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Direct Stress Calculator

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Stress Strain Stress and Strain

✖The Axial Thrust is the resultant force of all the axial forces (F) acting on the object or material.ⓘ Axial Thrust [P_axial]			+10% -10%
✖Cross sectional area is the area of a two-dimensional shape that is obtained when a three-dimensional shape is sliced perpendicular to some specified axis at a point.ⓘ Cross Sectional Area [A_cs]			+10% -10%

✖The Direct Stress is defined as axial thrust acting per unit area.ⓘ Direct Stress [σ]

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Direct Stress Solution

STEP 0: Pre-Calculation Summary

Formula Used

Direct Stress = Axial Thrust/Cross Sectional Area
σ = P_axial/A_cs
This formula uses 3 Variables

Variables Used

Direct Stress - (Measured in Pascal) - The Direct Stress is defined as axial thrust acting per unit area.
Axial Thrust - (Measured in Newton) - The Axial Thrust is the resultant force of all the axial forces (F) acting on the object or material.
Cross Sectional Area - (Measured in Square Meter) - Cross sectional area is the area of a two-dimensional shape that is obtained when a three-dimensional shape is sliced perpendicular to some specified axis at a point.

STEP 1: Convert Input(s) to Base Unit

Axial Thrust: 2.332 Newton --> 2.332 Newton No Conversion Required
Cross Sectional Area: 1333.4 Square Millimeter --> 0.0013334 Square Meter (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

σ = P_axial/A_cs --> 2.332/0.0013334

Evaluating ... ...

σ = 1748.91255437228

STEP 3: Convert Result to Output's Unit

1748.91255437228 Pascal --> No Conversion Required

FINAL ANSWER

1748.91255437228 ≈ 1748.913 Pascal <-- Direct Stress

(Calculation completed in 00.004 seconds)

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Created by Pragati Jaju

College Of Engineering (COEP), Pune

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Osmania University (OU), Hyderabad

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< Stress Calculators

Beam Shear Stress

LaTeX Go Beam Shear Stress = (Total Shear Force*First Moment of Area)/(Moment of Inertia*Thickness of Material)

Bending Stress

LaTeX Go Bending Stress = Bending Moment*Distance from Neutral Axis/Moment of Inertia

Bulk Stress

LaTeX Go Bulk Stress = Normal Inward Force/Cross Sectional Area

Direct Stress

LaTeX Go Direct Stress = Axial Thrust/Cross Sectional Area

Direct Stress Formula

LaTeX Go

Direct Stress = Axial Thrust/Cross Sectional Area
σ = P_axial/A_cs

What is Direct Stress?

The Direct Stress is the stress produced by the axial force acting on a unit area.Whenever a body is subjected to an axial tension or compression, a direct stress comes into play at every section of body.

How to Calculate Direct Stress?

Direct Stress calculator uses Direct Stress = Axial Thrust/Cross Sectional Area to calculate the Direct Stress, The Direct Stress formula is defined as themeasure of the stress produced by the axial force acting on a unit area. It is also called as normal stress. Direct Stress is denoted by σ symbol.

How to calculate Direct Stress using this online calculator? To use this online calculator for Direct Stress, enter Axial Thrust (P_axial) & Cross Sectional Area (A_cs) and hit the calculate button. Here is how the Direct Stress calculation can be explained with given input values -> 1748.913 = 2.332/0.0013334.

FAQ

What is Direct Stress?

The Direct Stress formula is defined as themeasure of the stress produced by the axial force acting on a unit area. It is also called as normal stress and is represented as σ = P_axial/A_cs or Direct Stress = Axial Thrust/Cross Sectional Area. The Axial Thrust is the resultant force of all the axial forces (F) acting on the object or material & Cross sectional area is the area of a two-dimensional shape that is obtained when a three-dimensional shape is sliced perpendicular to some specified axis at a point.

How to calculate Direct Stress?

The Direct Stress formula is defined as themeasure of the stress produced by the axial force acting on a unit area. It is also called as normal stress is calculated using Direct Stress = Axial Thrust/Cross Sectional Area. To calculate Direct Stress, you need Axial Thrust (P_axial) & Cross Sectional Area (A_cs). With our tool, you need to enter the respective value for Axial Thrust & Cross Sectional Area 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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