Direct Stress Solution

STEP 0: Pre-Calculation Summary
Formula Used
Direct Stress = Axial Thrust/Cross sectional area
σ = Paxial/Acs
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 = Paxial/Acs --> 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)

Credits

Created by Pragati Jaju
College Of Engineering (COEP), Pune
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Verified by Kethavath Srinath
Osmania University (OU), Hyderabad
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16 Stress Calculators

Stress due to Impact Loading
Go Stress due to Loading = Load*(1+sqrt(1+(2*Cross sectional area*Bending Stress*Height at which load falls)/(Load*Length of Weld)))/Cross sectional area
Brinell Hardness Number
Go Brinell Hardness Number = Load/((0.5*pi*Diameter of Ball Indentor)*(Diameter of Ball Indentor-(Diameter of Ball Indentor^2-Diameter of Indentation^2)^0.5))
Thermal Stress in Tapered Bar
Go Thermal Stress = (4*Load*Length of Weld)/(pi*Diameter of Bigger End*Diameter of Smaller End*Bending Stress)
Beam Shear Stress
Go Shearing Stress = (Total Shear Force*First Moment of Area)/(Moment of Inertia*Thickness of Material)
Shearing Stress
Go Shearing Stress = (Shearing Force*First Moment of Area)/(Moment of Inertia*Thickness of Material)
Shear Stress in Double Parallel Fillet Weld
Go Shearing Stress = Load on Double Parallel Fillet Weld/(0.707*Length of Weld*Leg of Weld)
Thermal Stress
Go Thermal Stress = Coefficient of Thermal Expansion*Bending Stress*Change in Temperature
Bending Stress
Go Bending Stress = Bending Moment*Distance from Neutral Axis/Moment of Inertia
Torsional Shear Stress
Go Shearing Stress = (Torque*Radius of Shaft)/Polar Moment of Inertia
Shear Stress of Circular Beam
Go Stress on Body = (4*Shearing Force)/(3*Cross sectional area)
Stress due to Gradual Loading
Go Stress due to Gradual Loading = Force/Cross sectional area
Maximum Shearing Stress
Go Stress on Body = (1.5*Shearing Force)/Cross sectional area
Shear Stress
Go Shearing Stress = Tangential Force/Cross sectional area
Bulk Stress
Go Bulk Stress = Normal Inward Force/Cross sectional area
Direct Stress
Go Direct Stress = Axial Thrust/Cross sectional area
Stress due to Sudden Loading
Go Stress on Body = 2*Force/Cross sectional area

Direct Stress Formula

Direct Stress = Axial Thrust/Cross sectional area
σ = Paxial/Acs

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 is defined as 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 (Paxial) & Cross sectional area (Acs) 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 is defined as the stress produced by the axial force acting on a unit area.It is also called as normal stress and is represented as σ = Paxial/Acs 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 is defined as 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 (Paxial) & Cross sectional area (Acs). 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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