(Outer Diameter of Hollow Circular Section^2))
Maximum value of eccentricity of load for hollow circular section
Go Eccentricity of Loading = (1/(8*Outer Diameter of Hollow Circular Section))*((Outer Diameter of Hollow Circular Section^2)+(Hollow Circular Section Inner Diameter^2))
Diameter of kernel for hollow circular section
Go Diameter of kernel = ((Outer Diameter of Hollow Circular Section^2)+(Hollow Circular Section Inner Diameter^2))/(4*Outer Diameter of Hollow Circular Section)
Section Modulus given Bending Stress and Eccentric Load on Hollow Circular Section
Go Section Modulus = (Eccentricity of Loading*Eccentric load on column)/Bending Stress in Column
Bending Stress for Hollow Circular Section using Eccentric Load and Eccentricity
Go Bending Stress in Column = (Eccentricity of Loading*Eccentric load on column)/Section Modulus
Eccentric Load given Bending Stress on Hollow Circular Section
Go Eccentric load on column = (Bending Stress in Column*Section Modulus)/Eccentricity of Loading
Eccentricity given Bending Stress on Hollow Circular Section
Go Eccentricity of Loading = (Bending Stress in Column*Section Modulus)/Eccentric load on column
Moment due to Eccentric Load Bending Stress on Hollow Circular Section
Go Moment due to eccentric load = Bending Stress in Column*Section Modulus
Section Modulus given Bending Stress on Hollow Circular Section
Go Section Modulus = Moment due to eccentric load/Bending Stress in Column
Bending stress for hollow circular section
Go Bending Stress in Column = Moment due to eccentric load/Section Modulus

Bending Stress for Hollow Circular Section using Eccentric Load and Eccentricity Formula

Bending Stress in Column = (Eccentricity of Loading*Eccentric load on column)/Section Modulus
σb = (eload*P)/S

Is bending stress a normal stress?

Bending stress is a more specific type of normal stress. The stress at the horizontal plane of the neutral is zero. The bottom fibers of the beam undergo normal tensile stress. It can be concluded therefore that the value of the bending stress will vary linearly with distance from the neutral axis.

How to Calculate Bending Stress for Hollow Circular Section using Eccentric Load and Eccentricity?

Bending Stress for Hollow Circular Section using Eccentric Load and Eccentricity calculator uses Bending Stress in Column = (Eccentricity of Loading*Eccentric load on column)/Section Modulus to calculate the Bending Stress in Column, The Bending stress for hollow circular section using eccentric load and eccentricity formula is defined as a more specific type of normal stress. Bending Stress in Column is denoted by σb symbol.

How to calculate Bending Stress for Hollow Circular Section using Eccentric Load and Eccentricity using this online calculator? To use this online calculator for Bending Stress for Hollow Circular Section using Eccentric Load and Eccentricity, enter Eccentricity of Loading (eload), Eccentric load on column (P) & Section Modulus (S) and hit the calculate button. Here is how the Bending Stress for Hollow Circular Section using Eccentric Load and Eccentricity calculation can be explained with given input values -> 1.2E-6 = (0.025*7000)/0.0012.

FAQ

What is Bending Stress for Hollow Circular Section using Eccentric Load and Eccentricity?
The Bending stress for hollow circular section using eccentric load and eccentricity formula is defined as a more specific type of normal stress and is represented as σb = (eload*P)/S or Bending Stress in Column = (Eccentricity of Loading*Eccentric load on column)/Section Modulus. Eccentricity of Loading is the distance between the actual line of action of loads and the line of action that would produce a uniform stress over the cross section of the specimen, Eccentric load on column is the load that causes direct stress as well as bending stress & Section Modulus is a geometric property for a given cross-section used in the design of beams or flexural members.
How to calculate Bending Stress for Hollow Circular Section using Eccentric Load and Eccentricity?
The Bending stress for hollow circular section using eccentric load and eccentricity formula is defined as a more specific type of normal stress is calculated using Bending Stress in Column = (Eccentricity of Loading*Eccentric load on column)/Section Modulus. To calculate Bending Stress for Hollow Circular Section using Eccentric Load and Eccentricity, you need Eccentricity of Loading (eload), Eccentric load on column (P) & Section Modulus (S). With our tool, you need to enter the respective value for Eccentricity of Loading, Eccentric load on column & Section Modulus 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 Bending Stress in Column?
In this formula, Bending Stress in Column uses Eccentricity of Loading, Eccentric load on column & Section Modulus. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Bending Stress in Column = Moment due to eccentric load/((pi/(32*Outer Diameter of Hollow Circular Section))*((Outer Diameter of Hollow Circular Section^4)-(Hollow Circular Section Inner Diameter^4)))
  • Bending Stress in Column = Moment due to eccentric load/Section Modulus
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