Normal & Shear Stress
Calculate normal stress (σ = N/A) and shear stress (τ = F/A) for any cross-section.
Inputs
Formula Interpretation
Normal Stress — Formula ①
is the internal force perpendicular to the cross-section (N); is the cross-sectional area (mm²); is the resulting normal stress (MPa).
Shear Stress — Formula ②
is the internal force parallel to the cross-section (N); is the cross-sectional area (mm²); is the resulting shear stress (MPa).
Circular Section Area
is the diameter (mm); is the resulting cross-sectional area (mm²).
Knowledge Points
Normal Stress
The stress arising from internal forces perpendicular to a cross-section is called normal stress (σ). Tensile loading produces positive normal stress; compressive loading produces negative normal stress.
Shear Stress
The stress arising from internal forces parallel to a cross-section is called shear stress (τ). Shear stress causes angular (distortional) deformation of the material.
Five Types of Stress
There are five types of stress corresponding to five load types: tension/compression, shear, bending and torsion. Bending stress is a combination of tensile and compressive normal stress. Torsional stress is a form of shear stress. Stress is a tensor quantity.
Worked Example
As shown in the figure, a circular rod with diameter is subjected to tensile forces of at both ends. Find the tensile normal stress in the rod.
Step 1 — Identify the internal force
Step 2 — Compute the cross-sectional area
Step 3 — Apply Formula ①
The tensile normal stress in the rod is .
Extended Knowledge
- •In structural engineering, normal stress analysis is fundamental for designing columns, beams and cables under axial loading.
- •Shear stress governs the design of bolts, pins, welds and adhesive joints that transmit loads through shear.
- •When a member is simultaneously subjected to normal and shear stresses (combined loading), failure criteria such as von Mises or Tresca must be applied for safe design.
- •For composite or variable cross-section members, stress distributions are non-uniform; advanced methods such as finite element analysis are required.
- •Dynamic loads introduce stress concentrations at notches, holes and section changes. Fatigue analysis must apply stress concentration factors () to predict service life.