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Mechanical

Normal strain from three-dimensional stress and temperature change

Strain in the x direction in an isotropic elastic solid under normal stresses in all three directions, plus the free thermal expansion.

Ref
MEC-81
Rev
v1
Field
Mechanical
Result
εx [µε]

For an isotropic linear elastic material, the normal strain in the x direction is εx = [σx − ν(σy + σz)]/E + αΔT. The first part is the generalised Hooke’s law: stress in x stretches the material and stress in y and z shrinks it through the Poisson effect. The second part is thermal expansion. The result is in microstrain (µε): 1 µε is 10⁻⁶. Enter tensile stresses as positive and compressive as negative; shear stress does not affect normal strain.

Strain in the x direction in an isotropic elastic solid under normal stresses in all three directions, plus the free thermal expansion. The other two normal strains follow by cycling x, y and z.

Calculator

Solve for
µε
MPa
−300500
MPa
−300500
MPa
−300500
GPa
1500
00.5
10⁻⁶/K
030
K
−100200
  • Mechanical strain (stress part)425 µε
  • Thermal strain, αΔT240 µε
  • Stress that would cancel the thermal strain if the member were fully restrained, EαΔT48 MPa

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

Normal strain in x (µε) current value 665 µε
EYoung’s modulusKey driver
41085,200
σxNormal stress in x (tension positive)
−1,3402,670
ΔTTemperature change
−7752,830
σyNormal stress in y (tension positive)
−101,190
σzNormal stress in z (tension positive)
−851,120
αThermal expansion coefficient
4251,030
νPoisson’s ratio
615740
  • With σx = 100 MPa, σy = 50 MPa and a 20 K temperature rise, the strain in x is 665 µε: 425 µε from the stresses and 240 µε from heating.
  • The y stress of 50 MPa reduces the x strain by 75 µε through the Poisson effect: ignoring it would overstate the strain by 17.6 %.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (µε)Local stepChange in result
E Young’s modulus1 to 500 GPa41085,24084,830+10%−5.81 %
σx Normal stress in x (tension positive)−300 to 500 MPa−1,3352,6654,000+16 MPa+12 %
ΔT Temperature change−100 to 200 K−7752,8253,600+6 K+10.8 %
σy Normal stress in y (tension positive)−300 to 500 MPa−101,1901,200+16 MPa−3.61 %
σz Normal stress in z (tension positive)−300 to 500 MPa−851,1151,200+16 MPa−3.61 %
α Thermal expansion coefficient0 to 30 10⁻⁶/K4251,025600+10%+3.61 %
ν Poisson’s ratio0 to 0.5 615740125+10%−1.13 %

Sweep of Normal stress in y (tension positive)

Normal stress in y (tension positive) (MPa)Normal strain in x (µε)
−3001,190
−2001,040
−100890
0740
100590
200440
300290
400140
500−10

Sweep one variable

Normal strain in x (µε)Hover, touch, or use the arrow keys on the chart
020040060080010001200 −300−100100300500 Normal stress in y (tension positive) (MPa) now 665

Variables and how each one contributes

εx

Normal strain in x

Result · µε

What the equation gives you. Everything else feeds it.

σx

Normal stress in x (tension positive)

MPa · typical −300 to 500

The normal stress in the x direction, in MPa (tension positive). Raises the strain in direct proportion: each extra MPa adds 1000/E microstrain, with E in GPa. Raising it by 10 MPa (to 110 MPa) moves the result by +7.52 %, from 665 to 715 µε.

σy

Normal stress in y (tension positive)

MPa · typical −300 to 500

The normal stress in the y direction, in MPa. Lowers the x strain through the Poisson effect: a tensile y stress narrows the material in x. Raising it by 10 MPa (to 60 MPa) moves the result by −2.26 %, from 665 to 650 µε.

σz

Normal stress in z (tension positive)

MPa · typical −300 to 500

The normal stress in the z direction, in MPa. It is zero in plane stress. Lowers the x strain through the Poisson effect, in the same way as σy. Raising it by 10 MPa (to 10 MPa) moves the result by −2.26 %, from 665 to 650 µε.

E

Young’s modulus

GPa · typical 1 to 500

Young’s modulus of the material, in GPa (about 200 for steel, 70 for aluminium). Lowers the mechanical part of the strain, because a stiffer material strains less for the same stress; the thermal part is not affected. Raising it by 10 GPa (to 210 GPa) moves the result by −3.04 %, from 665 to 644.8 µε.

ν

Poisson’s ratio

· typical 0 to 0.5

Poisson’s ratio of the material (about 0.3 for steel). Lowers the strain in x while the sum of σy and σz is positive, because a larger Poisson effect shrinks the material more. Raising it by 0.05 (to 0.35) moves the result by −1.88 %, from 665 to 652.5 µε.

α

Thermal expansion coefficient

10⁻⁶/K · typical 0 to 30

The coefficient of thermal expansion, in 10⁻⁶ per kelvin (about 12 for steel, 23 for aluminium). Raises the thermal part of the strain in direct proportion when ΔT is positive. Raising it by 1 (to 13) moves the result by +3.01 %, from 665 to 685 µε.

ΔT

Temperature change

K · typical −100 to 200

The temperature change from the stress-free state, in kelvin. Positive means heating. Raises the strain in direct proportion to the temperature rise, through thermal expansion. Raising it by 5 K (to 25 K) moves the result by +9.02 %, from 665 to 725 µε.

Worked example with the values above

  1. Mechanical part: [σx − ν(σy + σz)]/E = [100 − 0.3 × 50] / 200,000 MPa = 425 µε.
  2. Thermal part: αΔT = 12 × 20 = 240 µε.
  3. εx = 425 + 240 = 665 µε.

Assumptions and limits

  • A linear elastic, homogeneous and isotropic material, with strains small.
  • Stresses in MPa with moduli in GPa, giving strain in microstrain.
  • Thermal expansion free of any constraint except the stress components entered.

Common mistakes

  • Leaving out the Poisson contribution of the other two stresses.
  • Using the plane-stress shortcut when the through-thickness stress is not zero.
  • Mixing MPa and GPa without converting.

Statistics and uncertainty

Strain-gauge and temperature errors add directly: a 2 K error in ΔT with α = 12 × 10⁻⁶/K causes 24 µε of error, which may be as large as the stress effect being measured, so temperature compensation matters.

Where it is used

  • Interpreting strain-gauge readings in a pressurised or heated structure.
  • Checking the strain in a barrel, hull or pipe under combined pressure and temperature.

Maths you need

  • Stress and strain: force per area and relative change in length
  • Elastic modulus: stress divided by strain in the elastic range

Related formulas

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