Stress Calculator
Calculate different types of stresses in materials under various loading conditions
Results & Information

About Axial Stress

Axial stress (σ) is the force per unit area acting perpendicular to the cross-section of a member. It's calculated using σ = F/A, where F is the applied force and A is the cross-sectional area.

More Information

Understanding Stress Analysis
Key concepts and applications in engineering design

What is Stress?

Stress is the internal resistance or reaction of a material to external forces. It is measured as force per unit area and is a critical factor in determining whether a component will deform or fail under given loading conditions.

The total stress at a point often includes multiple components acting in different directions. Understanding these components and their interactions is essential for proper engineering design.

Axial Stress

Force acting perpendicular to a cross-section:

σ = F/A

Where:

  • F = applied force
  • A = cross-sectional area

Shear Stress

Force acting parallel to a cross-section:

τ = F/A

Where:

  • F = applied force
  • A = area of the shear surface

Bending Stress

Stress due to bending moments:

σ = My/I

Where:

  • M = bending moment
  • y = distance from neutral axis
  • I = moment of inertia

Torsional Stress

Stress due to twisting moments:

τ = Tr/J

Where:

  • T = applied torque
  • r = radius from center
  • J = polar moment of inertia

Von Mises Stress

Combines stresses for failure prediction:

σᵥ = √(σₓ² - σₓσᵧ + σᵧ² + 3τₓᵧ²)

Where:

  • σₓ = normal stress in x-direction
  • σᵧ = normal stress in y-direction
  • τₓᵧ = shear stress in xy-plane

Failure Theories

Several theories predict material failure:

  • Maximum Normal Stress Theory
  • Maximum Shear Stress (Tresca)
  • Distortion Energy (von Mises)
  • Mohr's Theory
  • Coulomb-Mohr Theory

Most common criterion:

SF = σₑ / σᵢ

Where SF = safety factor, σₑ = yield strength, σᵢ = induced stress

Safety Considerations

The safety factor is the ratio of the material's yield strength to the calculated stress. Generally:

  • SF < 1: Failure is likely to occur
  • SF = 1-1.5: Marginal safety, suitable for well-controlled conditions
  • SF = 1.5-2: Typical for well-understood static loads
  • SF = 2-3: Used for average conditions with some uncertainties
  • SF > 3: Used for uncertain loading conditions or critical applications

Important Notes

  • Stress units are typically in Pascal (Pa) or its multiples (MPa, GPa).
  • Stress analysis assumes linear-elastic behavior for most calculations.
  • Cross-sectional properties significantly influence stress distribution.
  • Temperature changes can introduce thermal stresses.
  • Stress concentrations occur at geometric discontinuities (holes, fillets, etc.).
  • Fatigue failure can occur at stress levels below the material's yield strength when subjected to cyclic loading.