Stress in Steel Calculator

Category	Engineering ↺

✖moment is an overturning effect (tends to bend or turn the member) created by the force(load) acting on a structural member.ⓘ moment [M_t]			+10% -10%
✖Tensile Reinforcement Area is defined as the area a composite material in which concrete's relatively low tensile strength and ductility.ⓘ Tensile Reinforcement Area [A_s]			+10% -10%
✖Ratio j is defined as the ratio of distance between centroid of compression and centroid of tension to depth d.ⓘ Ratio j [j]			+10% -10%
✖Depth of the Beam is the overall depth of the cross section of the beam perpendicular to the axis of the beam.ⓘ Depth of the Beam [D]			+10% -10%

✖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 in Steel [σ]

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Kethavath Srinath

Osmania University (OU), Hyderabad

Kethavath Srinath has created this Calculator and 400+ more calculators!

Rudrani Tidke

Cummins College of Engineering for Women (CCEW), Pune

Rudrani Tidke has verified this Calculator and 50+ more calculators!

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

Deflection for Hollow Rectangle When Load in Middle

Deflection of Beam=(Greatest Safe Load*Length of the Beam^3)/(32*(Sectional Area*(Depth of the Beam^2)-Interior Cross-Sectional Area of Beam*(Interior Depth of the Beam^2))) GO

Deflection for Hollow Rectangle When Load is Distributed

Deflection of Beam=Greatest Safe Load*(Length of the Beam^3)/(52*(Sectional Area*Depth of the Beam^-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam^2)) GO

Lateral Deflection of a Pile

lateral deflection=((coefficient Ay*lateral load*(characteristic pile length^3))/pile stiffness)+((coefficient By*moment*(characteristic pile length^2))/pile stiffness) GO

Greatest Safe Load for Hollow Rectangle When Load is Distributed

Greatest Safe Load=1780*(Sectional Area*Depth of the Beam-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam)/Distance between Supports GO

Greatest Safe Load for Hollow Rectangle When Load in Middle

Greatest Safe Load=(890*(Sectional Area*Depth of the Beam-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam))/Length of the Beam GO

Deflection for Solid Rectangle When Load is Distributed

Deflection of Beam=(Greatest safe distributed load*Length of the Beam^3)/(52*Sectional Area*Depth of the Beam^2) GO

Deflection for Solid Rectangle When Load in Middle

Deflection of Beam=(Greatest Safe Load*Length of the Beam^3)/(32*Sectional Area*Depth of the Beam^2) GO

Greatest Safe Load for Solid Rectangle When Load is Distributed

Greatest safe distributed load=1780*Sectional Area*Depth of the Beam/Length of the Beam GO

Greatest Safe Load for Solid Cylinder When Load is Distributed

Greatest Safe Load=1333*(Sectional Area*Depth of the Beam)/Length of the Beam GO

Greatest Safe Load for Solid Cylinder When Load in Middle

Greatest Safe Load=(667*Sectional Area*Depth of the Beam)/Length of the Beam GO

Greatest Safe Load for Solid Rectangle When Load in Middle

Greatest Safe Load=890*Sectional Area*Depth of the Beam/Length of the Beam GO

< 11 Other formulas that calculate the same Output

Stress due to impact loading

Stress=Force*(1+sqrt(1+2*Original cross sectional area*Elastic Modulus*Height at which load 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

Thermal Stress

Stress=Coefficient of thermal expansion*Elastic Modulus*Change in temperature 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 on the element

Stress=Specific Weight*Length of Rod 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

Stress=Force/Area GO

Stress in Steel Formula

Stress=moment/(Tensile Reinforcement Area*Ratio j*Depth of the Beam)
σ=M<sub>t</sub>/(A<sub>s*j*D)

More formulas

Stress in Concrete GO

Bending Moment when Stress in Concrete is Given GO

Width of Beam when Stress in Concrete is Given GO

Depth of Beam when Stress in Concrete is Given GO

Stress in Steel When Cross-Sectional Reinforcing Tensile Area to Beam Area Ratio is Given GO

Depth of Roof and Floor Slabs GO

Depth of Light Beams GO

Depth of Heavy Beams and Girders GO

Define stress?

In physics, stress is the force acting on the unit area of a material. The effect of stress on a body is named as strain. Stress can deform the body. How much force material experience can be measured using stress units.

How to Calculate Stress in Steel?

Stress in Steel calculator uses Stress=moment/(Tensile Reinforcement Area*Ratio j*Depth of the Beam) to calculate the Stress, The Stress in Steel formula is defined as the force acting on the unit area of a material. The effect of stress on a body is named as strain. Stress can deform the body. How much force material experience can be measured using stress units. Stress and is denoted by σ symbol.

How to calculate Stress in Steel using this online calculator? To use this online calculator for Stress in Steel, enter moment (M_t), Tensile Reinforcement Area (A_s), Ratio j (j) and Depth of the Beam (D) and hit the calculate button. Here is how the Stress in Steel calculation can be explained with given input values -> 39370.08 = 1/(0.0001*1*0.254000000001016).

FAQ

What is Stress in Steel?

The Stress in Steel formula is defined as the force acting on the unit area of a material. The effect of stress on a body is named as strain. Stress can deform the body. How much force material experience can be measured using stress units and is represented as σ=M_t/(A_s*j*D) or Stress=moment/(Tensile Reinforcement Area*Ratio j*Depth of the Beam). moment is an overturning effect (tends to bend or turn the member) created by the force(load) acting on a structural member, Tensile Reinforcement Area is defined as the area a composite material in which concrete's relatively low tensile strength and ductility, Ratio j is defined as the ratio of distance between centroid of compression and centroid of tension to depth d and Depth of the Beam is the overall depth of the cross section of the beam perpendicular to the axis of the beam.

How to calculate Stress in Steel?

The Stress in Steel formula is defined as the force acting on the unit area of a material. The effect of stress on a body is named as strain. Stress can deform the body. How much force material experience can be measured using stress units is calculated using Stress=moment/(Tensile Reinforcement Area*Ratio j*Depth of the Beam). To calculate Stress in Steel, you need moment (M_t), Tensile Reinforcement Area (A_s), Ratio j (j) and Depth of the Beam (D). With our tool, you need to enter the respective value for moment, Tensile Reinforcement Area, Ratio j and Depth of the Beam 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 moment, Tensile Reinforcement Area, Ratio j and Depth of the Beam. We can use 11 other way(s) to calculate the same, which is/are as follows -

Stress=Force/Area
Stress=Force/Area
Stress=2*Force/Area
Stress=Force*(1+sqrt(1+2*Original cross sectional area*Elastic Modulus*Height at which load 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=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=Force/Area
Stress=Normal Force/Shear Area
Stress=Specific Weight*Length of Rod

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