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Stress Solution

STEP 0: Pre-Calculation Summary
Formula Used
stress = Force/Area
σ = F/A
This formula uses 2 Variables
Variables Used
Force - Force is any interaction that, when unopposed, will change the motion of an object. In other words, a force can cause an object with mass to change its velocity. (Measured in Newton)
Area - The area is the amount of two-dimensional space taken up by an object. (Measured in Square Meter)
STEP 1: Convert Input(s) to Base Unit
Force: 2.5 Newton --> 2.5 Newton No Conversion Required
Area: 50 Square Meter --> 50 Square Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
σ = F/A --> 2.5/50
Evaluating ... ...
σ = 0.05
STEP 3: Convert Result to Output's Unit
0.05 Pascal --> No Conversion Required
FINAL ANSWER
0.05 Pascal <-- Stress
(Calculation completed in 00.016 seconds)
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11 Other formulas that you can solve using the same Inputs

Diagonal of a Rectangle when breadth and area are given
diagonal = sqrt(((Area)^2/(Breadth)^2)+(Breadth)^2) Go
Diagonal of a Rectangle when length and area are given
diagonal = sqrt(((Area)^2/(Length)^2)+(Length)^2) Go
Side of a Kite when other side and area are given
side_a = (Area*cosec(Angle Between Sides))/Side B Go
Work
work = Force*Displacement*cos(Angle A) Go
Torque
torque = Force*Displacement*sin(θ) Go
Impulse
impulse = Force*Time Taken to Travel Go
Surface Tension
surface_tension = Force/Length Go
Buoyant Force
buoyant_force = Pressure*Area Go
Perimeter of a square when area is given
perimeter = 4*sqrt(Area) Go
Diagonal of a Square when area is given
diagonal = sqrt(2*Area) Go
Pressure when force and area are given
pressure = Force/Area Go

11 Other formulas that calculate the same Output

Total Stress in Eccentric Loading when Load doesn't lie on a Plane
stress = (Axial Load/Cross sectional area)+((Eccentricity with respect to Principal axis YY*Axial Load*Distance from YY to outermost Fiber)/(Moment of Inertia about Y-axis))+((Eccentricity with respect to Principal axis XX*Axial Load*Distance from XX to outermost Fiber)/(Moment of Inertia about X-axis)) Go
Stress due to impact loading
stress = Force*(1+sqrt(1+2*Original cross sectional area*Elastic Modulus*Height at which Force falls/Force*Length))/Original cross sectional area Go
Thermal Stress in tapered bar
stress = (4*Force*Length)/(pi*Diameter of bigger end*Diameter of smaller end*Elastic Modulus) Go
Stress in Concrete
stress = 2*Bending moment/(Ratio k*Ratio j*Beam Width*Depth of the Beam^2) Go
Stress in Steel When Cross-Sectional Reinforcing Tensile Area to Beam Area Ratio is Given
stress = Bending moment/(Ratio p*Ratio j*Beam Width*Depth of the Beam^2) Go
Stress in Steel
stress = moment/(Tensile Reinforcement Area*Ratio j*Depth of the Beam) Go
Thermal Stress
stress = Coefficient of thermal expansion*Elastic Modulus*Change in temperature Go
Mean normal stress in shear plane for given normal force & shear area
stress = Normal Force/Shear Area Go
Stress due to sudden loading
stress = 2*Force/Area Go
Normal stress or longitudinal stress
stress = Force/Area Go
Stress due to gradual loading
stress = Force/Area Go

Stress Formula

stress = Force/Area
σ = F/A

How to Calculate Stress?

Stress calculator uses stress = Force/Area to calculate the Stress, The stress applied to a material is the force per unit area applied to the material. The maximum stress a material can stand before it breaks is called the breaking stress or ultimate tensile stress. Stress and is denoted by σ symbol.

How to calculate Stress using this online calculator? To use this online calculator for Stress, enter Force (F) and Area (A) and hit the calculate button. Here is how the Stress calculation can be explained with given input values -> 0.05 = 2.5/50.

FAQ

What is Stress?
The stress applied to a material is the force per unit area applied to the material. The maximum stress a material can stand before it breaks is called the breaking stress or ultimate tensile stress and is represented as σ = F/A or stress = Force/Area. Force is any interaction that, when unopposed, will change the motion of an object. In other words, a force can cause an object with mass to change its velocity and The area is the amount of two-dimensional space taken up by an object.
How to calculate Stress?
The stress applied to a material is the force per unit area applied to the material. The maximum stress a material can stand before it breaks is called the breaking stress or ultimate tensile stress is calculated using stress = Force/Area. To calculate Stress, you need Force (F) and Area (A). With our tool, you need to enter the respective value for Force and Area 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 Stress?
In this formula, Stress uses Force and Area. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • stress = Force/Area
  • stress = 2*Force/Area
  • stress = Force*(1+sqrt(1+2*Original cross sectional area*Elastic Modulus*Height at which Force falls/Force*Length))/Original cross sectional area
  • stress = Coefficient of thermal expansion*Elastic Modulus*Change in temperature
  • stress = (4*Force*Length)/(pi*Diameter of bigger end*Diameter of smaller end*Elastic Modulus)
  • stress = (Axial Load/Cross sectional area)+((Eccentricity with respect to Principal axis YY*Axial Load*Distance from YY to outermost Fiber)/(Moment of Inertia about Y-axis))+((Eccentricity with respect to Principal axis XX*Axial Load*Distance from XX to outermost Fiber)/(Moment of Inertia about X-axis))
  • stress = 2*Bending moment/(Ratio k*Ratio j*Beam Width*Depth of the Beam^2)
  • stress = Bending moment/(Ratio p*Ratio j*Beam Width*Depth of the Beam^2)
  • stress = moment/(Tensile Reinforcement Area*Ratio j*Depth of the Beam)
  • stress = Force/Area
  • stress = Normal Force/Shear Area
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