Maximum value of eccentricity for no tensile stress Calculator

✖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.ⓘ Maximum value of eccentricity for no tensile stress [e_load]

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Maximum value of eccentricity for no tensile stress

Formula

`"e"_{"load"} = "d"/8`

Example

`"17.75mm"="142mm"/8`

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Maximum value of eccentricity for no tensile stress Solution

STEP 0: Pre-Calculation Summary

Formula Used

Eccentricity of Loading = Diameter/8
e_load = d/8
This formula uses 2 Variables

Variables Used

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.
Diameter - (Measured in Meter) - Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.

STEP 1: Convert Input(s) to Base Unit

Diameter: 142 Millimeter --> 0.142 Meter (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

e_load = d/8 --> 0.142/8

Evaluating ... ...

e_load = 0.01775

STEP 3: Convert Result to Output's Unit

0.01775 Meter -->17.75 Millimeter (Check conversion here)

FINAL ANSWER

17.75 Millimeter <-- Eccentricity of Loading

(Calculation completed in 00.020 seconds)

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Home » Physics » Strength of Materials » Direct And Bending Stress » Middle Quarter Rule For Circular Section » Maximum value of eccentricity for no tensile stress

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National Institute Of Technology (NIT), Hamirpur

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< 18 Middle Quarter Rule For Circular Section Calculators

Eccentricity of Load given Minimum Bending Stress

Go Eccentricity of Loading = (((4*Eccentric load on column)/(pi*(Diameter^2)))-Minimum Bending Stress)*((pi*(Diameter^3))/(32*Eccentric load on column))

Minimum Bending Stress given Eccentric Load

Go Minimum Bending Stress = ((4*Eccentric load on column)/(pi*(Diameter^2)))*(1-((8*Eccentricity of Loading)/Diameter))

Eccentric Load given Minimum Bending Stress

Go Eccentric load on column = (Minimum Bending Stress*(pi*(Diameter^2)))*(1-((8*Eccentricity of Loading)/Diameter))/4

Eccentricity of Load given Maximum Bending Stress

Go Eccentricity of Loading = (Maximum Bending Moment*(pi*(Diameter^3)))/(32*Eccentric load on column)

Eccentric Load given maximum Bending Stress

Go Eccentric load on column = (Maximum Bending Moment*(pi*(Diameter^3)))/(32*Eccentricity of Loading)

Maximum Bending Stress given Eccentric Load

Go Maximum bending stress = (32*Eccentric load on column*Eccentricity of Loading)/(pi*(Diameter^3))

Maximum Bending Stress for Circular Section given Moment of Load

Go Maximum bending stress = (Moment due to eccentric load*Diameter of Circular section)/(2*MOI of Area of Circular Section)

Moment of Load given Maximum Bending Stress for Circular Section

Go Moment due to eccentric load = (Bending Stress in Column*(2*MOI of Area of Circular Section))/Diameter

Diameter of Circular Section given Maximum Bending Stress

Go Diameter = (Bending Stress in Column*(2*MOI of Area of Circular Section))/Moment due to eccentric load

Moment of Inertia of Circular Section given Maximum Bending Stress for Circular Section

Go MOI of Area of Circular Section = (Moment due to eccentric load*Diameter)/(2*Maximum bending stress)

Diameter of Circular Section given Direct Stress

Go Diameter = sqrt((4*Eccentric load on column)/(pi*Direct Stress))

Direct stress for circular section

Go Direct Stress = (4*Eccentric load on column)/(pi*(Diameter^2))

Eccentric load for given direct stress for circular section

Go Eccentric load on column = (Direct Stress*pi*(Diameter^2))/4

Minimum Bending Stress given Direct and Bending Stress

Go Minimum Bending Stress = Direct Stress-Bending Stress in Column

Condition for Maximum Bending Stress given Diameter

Go Diameter = 2*Distance from Neutral Layer

Condition for maximum bending stress

Go Distance from Neutral Layer = Diameter/2

Diameter of circular section if maximum value of eccentricity is known(for no tensile stress case)

Go Diameter = 8*Eccentricity of Loading

Maximum value of eccentricity for no tensile stress

Go Eccentricity of Loading = Diameter/8

Maximum value of eccentricity for no tensile stress Formula

Eccentricity of Loading = Diameter/8
e_load = d/8

What is shear stress and strain?

Shear strain is the deformation of an object or medium under shear stress. The shear modulus is the elastic modulus in this case. Shear stress is caused by forces acting along the object's two parallel surfaces.

How to Calculate Maximum value of eccentricity for no tensile stress?

Maximum value of eccentricity for no tensile stress calculator uses Eccentricity of Loading = Diameter/8 to calculate the Eccentricity of Loading, The Maximum value of eccentricity for no tensile stress formula is defined as distance between the actual line of action of compressive or tensile loads and the line of action that would produce a uniform stress over the cross section of the specimen. Eccentricity of Loading is denoted by e_load symbol.

How to calculate Maximum value of eccentricity for no tensile stress using this online calculator? To use this online calculator for Maximum value of eccentricity for no tensile stress, enter Diameter (d) and hit the calculate button. Here is how the Maximum value of eccentricity for no tensile stress calculation can be explained with given input values -> 17750 = 0.142/8.

FAQ

What is Maximum value of eccentricity for no tensile stress?

The Maximum value of eccentricity for no tensile stress formula is defined as distance between the actual line of action of compressive or tensile loads and the line of action that would produce a uniform stress over the cross section of the specimen and is represented as e_load = d/8 or Eccentricity of Loading = Diameter/8. Diameter is a straight line passing from side to side through the center of a body or figure, especially a circle or sphere.

How to calculate Maximum value of eccentricity for no tensile stress?

The Maximum value of eccentricity for no tensile stress formula is defined as distance between the actual line of action of compressive or tensile loads and the line of action that would produce a uniform stress over the cross section of the specimen is calculated using Eccentricity of Loading = Diameter/8. To calculate Maximum value of eccentricity for no tensile stress, you need Diameter (d). With our tool, you need to enter the respective value for Diameter 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 Loading?

In this formula, Eccentricity of Loading uses Diameter. We can use 2 other way(s) to calculate the same, which is/are as follows -

Eccentricity of Loading = (((4*Eccentric load on column)/(pi*(Diameter^2)))-Minimum Bending Stress)*((pi*(Diameter^3))/(32*Eccentric load on column))
Eccentricity of Loading = (Maximum Bending Moment*(pi*(Diameter^3)))/(32*Eccentric load on column)

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