0.182322
0.2
0.182322
-0.017678
9.7
%
1.2
0.182322
0.2
0.182322
-0.017678
9.7
%
1.2
The True Strain Calculator computes the logarithmic (true) strain and compares it with engineering strain to reveal the difference between these two measures of deformation. True strain is defined as:
$$\varepsilon_{\text{true}} = \ln\left(\frac{L}{L_0}\right) = \ln(1 + \varepsilon_{\text{eng}})$$
where $$L$$ is the current (deformed) length and $$L_0$$ is the original gauge length. Unlike engineering strain, which references only the initial length, true strain accounts for the continuously changing gauge length during deformation. This makes it the physically correct measure for large deformations encountered in metal forming, polymer stretching, and geological processes.
For incompressible materials (constant volume), true strain can also be computed from the reduction in cross-sectional area:
$$\varepsilon_{\text{true}} = \ln\left(\frac{A_0}{A}\right)$$
This is especially useful after necking in a tensile test, when the deformation is no longer uniform along the gauge length. True strain is additive for sequential deformations, a property that engineering strain lacks, making it indispensable in plasticity theory and finite-element simulations of forming processes.
Consider an infinitesimal element of length $$l$$ stretched by $$dl$$. The incremental strain is $$d\varepsilon = dl/l$$. Integrating from $$L_0$$ to $$L$$:
$$\varepsilon_{\text{true}} = \int_{L_0}^{L} \frac{dl}{l} = \ln\left(\frac{L}{L_0}\right)$$
This integral definition is why true strain is also called logarithmic strain or Hencky strain. Key relationships:
Why the difference matters: At $$\varepsilon_{\text{eng}} = 0.01$$ (1%), the error from using engineering strain instead of true strain is only 0.5%. But at $$\varepsilon_{\text{eng}} = 0.5$$ (50%), the true strain is $$\ln(1.5) = 0.405$$ — an 18.9% discrepancy. In deep drawing, forging, or rubber elasticity where strains exceed 100%, using engineering strain leads to serious errors.
Additivity: If a bar is stretched from $$L_0$$ to $$L_1$$, then from $$L_1$$ to $$L_2$$, the total true strain is $$\ln(L_1/L_0) + \ln(L_2/L_1) = \ln(L_2/L_0)$$. Engineering strain does not satisfy this: $$\varepsilon_1 + \varepsilon_2 \neq \varepsilon_{\text{total}}$$.
The True Strain is the logarithmic measure of deformation — physically meaningful for large deformations. The Engineering Strain is the simpler linear ratio. The Difference shows how much engineering strain overestimates the deformation (for tension) or underestimates it (for compression). The Relative Error quantifies this discrepancy as a percentage. The Stretch Ratio $$\lambda = L/L_0$$ is commonly used in rubber elasticity and hyperelastic material models. The True Strain from Area uses the volume-conservation approach, which is valid for metals undergoing plastic deformation.
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At 20% engineering strain, true strain is 0.1823 — an 8.8% lower value. Both length-based and area-based true strains agree, confirming volume conservation. A₀/A = 78.54/65.45 = 1.2 = L/L₀.
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At 100% engineering elongation (doubling the length), true strain is only ln(2) = 0.693. The 44% discrepancy shows why engineering strain is inadequate for forming simulations.
True strain is preferred in plasticity and large-deformation analysis for three reasons: (1) it is additive for sequential deformations, (2) it uses the current configuration as reference rather than a fixed initial state, and (3) it produces symmetric tension-compression behavior. A bar stretched to twice its length has $$\varepsilon_{\text{true}} = \ln 2 = 0.693$$, and compressed to half has $$\varepsilon_{\text{true}} = \ln 0.5 = -0.693$$. Engineering strain gives +1.0 and −0.5, which is asymmetric.
Engineering strain is sufficient when deformations are small ($$\varepsilon < 0.01$$ or 1%). In this regime, $$\ln(1+\varepsilon) \approx \varepsilon$$, so the two measures differ by less than 0.5%. Most structural engineering applications (buildings, bridges, machines) operate well below 1% strain, making engineering strain perfectly adequate.
For volume-conserving (incompressible) deformation: $$\sigma_{\text{true}} = \sigma_{\text{eng}}(1 + \varepsilon_{\text{eng}})$$. This is because the true stress uses the current cross-sectional area $$A = A_0/(1+\varepsilon_{\text{eng}})$$. Similarly, $$\sigma_{\text{true}} = \sigma_{\text{eng}} \cdot e^{\varepsilon_{\text{true}}}$$.
The stretch ratio $$\lambda = L/L_0$$ is widely used in rubber elasticity and hyperelastic constitutive models (Neo-Hookean, Mooney-Rivlin, Ogden). These models express strain energy as a function of principal stretch ratios $$\lambda_1, \lambda_2, \lambda_3$$. For an incompressible material, $$\lambda_1 \lambda_2 \lambda_3 = 1$$.
After necking begins in a tensile test, deformation localizes and the gauge length method becomes unreliable. Instead, true strain is measured from the minimum cross-sectional area at the neck: $$\varepsilon_{\text{true}} = \ln(A_0/A_{\text{min}})$$. This requires measuring the instantaneous neck diameter, often done with extensometers, digital image correlation (DIC), or post-test measurement of the fracture surface.
The Hencky strain tensor is the three-dimensional generalization of logarithmic strain: $$\mathbf{H} = \frac{1}{2}\ln(\mathbf{F}^T \mathbf{F})$$, where $$\mathbf{F}$$ is the deformation gradient tensor. In principal directions, it reduces to $$H_i = \ln \lambda_i$$. It is a Lagrangian strain measure that is work-conjugate to the rotated Kirchhoff stress and is used in advanced computational mechanics codes.
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