Audited 27 Jul 2026·Last updated 28 Oct 2026·3 citations·Tier 2·0 uses

Young's Modulus Calculator (from Test Data)

Work out Young's modulus from a tension or compression test: force, cross-sectional area, original length and measured stretch give stress, strain and E.

Young's Modulus Calculator

Force applied along the specimen's axis. Positive for tension (pulling), negative for compression.
Cross-sectional area perpendicular to the applied force, in square metres. 0.0002 m² = 200 mm².
Unloaded (gauge) length of the specimen before force is applied.
How much the specimen actually stretched (positive) or compressed (negative) under the applied force. Cannot be zero.
Young's modulus (E)
200,000,000,000
Young's modulus in pascals: stress divided by strain, the material's stiffness within its elastic range.
Young's modulus (E)
200 GPa
Stress (σ)
25,000,000 Pa
Strain (ε)
1.250 × 10⁻⁴

Background.

Hang about 510 kg from a steel bar two metres long and 200 mm² in section and it stretches by a quarter of a millimetre. Young's modulus is the material property that predicts that stretch, and it is found the other way round: load a specimen, measure how far it extends, and divide the stress by the strain. That is the calculation done here, with E as the unknown worked back from test data. If you already know E from a handbook and want to predict how far a part will stretch, the companion stress–strain calculator runs the same equation in the other direction.

Stress is the force spread over the cross-section, F/A, in pascals. Strain is the stretch as a fraction of the original length, ΔL/L₀, a pure number. Dividing one by the other cancels the specimen's size. A bar twice as thick needs twice the force to reach the same strain, and a bar twice as long stretches twice as far under the same stress, yet both give the same E. That is why the modulus can be tabulated for a material rather than for a particular part: OpenStax's University Physics lists about 200 GPa for steel, 110 GPa for copper and 70 GPa for aluminium.

The ratio means something only while the material is behaving elastically, in the straight opening stretch of its stress–strain curve where removing the load returns the specimen to its original length. Beyond that proportional limit part of the stretch becomes permanent, strain grows faster than stress, and a modulus worked from those readings comes out too low. Nothing in the arithmetic can tell which side of the limit your numbers came from, which is why the stress is reported alongside E: compare it with the yield strength of the material you tested.

What is young's modulus calculator?

Young's modulus, also called the elastic modulus or modulus of elasticity, is the ratio of tensile or compressive stress to the strain it produces, measured within the elastic range. On a stress–strain graph it is the slope of the initial straight portion. Its SI unit is the pascal, but values for engineering materials run into the billions, so tables quote gigapascals. It measures stiffness, not strength: E says how much a part deflects under a given load, while the yield and tensile strengths say when it gives way. Aluminium at about 70 GPa stretches nearly three times as far as steel at 200 GPa under the same stress, even where the two alloys are similarly strong.

How to use this calculator.

  1. Enter the axial force in newtons: positive if the specimen was pulled, negative if it was squashed. A machine reading in kilonewtons needs multiplying by 1,000.
  2. Enter the cross-sectional area in square metres, measured across the line of the force. Divide mm² by 1,000,000; a round bar of 16 mm diameter has π × 8² ≈ 201 mm², or about 0.000201 m².
  3. Enter the original length over which the extension was measured. With a clip-on extensometer that is its gauge length (50 mm is 0.05 m), not the full length of the specimen between the grips.
  4. Enter the measured change in length with the same sign as the force. Zero is not accepted, because a specimen that did not deform gives no strain to divide by.
  5. Read E in pascals and gigapascals, then check the stress figure against the yield strength of your material before trusting the modulus.

The formula.

E = σ ⁄ ε = (F ⁄ A) ⁄ (ΔL ⁄ L₀)

E = σ / ε = (F / A) / (ΔL / L₀), which rearranges to E = F × L₀ / (A × ΔL). F is the axial force in newtons, A the cross-sectional area in square metres, L₀ the unloaded length and ΔL the change in length. Stress σ = F/A comes out in pascals (N/m²); strain ε = ΔL/L₀ is dimensionless, so E also comes out in pascals, and dividing by 10⁹ gives the gigapascal figure. These are engineering stress and strain, based on the original area and length, which is the convention modulus tables use; at elastic strains of a fraction of a percent the difference from true stress and strain is negligible. The formula also assumes the force acts along the axis so that stress is uniform across the section. Because E is inversely proportional to both A and ΔL, the smallest measurements dominate the uncertainty. In the example below, misreading a 0.25 mm extension by just 0.01 mm moves E from 200 GPa to anywhere between 192.3 and 208.3 GPa, and a 1% error in a bar's measured diameter becomes about a 2% error in area and therefore in E. If force and extension are entered with opposite signs the result is negative, which signals a sign error rather than a property of the material.

A worked example.

Example

A steel bar with a cross-section of 0.0002 m² (200 mm²) and an original length of 2 m is pulled with 5,000 N, and its extension is measured as 0.00025 m, a quarter of a millimetre. Stress is 5,000 ÷ 0.0002 = 25,000,000 Pa, or 25 MPa. Strain is 0.00025 ÷ 2 = 0.000125 (displayed as 1.250 × 10⁻⁴), which engineers would call 125 microstrain. Young's modulus is the ratio: 25,000,000 ÷ 0.000125 = 200,000,000,000 Pa, or 200 GPa, the value tables give for steel. The stress check passes comfortably. At 25 MPa the bar is loaded to about a tenth of the 250 MPa yield strength of ordinary mild structural steel, so the reading comes from the straight part of the curve. The same numbers also give the bar's stiffness as a spring: 5,000 N ÷ 0.25 mm = 20,000 N per millimetre, which equals E × A ÷ L₀.

area0
original Length2
force5,000
change In Length0

Frequently asked questions.

Why is my modulus well below the handbook value for my material?
Three causes account for most low results. The load may have gone past the proportional limit, adding permanent stretch. The extension may have come from the machine's crosshead travel, which includes grip slip and the frame's own give, rather than from an extensometer on the specimen. Or the area may be overstated, for instance a nominal bar size used instead of a measured diameter.
Can I type both lengths in millimetres instead of metres?
Yes, as long as both are in millimetres. Strain is a length divided by a length, so the unit cancels and 0.25 mm over 2,000 mm gives the same 0.000125 as the metre values. The area is different: it must be in square metres and the force in newtons for the stress and modulus to come out in pascals.
Which readings from a load–extension record should I enter?
Take two points on the straight part of the record and enter the differences: the change in force between them and the change in extension. Working from increments ignores the slack taken up at the start of a test and any small preload, and because the elastic relationship is linear the arithmetic is unchanged. A single point from the very start of the curve is usually less reliable.
Does a compression test give the same modulus as a tension test?
For most metals, yes. Enter a negative force and a negative change in length; the signs cancel and E comes out positive. Some materials differ by direction, and OpenStax lists bone at 16 GPa in tension but 9 GPa in compression. Long, slender specimens can also buckle sideways under compression, which makes the measured shortening meaningless.
How does Young's modulus relate to the stiffness of a particular bar?
A bar under axial load behaves like a spring with stiffness k = E × A ÷ L₀. The modulus belongs to the material; the stiffness belongs to the part. Doubling the cross-section doubles the stiffness and doubling the length halves it, while E stays fixed. That is how the same steel can make both a rigid column and a flexible wire.
What figures should I expect for familiar materials?
The OpenStax table this calculation follows gives, in gigapascals, about 210 for iron and nickel, 200 for steel, 110 for copper, 90 for brass, 70 for aluminium, 60 for crown glass and marble, 20 for concrete and 15 for hardwood. A result within a few percent of the right row is typical; real alloys, heat treatments and wood species shift the value.

References& sources.

  1. [1]OpenStax. University Physics Volume 1, Section 12.3 'Stress, Strain, and Elastic Modulus' — defines Young's modulus Y = tensile stress/tensile strain = (F⊥/A)/(ΔL/L₀), valid in the linear (elastic) regime.
  2. [2]National Institute of Standards and Technology (NIST). CODATA-adjacent SI unit definitions — the pascal (Pa = N/m²) as the SI-derived unit of stress and pressure.
  3. [3]Gere, J. M., & Goodno, B. J. (2013). Mechanics of Materials, 8th edition, Chapter 1 (Tension, Compression, and Shear) — the tensile test, Hooke's law, and the elastic-limit assumption underlying E = stress/strain. Cengage Learning.

How this page was produced

Published by
Quanta Calculator
Primary sources
3 cited below
Method
E = σ ⁄ ε = (F ⁄ A) ⁄ (ΔL ⁄ L₀)
Published
Last verified

Built with AI assistance and verified by automated tests against the cited sources — every worked example on this page is computed by the same code that runs the calculator. How we build and check calculators.

In this category

Embed

Quanta Pro

Paid features are coming later.

  • All 1560 calculators remain free
  • No billing is enabled
Coming soon