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Estimates of Notch-Stresses and Strains for Local Yielding using Neuber's Rule 
by Julio C. Banks, P. E. 
Few closed-form solutions exist for determining notch strains during plastic deformation. Numerical 
methods (such as finite elements) can be used, but nonlinear elasto-plastic stress-strain relationships 
complicates and increases the cost of the solution. Although nonlinear numerical analysis is sometimes 
necessary, various approximate methods have been developed for estimating the notch stresses and 
strain. Neuber's rule is the most widely used method and it will be illustrated in this article [1]. 
Example: Aluminum AMS 4117, T6 used in tubing applications (at T= -400 oF) 
Elastic Modulus: E  11.2103ksi Ultimate strain: εu  23% 
Yield Strength: Sy  48ksi Ultimate Strength: Su  60ksi 
Predicted Using Linear Elastic FEA: σFEA  100.6ksi 
Solution 
σ = E(ε  0.2%) and Ν = Spεp 
2 
E 
Skt 
= where Skt  σFEA 
therefore εy 
Sy 
E 
  0.2%  0.6286% and Ν 
2 
E 
Skt 
  0.9036ksi 
Plastic Stress-Strain linearize relationship: Et 
Su  Sy 
εu ε y 
  53.64ksi b  Sy  Etεy  47.66ksi 
2 
εp  εyεy  0.001  εu Spεp  Etεp  b SpNεp Skt 
E ε p 
 
0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 
150 
140 
130 
120 
110 
100 
90 
80 
70 
60 
50 
40 
30 
20 
10 
0 
Neuber Plastic State Point 
Sp ε p 
ksi 
SpN ε p 
ksi 
εp 
% 
Julio C. Banks, P.E. MathCAD - Neuber A6061.xmcd page 1 of 5
Plastic Stress-Strain linearize relationship: Et 
Su  Sy 
εu ε y 
= 
Sp  Sy 
εp ε y 
= 
Initial guess for the plastic stress: Sp  1.2Sy εp  1.2εy 
Given 
Et 
Sp  Sy 
εp ε y 
= (1) 
Ν = Spεp (2) 
εy  εp  εu 
Sp 
εp 
 
 
 FindSpεp 
Sp 
ksi 
εp 
% 
 
 
48.659 
1.857 
 
 
 
Post-Process 
Skt = KtSp therefore Kt 
Skt 
Sp 
  2.067 
Summary 
Young's Modulus: E  1.120  104ksi 
Tangent Modulus: Et  53.64ksi 
Plastic Modulus: Ep 
Et 
1 
  53.90ksi 
Et 
E 
 
Yield Point: εy  0.63% Sy  48.00ksi 
Ultimate Point: εu  23% Su  60.00ksi 
Julio C. Banks, P.E. MathCAD - Neuber A6061.xmcd page 2 of 5
2.0 Closed-form solution 
The appendix provides the derivation and also the detail closed-form solution. For brevity, only the 
essential results are provide in this section 
Example 
Yield strength: Sy  48.00ksi 
Yield strain: εy  0.6286% 
Tangent Moduls: Et  53.64ksi 
Neuber Constant: Ν  0.9036ksi 
B1 
1 
2 
 
Sy 
Et 
 
 
 εy 
 
 
   0.4443 
B0 
 1.685 10 2    
Ν 
Et 
Λ 
B0 
B12 
8.534 10 2    
εp  B11  1  Λ  1.857% QED 
REFERENCE 
1. Rolfe & Barson, "Fracture & Fatigue Controls in Structures", Prentice Hall. 
Pages 598 through 599. 
Julio C. Banks, P.E. MathCAD - Neuber A6061.xmcd page 3 of 5
Appendix 
Obtain a closed-form solution for the Neuber (plastic) point on the linearized 
stress-strain material functions given by equations 1 and 2. 
Et 
Sp  Sy 
εp ε y 
= (1) 
Ν = Spεp (2) 
Solve for Sp from Eq, 2 
Sp 
Ν 
= (3) 
εp 
Substitute Eq. 3 into Eq. 1 
Et 
Ν 
εp 
 
 
 Sy 
= (4) 
εp ε y 
Now solver for the plastic strain from Eq. 4 
Et 
Ν  Syεp 
εp 
2 εy ε  p 
= 
1 
Ν 
Et 
 
 
Sy 
Et 
 
 
ε  p 
εp 
2 εy ε  p 
= 
2 Sy 
(5) εp 
Et 
 
 
 εy 
 
 
 εp 
Ν 
Et 
 = 0 
1 
2 
Let B (6) 1 
 
Sy 
Et 
 
 
 εy 
 
 
  
B0 
Ν 
Et 
  (7) 
Julio C. Banks, P.E. MathCAD - Neuber A6061.xmcd page 4 of 5
Substitute equations 6 and 7 into Eq. 5 
εp 
2 2B1 ε  p  B0 = 0 (8) 
The solution of the quadratic equation 8 is 
εp B1 
1  1  Λ 
1  1  Λ 
 
 
=  (9) 
Example 
Yield strength: Sy  48.00ksi 
Yield strain: εy  0.6286% 
Tangent Modulus: Et  53.64ksi 
Neuber Constant: Ν  0.9036ksi 
Numerical experimentation shows the sign of all pertinent parameter to assist the a-priori selection of 
the positive-real root. In order for the solution to be real (not imaginary), 1  Λ  0, Also, Λ  0 and 
1  Λ  1, therefore, 1  Λ>1. Since B1  0 and the solution sought is εp  0 then the first root, is 
the appropriate answer sought, 
B1 
1 
2 
 
Sy 
Et 
 
 
 εy 
 
 
   0.4443 
B0 
 1.685 10 2    
Ν 
Et 
Λ 
B0 
B12 
8.534 10 2    
εp  B11  1  Λ  1.857% 
Julio C. Banks, P.E. MathCAD - Neuber A6061.xmcd page 5 of 5

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MathCAD Neuber A6061

  • 1. Estimates of Notch-Stresses and Strains for Local Yielding using Neuber's Rule by Julio C. Banks, P. E. Few closed-form solutions exist for determining notch strains during plastic deformation. Numerical methods (such as finite elements) can be used, but nonlinear elasto-plastic stress-strain relationships complicates and increases the cost of the solution. Although nonlinear numerical analysis is sometimes necessary, various approximate methods have been developed for estimating the notch stresses and strain. Neuber's rule is the most widely used method and it will be illustrated in this article [1]. Example: Aluminum AMS 4117, T6 used in tubing applications (at T= -400 oF) Elastic Modulus: E  11.2103ksi Ultimate strain: εu  23% Yield Strength: Sy  48ksi Ultimate Strength: Su  60ksi Predicted Using Linear Elastic FEA: σFEA  100.6ksi Solution σ = E(ε  0.2%) and Ν = Spεp 2 E Skt = where Skt  σFEA therefore εy Sy E   0.2%  0.6286% and Ν 2 E Skt   0.9036ksi Plastic Stress-Strain linearize relationship: Et Su  Sy εu ε y   53.64ksi b  Sy  Etεy  47.66ksi 2 εp  εyεy  0.001  εu Spεp  Etεp  b SpNεp Skt E ε p  0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 150 140 130 120 110 100 90 80 70 60 50 40 30 20 10 0 Neuber Plastic State Point Sp ε p ksi SpN ε p ksi εp % Julio C. Banks, P.E. MathCAD - Neuber A6061.xmcd page 1 of 5
  • 2. Plastic Stress-Strain linearize relationship: Et Su  Sy εu ε y = Sp  Sy εp ε y = Initial guess for the plastic stress: Sp  1.2Sy εp  1.2εy Given Et Sp  Sy εp ε y = (1) Ν = Spεp (2) εy  εp  εu Sp εp    FindSpεp Sp ksi εp %   48.659 1.857    Post-Process Skt = KtSp therefore Kt Skt Sp   2.067 Summary Young's Modulus: E  1.120  104ksi Tangent Modulus: Et  53.64ksi Plastic Modulus: Ep Et 1   53.90ksi Et E  Yield Point: εy  0.63% Sy  48.00ksi Ultimate Point: εu  23% Su  60.00ksi Julio C. Banks, P.E. MathCAD - Neuber A6061.xmcd page 2 of 5
  • 3. 2.0 Closed-form solution The appendix provides the derivation and also the detail closed-form solution. For brevity, only the essential results are provide in this section Example Yield strength: Sy  48.00ksi Yield strain: εy  0.6286% Tangent Moduls: Et  53.64ksi Neuber Constant: Ν  0.9036ksi B1 1 2  Sy Et    εy      0.4443 B0  1.685 10 2    Ν Et Λ B0 B12 8.534 10 2    εp  B11  1  Λ  1.857% QED REFERENCE 1. Rolfe & Barson, "Fracture & Fatigue Controls in Structures", Prentice Hall. Pages 598 through 599. Julio C. Banks, P.E. MathCAD - Neuber A6061.xmcd page 3 of 5
  • 4. Appendix Obtain a closed-form solution for the Neuber (plastic) point on the linearized stress-strain material functions given by equations 1 and 2. Et Sp  Sy εp ε y = (1) Ν = Spεp (2) Solve for Sp from Eq, 2 Sp Ν = (3) εp Substitute Eq. 3 into Eq. 1 Et Ν εp    Sy = (4) εp ε y Now solver for the plastic strain from Eq. 4 Et Ν  Syεp εp 2 εy ε  p = 1 Ν Et   Sy Et   ε  p εp 2 εy ε  p = 2 Sy (5) εp Et    εy    εp Ν Et  = 0 1 2 Let B (6) 1  Sy Et    εy     B0 Ν Et   (7) Julio C. Banks, P.E. MathCAD - Neuber A6061.xmcd page 4 of 5
  • 5. Substitute equations 6 and 7 into Eq. 5 εp 2 2B1 ε  p  B0 = 0 (8) The solution of the quadratic equation 8 is εp B1 1  1  Λ 1  1  Λ   =  (9) Example Yield strength: Sy  48.00ksi Yield strain: εy  0.6286% Tangent Modulus: Et  53.64ksi Neuber Constant: Ν  0.9036ksi Numerical experimentation shows the sign of all pertinent parameter to assist the a-priori selection of the positive-real root. In order for the solution to be real (not imaginary), 1  Λ  0, Also, Λ  0 and 1  Λ  1, therefore, 1  Λ>1. Since B1  0 and the solution sought is εp  0 then the first root, is the appropriate answer sought, B1 1 2  Sy Et    εy      0.4443 B0  1.685 10 2    Ν Et Λ B0 B12 8.534 10 2    εp  B11  1  Λ  1.857% Julio C. Banks, P.E. MathCAD - Neuber A6061.xmcd page 5 of 5