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.
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)
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
The J-integral around a crack tip is frequently expressed in a more general form[7] (and inindex notation) as
where is the component of the J-integral for crack opening in the direction and is a small region around the crack tip.UsingGreen's theorem we can show that this integral is zero when the boundary 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 of is zero over a closed contour in a simply connected domain. Let us just consider the expression for which is
where is the area enclosed by the contour. Now, if there areno body forces present, equilibrium (conservation of linear momentum) requires that
Also,
Therefore,
From the balance of angular momentum we have. Hence,
The J-integral may then be written as
Now, for an elastic material the stress can be derived from the stored energy function using
Then, if the elastic modulus tensor is homogeneous, using thechain rule of differentiation,
Therefore, we have 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 contour. Since this contour is closed and encloses a simply connected region, the J-integral around the contour is zero, i.e.
assuming that counterclockwise integrals around the crack tip have positive sign. Now, since the crack surfaces are parallel to the axis, the normal component on these surfaces. Also, since the crack surfaces are traction free,. Therefore,
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
where is the critical strain energy release rate, is the fracture toughness in Mode I loading, 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 () is
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]
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
Since the total integral around the crack vanishes and the contributions along the surface of the crack are zero, we have
If the path Γ2 is chosen such that it is inside the fully plastic domain, Hutchinson showed that
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
and an expression forK in terms of the far-field stress
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:
where and 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.
^G. P. Cherepanov, The propagation of cracks in a continuous medium, Journal of Applied Mathematics and Mechanics, 31(3), 1967, pp. 503–512.
^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.
^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]
^Meyers and Chawla (1999): "Mechanical Behavior of Materials," 445–448.
^abYoda, M., 1980,The J-integral fracture toughness for Mode II, Int. J. Fracture, 16(4), pp. R175–R178.
^"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)
^Ramberg, Walter; Osgood, William R. (1943), "Description of stress-strain curves by three parameters",US National Advisory Committee for Aeronautics,902