Hariharan V S
Indian Institute of Technology (IIT), Chennai
Hariharan V S has created this Calculator and 25+ more calculators!

## < 11 Other formulas that you can solve using the same Inputs

Brinell Hardness Number
Brinell Hardness Number=Force/((0.5*pi*Diameter of the ball indentor)*(Diameter of the ball indentor-((Diameter of the ball indentor^2)-(Diameter of indentation^2))^0.5)) GO
Stress=Force*(1+sqrt(1+2*Original cross sectional area*Elastic Modulus*Height at which load falls/Force*Length))/Original cross sectional area GO
Heat Transfer Through Plane Wall or Surface
Heat Rate=-Thermal Conductivity*Original cross sectional area*(Outside Temperature-Inside Temperature)/Width GO
Percent cold work
Percent cold work=100*(Original cross sectional area-Area after deformation)/Original cross sectional area GO
Percent reduction in area
Percent reduction in area=(Original cross sectional area-Fracture area)*100/Original cross sectional area GO
Elongation circular tapered bar
Elongation=4*Force*Length/(pi*Diameter of bigger end*Diameter of smaller end *Elastic Modulus) GO
Elongation of prismatic bar due to its own weight
Elongation=2*Force*Length of Rod/(Area*Elastic Modulus) GO
Hooke's law
Young's Modulus=Force*Elongation/(Area*Initial length) GO
Axial elongation of prismatic bar due to external load
Elongation=Force*Length of Rod/(Area*Elastic Modulus) GO
Strain Energy if applied tension load is given
Strain Energy=Force^2*Length/(2*Area*Young's Modulus) GO
Aspiration Effect
Aspiration Effect=Area/Original cross sectional area GO

### Engineering stress Formula

Engineering stress=Force/Original cross sectional area
More formulas
Engineering strain GO
ASTM grain size number to Number of grains GO
Percent elongation GO
Percent reduction in area GO
True strain GO
Modulus of resilience GO
True stress GO
True strain from Engineering strain GO
Strain hardening exponent GO
Tensile strength from Brinell hardness GO
Brinell hardness GO
Vickers hardness GO
Knoop hardness GO
Resolved shear stress GO
Safe stress GO
Percent cold work GO
Critical stress for crack propagation GO
Stress concentration factor GO
Maximum stress at crack tip GO
Mean stress of stress cycle (fatigue) GO
Range of stress (fatigue) GO
Stress amplitude (fatigue) GO
Stress ratio (fatigue) GO
Maximum shear stress from Tresca criterion GO
Maximum shear stress from von mises criterion GO
Hall - Petch Relation GO
Fracture toughness GO

## Engineering Stress

Engineering stress is commonly used in design of components and considers only the original area of cross section that is, before the application of load.

## How to Calculate Engineering stress?

Engineering stress calculator uses Engineering stress=Force/Original cross sectional area to calculate the Engineering stress, Engineering stress is the force acting perpendicular to the original area of cross section. Engineering stress and is denoted by σ symbol.

How to calculate Engineering stress using this online calculator? To use this online calculator for Engineering stress, enter Force (F) and Original cross sectional area (A0) and hit the calculate button. Here is how the Engineering stress calculation can be explained with given input values -> 1 = 1000/0.001.

### FAQ

What is Engineering stress?
Engineering stress is the force acting perpendicular to the original area of cross section and is represented as σ=F/A0 or Engineering stress=Force/Original cross sectional area. Force is the instantaneous load applied perpendicular to the specimen cross section and The original cross sectional area before any load is applied.
How to calculate Engineering stress?
Engineering stress is the force acting perpendicular to the original area of cross section is calculated using Engineering stress=Force/Original cross sectional area. To calculate Engineering stress, you need Force (F) and Original cross sectional area (A0). With our tool, you need to enter the respective value for Force and Original 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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