Direct Stress for Circular Section Solution

STEP 0: Pre-Calculation Summary
Formula Used
Direct Stress = (4*Eccentric Load on Column)/(pi*(Diameter^2))
σ = (4*P)/(pi*(d^2))
This formula uses 1 Constants, 3 Variables
Constants Used
pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288
Variables Used
Direct Stress - (Measured in Pascal) - Direct Stress is defined as axial thrust acting per unit area.
Eccentric Load on Column - (Measured in Newton) - Eccentric Load on Column is the load that causes direct stress as well as bending stress.
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
Eccentric Load on Column: 7 Kilonewton --> 7000 Newton (Check conversion ​here)
Diameter: 142 Millimeter --> 0.142 Meter (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
σ = (4*P)/(pi*(d^2)) --> (4*7000)/(pi*(0.142^2))
Evaluating ... ...
σ = 442009.363873544
STEP 3: Convert Result to Output's Unit
442009.363873544 Pascal -->0.442009363873544 Megapascal (Check conversion ​here)
FINAL ANSWER
0.442009363873544 0.442009 Megapascal <-- Direct Stress
(Calculation completed in 00.004 seconds)

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Created by Anshika Arya
National Institute Of Technology (NIT), Hamirpur
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Verified by Kumar Siddhant
Indian Institute of Information Technology, Design and Manufacturing (IIITDM), Jabalpur
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Middle Quarter Rule for Circular Section Calculators

Eccentricity of Load given Minimum Bending Stress
​ LaTeX ​ Go Eccentricity of Loading = (((4*Eccentric Load on Column)/(pi*(Diameter^2)))-Minimum Bending Stress)*((pi*(Diameter^3))/(32*Eccentric Load on Column))
Condition for Maximum Bending Stress given Diameter
​ LaTeX ​ Go Diameter = 2*Distance from Neutral Layer
Diameter of Circular Section given Maximum Value of Eccentricity
​ LaTeX ​ Go Diameter = 8*Eccentricity of Loading
Maximum value of Eccentricity for No Tensile Stress
​ LaTeX ​ Go Eccentricity of Loading = Diameter/8

Direct Stress for Circular Section Formula

​LaTeX ​Go
Direct Stress = (4*Eccentric Load on Column)/(pi*(Diameter^2))
σ = (4*P)/(pi*(d^2))

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 Direct Stress for Circular Section?

Direct Stress for Circular Section calculator uses Direct Stress = (4*Eccentric Load on Column)/(pi*(Diameter^2)) to calculate the Direct Stress, The Direct Stress for Circular Section formula is defined as a measure of the internal force per unit area that occurs within a circular section of a material when an external force is applied, providing a way to calculate the stress experienced by the material under various loads. Direct Stress is denoted by σ symbol.

How to calculate Direct Stress for Circular Section using this online calculator? To use this online calculator for Direct Stress for Circular Section, enter Eccentric Load on Column (P) & Diameter (d) and hit the calculate button. Here is how the Direct Stress for Circular Section calculation can be explained with given input values -> 4.4E-7 = (4*7000)/(pi*(0.142^2)).

FAQ

What is Direct Stress for Circular Section?
The Direct Stress for Circular Section formula is defined as a measure of the internal force per unit area that occurs within a circular section of a material when an external force is applied, providing a way to calculate the stress experienced by the material under various loads and is represented as σ = (4*P)/(pi*(d^2)) or Direct Stress = (4*Eccentric Load on Column)/(pi*(Diameter^2)). Eccentric Load on Column is the load that causes direct stress as well as bending stress & 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 Direct Stress for Circular Section?
The Direct Stress for Circular Section formula is defined as a measure of the internal force per unit area that occurs within a circular section of a material when an external force is applied, providing a way to calculate the stress experienced by the material under various loads is calculated using Direct Stress = (4*Eccentric Load on Column)/(pi*(Diameter^2)). To calculate Direct Stress for Circular Section, you need Eccentric Load on Column (P) & Diameter (d). With our tool, you need to enter the respective value for Eccentric Load on Column & Diameter and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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