Young's Modulus Reference Table

Elastic modulus, shear modulus, and Poisson's ratio for materials

Reference table of Young's modulus (E), shear modulus (G), and Poisson's ratio for common engineering materials, with a calculator for axial stretch from stress using Hooke's law. It runs free in your browser on Gera Tools, with nothing uploaded.

Last updated Source: Gera Tools

What is Young's modulus?

Young's modulus (E) is the ratio of tensile stress to tensile strain in the elastic region — it measures stiffness. A high E means the material resists stretching: steel at about 200 GPa is roughly three times stiffer than aluminium at 69 GPa.

Young’s modulus tells you how stiff a material is — how much it stretches under load. This reference lists Young’s modulus, shear modulus, and Poisson’s ratio for common materials and computes elastic strain from an applied stress using Hooke’s law.

How it works

In the elastic region stress and strain are proportional, and the constant of proportionality is Young’s modulus E:

strain = stress / E

For an isotropic material the three elastic constants are linked by:

E = 2 * G * (1 + ν)

so the shear modulus G and Poisson’s ratio ν are not independent of E. The calculator takes a stress in MPa, divides by E (converted to MPa), and reports the dimensionless strain and its percent elongation. A 250 MPa stress in steel (E ≈ 200000 MPa) gives a strain of 250 / 200000 = 0.00125, about 0.125 percent.

Material comparisons at a glance

The wide range of Young’s modulus values across materials is one of the key reasons engineers choose one over another for a given application. A few illustrative points:

MaterialYoung’s modulus (approx.)Character
Diamond~1000 GPaStiffer than any common engineering material
Steel (carbon and alloy)~200 GPaThe backbone of structural engineering
Titanium alloys~110 GPaHalf the stiffness of steel at ~60% the density
Aluminium alloys~69 GPaOne-third the stiffness of steel; much lighter
Concrete~30 GPaStiff in compression, weak in tension
Wood (along grain)8–15 GPaHighly direction-dependent
Rubber~0.01–0.1 GPaFour to five orders of magnitude softer than steel

This spread explains, for example, why an aluminium aircraft structure deflects measurably more than an equivalent steel one under the same aerodynamic load, and why composite designs mix fibres with very different moduli.

Worked example

For example, a steel rod with cross-section 10 mm × 10 mm carries a tensile load of 25 kN. Stress = 25,000 N ÷ (0.01 m × 0.01 m) = 250 MPa. With E = 200,000 MPa, strain = 250 ÷ 200,000 = 0.00125, or 0.125 percent elongation. A 1-metre section of that rod would stretch by 1.25 mm under that load.

Running the same calculation with aluminium (E ≈ 69,000 MPa) gives a strain of ~0.0036 and 3.6 mm of stretch — nearly three times more deflection under the same force.

Tips and notes

  • Stay in the elastic region: Hooke’s law only holds below the yield stress. Computing a large strain does not mean the material behaves that way — it means it has yielded or fractured.
  • All carbon and alloy steels share roughly 200 GPa — alloying changes strength and toughness far more than it changes stiffness.
  • Most metals have Poisson’s ratio near 0.3; rubber approaches the incompressible limit of 0.5; cork is near zero.
  • Modulus drops slowly with temperature. The calculator gives a room-temperature value; use a corrected figure for high-temperature or cryogenic service.