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Linear to True Stress-Strain

The following analysis produces an estimated local stress and strain from an elastic point stress using the Neuber and Glinka methods and a weighted Unified Estimate between them. This is useful in predicting a peak stress and strain in a high gradient area from a linear finite element (FE) analysis. This method allows an estimate of an true stress and strain at a stress concentration without having to run a material nonlinear FE analysis.

  • Used for calculating effect stress concentration factors in notches - inelastic strains

  • Uses Neuber (upper bound), Glinka (lower bound), and a weighted Unified Estimate between them

  • Iterative method solves for true stress using Newton's method

  • True stress is calculated using a modified Ramberg-Osgood equation

Point Stress and Material Properties Inputs


Unit System: /

Material Properties and Point Stress






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Neuber Method

Neuber's Rule for Estimating Elastic-Plastic Stress and Strain at Notches

1. Introduction and Physical Basis

Neuber's rule, developed by Heinz Neuber in 1961, provides a method for estimating the true elastic-plastic stress and strain at a stress concentration (notch) from linear elastic finite element analysis (FEA) results. The rule is based on the principle of strain energy density conservation.

When a component with a notch or stress concentration is loaded beyond the elastic limit, the material at the notch root yields and undergoes plastic deformation. A linear elastic FEA cannot capture this plasticity, resulting in artificially high "pseudo-elastic" stresses. Neuber's rule corrects these elastic predictions to account for yielding.

Key Principle: Neuber's rule assumes that the total strain energy density at the notch root calculated from an elastic analysis equals the actual elastic-plastic strain energy density.

2. Stress Concentration Factors

Before deriving Neuber's rule, we must define three concentration factors:

Theoretical (Elastic) Stress Concentration Factor:
Kt = σelastic / σnom

Actual Stress Concentration Factor (with plasticity):
Kσ = σtrue / σnom

Actual Strain Concentration Factor (with plasticity):
Kε = εtrue / εnom

Where:

  • σnom = nominal (far-field) stress
  • σelastic = elastic stress at notch from linear FEA = Kt · σnom
  • σtrue = actual elastic-plastic stress at notch
  • εnom = σnom / E = nominal strain
  • εelastic = σelastic / E = elastic strain at notch from linear FEA
  • εtrue = actual elastic-plastic strain at notch (includes plastic component)

3. Derivation of Neuber's Rule

3.1 Elastic Strain Energy Density

For a uniaxial stress state, the elastic strain energy density is:

Welastic = (1/2) · σ · ε = σ2 / (2E)

At the notch root, using the elastic FEA stress:

Welastic,notch = σelastic2 / (2E) = (Kt · σnom)2 / (2E)

In the far field (nominal region):

Welastic,nom = σnom2 / (2E)

3.2 Neuber's Hypothesis

Neuber proposed that the product of stress and strain at the notch is preserved when transitioning from elastic to elastic-plastic behavior:

σelastic · εelastic = σtrue · εtrue

This can also be written in terms of concentration factors:

Kt2 = Kσ · Kε

3.3 Neuber's Rule in Practical Form

Substituting the definitions of the elastic stress and strain:

(Kt · σnom) · (Kt · σnom / E) = σtrue · εtrue

Simplifying:

Kt2 · σnom2 / E = σtrue · εtrue

Recognizing that σelastic = Kt · σnom:

Neuber's Rule: σtrue · εtrue = σelastic2 / E

This is the fundamental form of Neuber's rule used in practice.

4. Solution Procedure with Ramberg-Osgood Material Model

To find the actual stress and strain at the notch, we must solve Neuber's rule simultaneously with the material's stress-strain relationship. The Ramberg-Osgood equation is commonly used:

Ramberg-Osgood Equation: ε = σ/E + (σ/K')1/n'

Where:

  • E = elastic modulus
  • K' = strength coefficient (Ramberg-Osgood parameter)
  • n' = strain hardening exponent (Ramberg-Osgood parameter)

4.1 System of Equations

We have two equations with two unknowns (σtrue and εtrue):

Equation 1 (Neuber): σtrue · εtrue = σelastic2 / E

Equation 2 (Ramberg-Osgood): εtrue = σtrue/E + (σtrue/K')1/n'

4.2 Combining into Single Nonlinear Equation

Substitute the Ramberg-Osgood equation into Neuber's rule:

σtrue · [σtrue/E + (σtrue/K')1/n'] = σelastic2 / E

Let RHS = σelastic2 / E, then rearranging to find the root:

Function to solve (f(σ) = 0): f(σ) = σ · [σ/E + (σ/K')1/n'] - RHS = 0

4.3 Iterative Solution (Newton's Method)

This nonlinear equation is solved iteratively using Newton's method:

σi+1 = σi - f(σi) / f'(σi)

The derivative is:

f'(σ) = 2σ/E + (1 + 1/n') · (σ/K')1/n'

Once σtrue converges, the true strain is calculated directly from Ramberg-Osgood:

εtrue = σtrue/E + (σtrue/K')1/n'

5. Graphical Interpretation

On a stress-strain diagram:

  1. Neuber's rule defines a hyperbola with constant product σ · ε = RHS
  2. The Ramberg-Osgood curve describes the material's actual stress-strain behavior
  3. The intersection of these two curves gives the elastic-plastic solution

Note: The elastic point (σelastic, εelastic) lies on the elastic line ε = σ/E and has the same σ · ε product as the true elastic-plastic point.

6. Limitations and Accuracy

Important Limitations:

  • Tends to OVERESTIMATE strains: Neuber's rule typically predicts higher strains than experimentally measured values
  • Small-scale yielding: Most accurate when the plastic zone is small compared to the notch radius
  • Uniaxial loading: Originally developed for uniaxial stress states; extensions exist for multiaxial loading
  • Monotonic loading: Most accurate for monotonic (non-cyclic) loading; cyclic plasticity requires modifications

7. Comparison with Glinka's Method

Glinka's equivalent strain energy density (ESED) method is an alternative that typically provides more accurate results:

  • Neuber: Conserves the product σ · ε (total strain energy density)
  • Glinka: Conserves the integral of stress over strain (includes plastic work properly)
  • Result: Glinka tends to give slightly lower (more accurate) strain predictions than Neuber

8. Applications

Neuber's rule is widely used in:

  • Fatigue life prediction at notches and stress concentrations
  • Low-cycle fatigue (LCF) analysis
  • Post-processing of linear elastic FEA results
  • Notch analysis when full nonlinear FEA is not practical
  • Strain-life (ε-N) fatigue calculations

9. References

Key references for Neuber's rule:

  • Neuber, H. (1961). "Theory of Stress Concentration for Shear-Strained Prismatical Bodies With Arbitrary Nonlinear Stress-Strain Law." Journal of Applied Mechanics, 28(4), 544-550.
  • Dowling, N.E. (2013). Mechanical Behavior of Materials: Engineering Methods for Deformation, Fracture, and Fatigue, 4th Edition, Pearson.
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Glinka Method

Glinka's Equivalent Strain Energy Density (ESED) Method

1. Introduction and Physical Basis

The equivalent strain energy density (ESED) method, developed by Molski and Glinka in 1981, provides an improved approach for estimating elastic-plastic stress and strain at stress concentrations compared to Neuber's rule. Like Neuber, it corrects linear elastic FEA results to account for plasticity, but it does so more accurately by properly accounting for plastic work.

The key innovation of Glinka's method is that it equates the total strain energy density (elastic plus plastic) rather than just the product of stress and strain.

Key Principle: Glinka's ESED method assumes that the total strain energy density (elastic energy plus plastic work) at the notch root from an elastic analysis equals the actual total strain energy density in the elastic-plastic case.

2. Strain Energy Density Components

For an elastic-plastic material, the total strain energy density has two components:

Elastic Strain Energy Density:
Welastic = σ2 / (2E)

Plastic Work (strain energy absorbed in plastic deformation):
Wplastic = ∫0εp σ dεp

The total strain energy density is:

Total Strain Energy Density:
Wtotal = Welastic + Wplastic = σ2/(2E) + ∫0εp σ dεp

3. Derivation of Glinka's Method

3.1 Elastic Case (from linear FEA)

For the elastic case at the notch root:

Welastic,notch = σelastic2 / (2E)

Where σelastic is the pseudo-elastic stress from linear FEA.

3.2 Elastic-Plastic Case (actual behavior)

For the actual elastic-plastic state:

Wtotal,true = σtrue2/(2E) + ∫0εp,true σ dεp

3.3 Glinka's Energy Balance

Glinka's hypothesis states that these energies are equal:

Energy Balance:
σelastic2 / (2E) = σtrue2/(2E) + ∫0εp,true σ dεp

Rearranging:

(σelastic2 - σtrue2) / (2E) = ∫0εp,true σ dεp

4. Integration for Ramberg-Osgood Material

For a Ramberg-Osgood material, the plastic strain is:

εp = (σ/K')1/n'

Therefore:

dεp = (1/n') · (1/K')1/n' · σ(1/n')-1 dσ

4.1 Evaluation of Plastic Work Integral

The plastic work integral becomes:

∫0εp σ dεp = ∫0σ σ · (1/n') · (1/K')1/n' · σ(1/n')-1 dσ

Simplifying:

= (1/n') · (1/K')1/n' ∫0σ σ1/n' dσ

Integrating:

= (1/n') · (1/K')1/n' · [σ1 + 1/n' / (1 + 1/n')]

Simplifying the expression:

= σ1 + 1/n' / [n'(1 + 1/n') · K'1/n']

Factor out σ from the numerator:

= σ · σ1/n' / [n'(1 + 1/n') · K'1/n']

Recognize that σ1/n' / K'1/n' = (σ/K')1/n' = εp:

= σ · (σ/K')1/n' / [n'(1 + 1/n')]

Simplifying the denominator: n'(1 + 1/n') = n' + 1

Plastic Work:
Wplastic = σ · (σ/K')1/n' / (1 + n')

5. Glinka's Rule in Practical Form

Substituting the plastic work expression into the energy balance:

σelastic2 / (2E) = σtrue2/(2E) + σtrue · (σtrue/K')1/n' / (1 + n')

Let RHSG = σelastic2 / (2E), then:

Glinka's Rule:
σtrue2/(2E) + [σtrue/(1+n')] · (σtrue/K')1/n' = σelastic2 / (2E)

This is the fundamental form of Glinka's ESED method.

6. Solution Procedure

6.1 System of Equations

We solve two equations simultaneously:

Equation 1 (Glinka): σ2/(2E) + [σ/(1+n')] · (σ/K')1/n' = RHSG

Equation 2 (Ramberg-Osgood): ε = σ/E + (σ/K')1/n'

6.2 Nonlinear Equation to Solve

Rearranging Glinka's equation to find the root:

Function to solve (f(σ) = 0):
f(σ) = σ2/(2E) + [σ/(1+n')] · (σ/K')1/n' - RHSG = 0

6.3 Iterative Solution (Newton's Method)

Using Newton's method:

σi+1 = σi - f(σi) / f'(σi)

The derivative is:

f'(σ) = σ/E + [1/(1+n')] · (1 + 1/n') · (σ/K')1/n'

Once σtrue converges, calculate εtrue from Ramberg-Osgood:

εtrue = σtrue/E + (σtrue/K')1/n'

7. Comparison with Neuber's Rule

Aspect Neuber's Rule Glinka's ESED Method
Energy conserved σ · ε product
(strain energy density)
Total energy including plastic work
σ2/(2E) + ∫σ dεp
Equation form σ · ε = σelastic2/E σ2/(2E) + σ · εp/(1+n') = σelastic2/(2E)
Accuracy Tends to OVERESTIMATE strains More accurate, slight UNDERESTIMATION
Complexity Simpler formulation Requires plastic work integration
Best for Conservative estimates, quick calculations High stress concentrations, accurate predictions

8. Physical Interpretation

Key Difference from Neuber:

  • Neuber: Assumes all energy goes into elastic deformation (σ · ε), neglecting that plastic work dissipates energy differently
  • Glinka: Properly accounts for the fact that plastic deformation involves irreversible work, which is correctly integrated as ∫σ dεp
  • Result: Glinka provides more physically realistic predictions, especially for materials with significant plastic deformation

9. Limitations and Applicability

Glinka's method shares some limitations with Neuber's rule:

  • Small-scale yielding: Most accurate when plastic zone is small relative to notch size
  • Monotonic loading: Originally formulated for monotonic loading paths
  • Uniaxial stress: Extensions needed for multiaxial stress states
  • Material model dependent: Requires accurate Ramberg-Osgood parameters

Advantage over Neuber: Glinka's method typically provides more accurate predictions than Neuber, particularly under plane strain conditions and for sharp notches (high Kt values).

10. Applications

Glinka's ESED method is used in:

  • Accurate fatigue life predictions at notches
  • Low-cycle fatigue (LCF) analysis requiring precision
  • Sharp notches and crack-like defects (high stress concentrations)
  • Situations where Neuber's overestimation is problematic
  • Strain-based fracture mechanics
  • Validation of nonlinear FEA results

11. References

Key references for Glinka's ESED method:

  • Molski, K., and Glinka, G. (1981). "A Method of Elastic-Plastic Stress and Strain Calculation at a Notch Root." Materials Science and Engineering, 50(1), 93-100.
  • Glinka, G. (1985). "Energy Density Approach to Calculation of Inelastic Strain-Stress Near Notches and Cracks." Engineering Fracture Mechanics, 22(3), 485-508.
  • Dowling, N.E. (2013). Mechanical Behavior of Materials: Engineering Methods for Deformation, Fracture, and Fatigue, 4th Edition, Pearson.
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Unified Estimate Method

Unified Estimate Method (Weighted Neuber-Glinka)

1. What the Calculator Computes

The Unified Estimate is a weighted average of the Neuber and Glinka solutions already calculated on this page. With the weighting parameter α entered in the form:

σU = (1 − α) · σN + α · σG
εU = (1 − α) · εN + α · εG

α = 0 returns the Neuber result, α = 1 returns the Glinka result, and α = 0.5 is the midpoint. The estimate is an interpolation between two bounds. It is not a derived notch rule and does not solve an additional energy balance; in particular it is not the unified expression of Ye, Hertel & Vormwald (2008), which is a separate method not implemented here.

2. Why the Two Methods Bracket the Answer

Neuber's rule conserves the product σ · ε and tends to over-predict notch strain, most noticeably under plane strain (thick sections, interior points, sharp notches). Glinka's equivalent strain energy density method accounts for plastic work and tends to under-predict notch strain, most noticeably under plane stress (thin sections, free surfaces). Experimental and finite element comparisons (for example Sharpe, Yang & Turner, 1992) place the true elastic-plastic response between the two. The weighting parameter lets the user move the estimate toward whichever bound better matches the constraint at the point of interest.

3. Selecting α

  • α = 0: Neuber only - very thin sections, extreme plane stress, or when a conservative (high strain) estimate is wanted
  • α = 0.2-0.4: Plane stress - thin sheets, skin panels, surface points
  • α = 0.5: Balanced estimate when the constraint is uncertain
  • α = 0.6-0.8: Plane strain - thick sections, interior points, forgings, sharp notches
  • α = 1: Glinka only - extreme plane strain, very thick sections

Indicators of plane stress (use a lower α): section thickness less than about 3-5 times the plastic zone size, surface or edge locations, sheet metal structures, low stress triaxiality.

Indicators of plane strain (use a higher α): section thickness more than about 10 times the plastic zone size, interior points far from free surfaces, thick forgings or castings, high stress triaxiality.

4. Cautions

  • The estimate has not been validated against elastic-plastic finite element results in this tool. Treat it as an engineering interpolation, not a calibrated method.
  • For a conservative design value use the Neuber result directly.
  • When the point of interest is critical, an elastic-plastic finite element submodel of the notch region with the same Ramberg-Osgood curve is the reference solution that all of these estimates approximate.
  • All three results on this page are uniaxial. For biaxial notch-root states use the plane-strain modulus or a multiaxial extension (Hoffmann & Seeger, 1985).

5. References

  • Neuber, H. (1961). "Theory of Stress Concentration for Shear-Strained Prismatical Bodies With Arbitrary Nonlinear Stress-Strain Law." Journal of Applied Mechanics, 28(4), 544-550.
  • Molski, K., and Glinka, G. (1981). "A Method of Elastic-Plastic Stress and Strain Calculation at a Notch Root." Materials Science and Engineering, 50(1), 93-100.
  • Sharpe, W. N., Yang, C. H., and Turner, R. L. (1992). "An Evaluation of the Neuber and Glinka Relations for Monotonic Loading." Journal of Applied Mechanics, 59(2S), S50-S56.
  • Hoffmann, M., and Seeger, T. (1985). "A Generalized Method for Estimating Multiaxial Elastic-Plastic Notch Stresses and Strains, Part 1: Theory." Journal of Engineering Materials and Technology, 107(4), 250-254.
  • Ye, D., Hertel, O., and Vormwald, M. (2008). "A Unified Expression of Elastic-Plastic Notch Stress-Strain Calculation in Bodies Subjected to Multiaxial Cyclic Loading." International Journal of Solids and Structures, 45(24), 6177-6189. [Source of the idea that Neuber and Glinka are limiting cases of a constraint-dependent family; its expression is not implemented here.]
  • Dowling, N. E. (2013). Mechanical Behavior of Materials, 4th ed., Pearson. [General discussion of notch approximation methods]



References

Neuber, H. (1961). "Theory of Stress Concentration for Shear-Strained Prismatical Bodies with Arbitrary Nonlinear Stress-Strain Law." Journal of Applied Mechanics, Vol. 28, No. 4, pp. 544–550.

Molski, K., and Glinka, G. (1981). "A Method of Elastic-Plastic Stress and Strain Calculation at a Notch Root." Materials Science and Engineering, Vol. 50, No. 1, pp. 93–100.

Glinka, G. (1985). "Energy Density Approach to Calculation of Inelastic Strain-Stress Near Notches and Cracks." Engineering Fracture Mechanics, Vol. 22, No. 3, pp. 485–508.

Ye, D., Hertel, O., and Vormwald, M. (2008). "A Unified Expression of Elastic-Plastic Notch Stress-Strain Calculation in Bodies Subjected to Multiaxial Cyclic Loading." International Journal of Solids and Structures, Vol. 45, No. 24, pp. 6177–6189.

Hoffmann, M., and Seeger, T. (1985). "A Generalized Method for Estimating Multiaxial Elastic-Plastic Notch Stresses and Strains, Part 1: Theory." Journal of Engineering Materials and Technology, Vol. 107, No. 4, pp. 250–254.

Moftakhar, A., Buczynski, A., and Glinka, G. (1995). "Calculation of Elasto-Plastic Strains and Stresses in Notches under Multiaxial Loading." International Journal of Fracture, Vol. 70, No. 4, pp. 357–373.

Conle, A., and Chu, C. C. (1997). "Fatigue Analysis and the Local Stress-Strain Approach in Complex Vehicular Structures." International Journal of Fatigue, Vol. 19, Supplement 1, pp. S317–S323.

Amstutz, B. E., Kardomateas, G. A., and Taggart, D. G. (1997). "Further Investigation of Neuber's Rule and the Equivalent Strain Energy Density (ESED) Method." International Journal of Fatigue, Vol. 19, No. 8–9, pp. 721–727.

Ramberg, W., and Osgood, W. R. (1943). Description of Stress-Strain Curves by Three Parameters. NACA Technical Note 902, National Bureau of Standards, Washington, D.C.

Dowling, N. E. (2013). Mechanical Behavior of Materials: Engineering Methods for Deformation, Fracture, and Fatigue, 4th ed. Pearson Education, Upper Saddle River, NJ.

Stephens, R. I., Fatemi, A., Stephens, R. R., and Fuchs, H. O. (2001). Metal Fatigue in Engineering, 2nd ed. John Wiley & Sons, New York.

Bannantine, J. A., Comer, J. J., and Handrock, J. L. (1990). Fundamentals of Metal Fatigue Analysis. Prentice Hall, Englewood Cliffs, NJ.

Battelle Memorial Institute (current edition). Metallic Materials Properties Development and Standardization (MMPDS). Columbus, OH.


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