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J-integral

From Wikipedia, the free encyclopedia
Calculation of strain energy release rate
Part of a series on
Continuum mechanics
J=Ddφdx{\displaystyle J=-D{\frac {d\varphi }{dx}}}

TheJ-integral represents a way to calculate thestrain energy release rate, or work (energy) per unit fracture surface area, in a material.[1] The theoretical concept of J-integral was developed in 1967 by G. P. Cherepanov[2] and independently in 1968 byJames R. Rice,[3] who showed that an energeticcontour path integral (calledJ) was independent of the path around acrack.

Experimental methods were developed using the integral that allowed the measurement of critical fracture properties in sample sizes that are too small for Linear ElasticFracture Mechanics (LEFM) to be valid.[4] These experiments allow the determination offracture toughness from the critical value of fracture energyJIc, which defines the point at which large-scaleplastic yielding during propagation takes place under mode I loading.[1][5]

The J-integral is equal to thestrain energy release rate for a crack in a body subjected tomonotonic loading.[6] This is generally true, under quasistatic conditions, only forlinear elastic materials. For materials that experience small-scaleyielding at the crack tip,J can be used to compute the energy release rate under special circumstances such as monotonic loading inmode III (antiplane shear). The strain energy release rate can also be computed fromJ for pure power-law hardeningplastic materials that undergo small-scale yielding at the crack tip.

The quantityJ is not path-independent for monotonicmode I andmode II loading of elastic-plastic materials, so only a contour very close to the crack tip gives the energy release rate. Also, Rice showed thatJ is path-independent in plastic materials when there is no non-proportional loading. Unloading is a special case of this, but non-proportional plastic loading also invalidates the path-independence. Such non-proportional loading is the reason for the path-dependence for the in-plane loading modes on elastic-plastic materials.

Two-dimensional J-integral

[edit]
Figure 1. Line J-integral around a notch in two dimensions.

The two-dimensional J-integral was originally defined as[3] (see Figure 1 for an illustration)

J:=Γ(W dx2tux1 ds)=Γ(W dx2tiuix1 ds){\displaystyle J:=\int _{\Gamma }\left(W~\mathrm {d} x_{2}-\mathbf {t} \cdot {\cfrac {\partial \mathbf {u} }{\partial x_{1}}}~\mathrm {d} s\right)=\int _{\Gamma }\left(W~\mathrm {d} x_{2}-t_{i}\,{\cfrac {\partial u_{i}}{\partial x_{1}}}~\mathrm {d} s\right)}

whereW(x1,x2) is the strain energy density,x1,x2 are the coordinate directions,t = [σ]n is thesurface traction vector,n is the normal to the curve Γ, [σ] is theCauchy stress tensor, andu is thedisplacement vector. The strain energy density is given by

W=0[ε][σ]:d[ε] ;  [ε]=12[u+(u)T] .{\displaystyle W=\int _{0}^{[\varepsilon ]}[{\boldsymbol {\sigma }}]:d[{\boldsymbol {\varepsilon }}]~;~~[{\boldsymbol {\varepsilon }}]={\tfrac {1}{2}}\left[{\boldsymbol {\nabla }}\mathbf {u} +({\boldsymbol {\nabla }}\mathbf {u} )^{T}\right]~.}

The J-integral around a crack tip is frequently expressed in a more general form[7] (and inindex notation) as

Ji:=limε0Γε(W(Γ)ninjσjk uk(Γ,xi)xi)dΓ{\displaystyle J_{i}:=\lim _{\varepsilon \rightarrow 0}\int _{\Gamma _{\varepsilon }}\left(W(\Gamma )n_{i}-n_{j}\sigma _{jk}~{\cfrac {\partial u_{k}(\Gamma ,x_{i})}{\partial x_{i}}}\right)\,d\Gamma }

whereJi{\displaystyle J_{i}} is the component of the J-integral for crack opening in thexi{\displaystyle x_{i}} direction andε{\displaystyle \varepsilon } is a small region around the crack tip.UsingGreen's theorem we can show that this integral is zero when the boundaryΓ{\displaystyle \Gamma } is closed and encloses a region that contains nosingularities and issimply connected. If the faces of the crack do not have anysurface tractions on them then the J-integral is alsopath independent.

Rice also showed that the value of the J-integral represents the energy release rate for planar crack growth.The J-integral was developed because of the difficulties involved in computing thestress close to a crack in a nonlinearelastic or elastic-plastic material. Rice showed that if monotonic loading was assumed (without any plastic unloading) then the J-integral could be used to compute the energy release rate of plastic materials too.

Proof that the J-integral is zero over a closed path
To show the path independence of the J-integral, we first have to show that the value ofJ{\displaystyle J} is zero over a closed contour in a simply connected domain. Let us just consider the expression forJ1{\displaystyle J_{1}} which is
J1:=Γ(Wn1njσjk ukx1)dΓ{\displaystyle J_{1}:=\int _{\Gamma }\left(Wn_{1}-n_{j}\sigma _{jk}~{\cfrac {\partial u_{k}}{\partial x_{1}}}\right)\,d\Gamma }

We can write this as

J1=Γ(Wδ1jσjk ukx1)njdΓ{\displaystyle J_{1}=\int _{\Gamma }\left(W\delta _{1j}-\sigma _{jk}~{\cfrac {\partial u_{k}}{\partial x_{1}}}\right)n_{j}\,d\Gamma }

FromGreen's theorem (or the two-dimensionaldivergence theorem) we have

Γfj nj dΓ=Afjxj dA{\displaystyle \int _{\Gamma }f_{j}~n_{j}~d\Gamma =\int _{A}{\cfrac {\partial f_{j}}{\partial x_{j}}}~dA}

Using this result we can expressJ1{\displaystyle J_{1}} as

J1=Axj(Wδ1jσjk ukx1)dA=A[Wx1σjkxj ukx1σjk 2ukx1xj] dA{\displaystyle {\begin{aligned}J_{1}&=\int _{A}{\cfrac {\partial }{\partial x_{j}}}\left(W\delta _{1j}-\sigma _{jk}~{\cfrac {\partial u_{k}}{\partial x_{1}}}\right)dA\\&=\int _{A}\left[{\cfrac {\partial W}{\partial x_{1}}}-{\cfrac {\partial \sigma _{jk}}{\partial x_{j}}}~{\cfrac {\partial u_{k}}{\partial x_{1}}}-\sigma _{jk}~{\cfrac {\partial ^{2}u_{k}}{\partial x_{1}\partial x_{j}}}\right]~dA\end{aligned}}}

whereA{\displaystyle A} is the area enclosed by the contourΓ{\displaystyle \Gamma }. Now, if there areno body forces present, equilibrium (conservation of linear momentum) requires that

σ=0σjkxj=0 .{\displaystyle {\boldsymbol {\nabla }}\cdot {\boldsymbol {\sigma }}=\mathbf {0} \qquad \implies \qquad {\cfrac {\partial \sigma _{jk}}{\partial x_{j}}}=0~.}

Also,

[ε]=12[u+(u)T]εjk=12(ukxj+ujxk) .{\displaystyle [{\boldsymbol {\varepsilon }}]={\tfrac {1}{2}}\left[{\boldsymbol {\nabla }}\mathbf {u} +({\boldsymbol {\nabla }}\mathbf {u} )^{T}\right]\qquad \implies \qquad \varepsilon _{jk}={\tfrac {1}{2}}\left({\cfrac {\partial u_{k}}{\partial x_{j}}}+{\cfrac {\partial u_{j}}{\partial x_{k}}}\right)~.}

Therefore,

σjkεjkx1=12(σjk2ukx1xj+σjk2ujx1xk){\displaystyle \sigma _{jk}{\cfrac {\partial \varepsilon _{jk}}{\partial x_{1}}}={\tfrac {1}{2}}\left(\sigma _{jk}{\cfrac {\partial ^{2}u_{k}}{\partial x_{1}\partial x_{j}}}+\sigma _{jk}{\cfrac {\partial ^{2}u_{j}}{\partial x_{1}\partial x_{k}}}\right)}

From the balance of angular momentum we haveσjk=σkj{\displaystyle \sigma _{jk}=\sigma _{kj}}. Hence,

σjkεjkx1=σjk2ujx1xk{\displaystyle \sigma _{jk}{\cfrac {\partial \varepsilon _{jk}}{\partial x_{1}}}=\sigma _{jk}{\cfrac {\partial ^{2}u_{j}}{\partial x_{1}\partial x_{k}}}}

The J-integral may then be written as

J1=A[Wx1σjk εjkx1] dA{\displaystyle J_{1}=\int _{A}\left[{\cfrac {\partial W}{\partial x_{1}}}-\sigma _{jk}~{\cfrac {\partial \varepsilon _{jk}}{\partial x_{1}}}\right]~dA}

Now, for an elastic material the stress can be derived from the stored energy functionW{\displaystyle W} using

σjk=Wεjk{\displaystyle \sigma _{jk}={\cfrac {\partial W}{\partial \varepsilon _{jk}}}}

Then, if the elastic modulus tensor is homogeneous, using thechain rule of differentiation,

σjk εjkx1=Wεjk εjkx1=Wx1{\displaystyle \sigma _{jk}~{\cfrac {\partial \varepsilon _{jk}}{\partial x_{1}}}={\cfrac {\partial W}{\partial \varepsilon _{jk}}}~{\cfrac {\partial \varepsilon _{jk}}{\partial x_{1}}}={\cfrac {\partial W}{\partial x_{1}}}}

Therefore, we haveJ1=0{\displaystyle J_{1}=0} for a closed contour enclosing a simply connected region without any elastic inhomogeneity, such as voids and cracks.

Proof that the J-integral is path-independent
Figure 2. Integration paths around a notch in two dimensions.

Consider the contourΓ=Γ1+Γ++Γ2+Γ{\displaystyle \Gamma =\Gamma _{1}+\Gamma ^{+}+\Gamma _{2}+\Gamma ^{-}}. Since this contour is closed and encloses a simply connected region, the J-integral around the contour is zero, i.e.

J=J(1)+J+J(2)J=0{\displaystyle J=J_{(1)}+J^{+}-J_{(2)}-J^{-}=0}

assuming that counterclockwise integrals around the crack tip have positive sign. Now, since the crack surfaces are parallel to thex1{\displaystyle x_{1}} axis, the normal componentn1=0{\displaystyle n_{1}=0} on these surfaces. Also, since the crack surfaces are traction free,tk=0{\displaystyle t_{k}=0}. Therefore,

J+=J=Γ(Wn1tk ukx1)dΓ=0{\displaystyle J^{+}=J^{-}=\int _{\Gamma }\left(Wn_{1}-t_{k}~{\cfrac {\partial u_{k}}{\partial x_{1}}}\right)\,d\Gamma =0}

Therefore,

J(1)=J(2){\displaystyle J_{(1)}=J_{(2)}}

and the J-integral is path independent.

J-integral and fracture toughness

[edit]

For isotropic, perfectly brittle, linear elastic materials, the J-integral can be directly related to thefracture toughness if the crack extends straight ahead with respect to its original orientation.[6]

For plane strain, underMode I loading conditions, this relation is

JIc=GIc=KIc2(1ν2E){\displaystyle J_{\rm {Ic}}=G_{\rm {Ic}}=K_{\rm {Ic}}^{2}\left({\frac {1-\nu ^{2}}{E}}\right)}

whereGIc{\displaystyle G_{\rm {Ic}}} is the critical strain energy release rate,KIc{\displaystyle K_{\rm {Ic}}} is the fracture toughness in Mode I loading,ν{\displaystyle \nu } is the Poisson's ratio, andE is theYoung's modulus of the material.

ForMode II loading, the relation between the J-integral and the mode II fracture toughness (KIIc{\displaystyle K_{\rm {IIc}}}) is

JIIc=GIIc=KIIc2[1ν2E]{\displaystyle J_{\rm {IIc}}=G_{\rm {IIc}}=K_{\rm {IIc}}^{2}\left[{\frac {1-\nu ^{2}}{E}}\right]}

ForMode III loading, the relation is

JIIIc=GIIIc=KIIIc2(1+νE){\displaystyle J_{\rm {IIIc}}=G_{\rm {IIIc}}=K_{\rm {IIIc}}^{2}\left({\frac {1+\nu }{E}}\right)}

Elastic-plastic materials and the HRR solution

[edit]
Paths for J-integral calculation around a crack in a two-dimensional elastic-plastic material.

Hutchinson, Rice and Rosengren[8][9] subsequently showed that J characterizes thesingular stress and strain fields at the tip of a crack in nonlinear (power law hardening) elastic-plastic materials where the size of the plastic zone is small compared with the crack length. Hutchinson used a materialconstitutive law of the form suggested byW. Ramberg and W. Osgood:[10]

εεy=σσy+α(σσy)n{\displaystyle {\frac {\varepsilon }{\varepsilon _{y}}}={\frac {\sigma }{\sigma _{y}}}+\alpha \left({\frac {\sigma }{\sigma _{y}}}\right)^{n}}

whereσ is thestress in uniaxial tension,σy is ayield stress,ε is thestrain, andεy =σy/E is the corresponding yield strain. The quantityE is the elasticYoung's modulus of the material. The model is parametrized byα, a dimensionless constant characteristic of the material, andn, the coefficient ofwork hardening. This model is applicable only to situations where the stress increases monotonically, the stress components remain approximately in the same ratios as loading progresses (proportional loading), and there is nounloading.

If a far-field tensile stressσfar is applied to the body shown in the adjacent figure, the J-integral around the path Γ1 (chosen to be completely inside the elastic zone) is given by

JΓ1=π(σfar)2.{\displaystyle J_{\Gamma _{1}}=\pi \,(\sigma _{\text{far}})^{2}\,.}

Since the total integral around the crack vanishes and the contributions along the surface of the crack are zero, we have

JΓ1=JΓ2.{\displaystyle J_{\Gamma _{1}}=-J_{\Gamma _{2}}\,.}

If the path Γ2 is chosen such that it is inside the fully plastic domain, Hutchinson showed that

JΓ2=αKn+1r(n+1)(s2)+1I{\displaystyle J_{\Gamma _{2}}=-\alpha \,K^{n+1}\,r^{(n+1)(s-2)+1}\,I}

whereK is a stress amplitude, (r,θ) is apolar coordinate system with origin at the crack tip,s is a constant determined from an asymptotic expansion of the stress field around the crack, andI is a dimensionless integral. The relation between the J-integrals around Γ1 and Γ2 leads to the constraint

s=2n+1n+1{\displaystyle s={\frac {2n+1}{n+1}}}

and an expression forK in terms of the far-field stress

K=(βπαI)1n+1(σfar)2n+1{\displaystyle K=\left({\frac {\beta \,\pi }{\alpha \,I}}\right)^{\frac {1}{n+1}}\,(\sigma _{\text{far}})^{\frac {2}{n+1}}}

whereβ = 1 forplane stress andβ = 1 −ν2 forplane strain (ν is thePoisson's ratio).

The asymptotic expansion of the stress field and the above ideas can be used to determine the stress and strain fields in terms of the J-integral:

σij=σy(EJrασy2I)1n+1σ~ij(n,θ){\displaystyle \sigma _{ij}=\sigma _{y}\left({\frac {EJ}{r\,\alpha \sigma _{y}^{2}I}}\right)^{{1} \over {n+1}}{\tilde {\sigma }}_{ij}(n,\theta )}
εij=αεyE(EJrασy2I)nn+1ε~ij(n,θ){\displaystyle \varepsilon _{ij}={\frac {\alpha \varepsilon _{y}}{E}}\left({\frac {EJ}{r\,\alpha \sigma _{y}^{2}I}}\right)^{{n} \over {n+1}}{\tilde {\varepsilon }}_{ij}(n,\theta )}

whereσ~ij{\displaystyle {\tilde {\sigma }}_{ij}} andε~ij{\displaystyle {\tilde {\varepsilon }}_{ij}} are dimensionless functions.

These expressions indicate thatJ can be interpreted as a plastic analog to thestress intensity factor (K) that is used in linear elastic fracture mechanics, i.e., we can use a criterion such asJ >JIc as a crack growth criterion.

See also

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References

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  1. ^abVan Vliet, Krystyn J. (2006); "3.032 Mechanical Behavior of Materials"
  2. ^G. P. Cherepanov, The propagation of cracks in a continuous medium, Journal of Applied Mathematics and Mechanics, 31(3), 1967, pp. 503–512.
  3. ^abJ. R. Rice,A Path Independent Integral and the Approximate Analysis of Strain Concentration by Notches and Cracks, Journal of Applied Mechanics, 35, 1968, pp. 379–386.
  4. ^Lee, R. F., & Donovan, J. A. (1987). J-integral and crack opening displacement as crack initiation criteria in natural rubber in pure shear and tensile specimens. Rubber chemistry and technology, 60(4), 674–688.[1]
  5. ^Meyers and Chawla (1999): "Mechanical Behavior of Materials," 445–448.
  6. ^abYoda, M., 1980,The J-integral fracture toughness for Mode II, Int. J. Fracture, 16(4), pp. R175–R178.
  7. ^"J-integral Theory".COMSOL Documentation. COMSOL, Inc. Archived from the original on 2 May 2025. Retrieved2 May 2025.{{cite web}}: CS1 maint: bot: original URL status unknown (link)
  8. ^Hutchinson, J. W. (1968),"Singular behaviour at the end of a tensile crack in a hardening material"(PDF),Journal of the Mechanics and Physics of Solids,16 (1):13–31,Bibcode:1968JMPSo..16...13H,doi:10.1016/0022-5096(68)90014-8
  9. ^Rice, J. R.; Rosengren, G. F. (1968),"Plane strain deformation near a crack tip in a power-law hardening material",Journal of the Mechanics and Physics of Solids,16 (1):1–12,Bibcode:1968JMPSo..16....1R,doi:10.1016/0022-5096(68)90013-6, archived fromthe original on September 4, 2013
  10. ^Ramberg, Walter; Osgood, William R. (1943), "Description of stress-strain curves by three parameters",US National Advisory Committee for Aeronautics,902

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