The Griffiths equation describes the relationship between applied nominal stress and crack length at fracture, i.e. when it becomes energetically favourable for a crack to grow.  Griffith was concerned with the energetics of fracture, and considered the energy changes associated with incremental crack extension.

For a loaded brittle body undergoing incremental crack extension, the only contributors to energy changes are the energy of the new fracture surfaces (two surfaces per crack tip) and the change in potential energy in the body.  The surface energy term (S) represents energy absorbed in crack growth, while the some stored strain energy (U) is released as the crack extends (due to unloading of regions adjacent to the new fracture surfaces).  Surface energy has a constant value per unit area (or unit length for a unit thickness of body) and is therefore a linear function of (crack length), while the stored strain energy released in crack growth is a function of (crack length)2, and is hence parabolic.  These changes are indicated in the figure below:

Griff1.jpg (97770 bytes)

The next step in the development of Griffith's argument was consideration of the rates of energy change with crack extension, because the critical condition corresponds to the maximum point in the total energy curve, i.e. dW/da = 0, where a = a*.  For crack lengths greater than this value (under a given applied stress), the body is going to a lower energy state, which is favourable, and hence fast fracture occurs.  dW/da = 0 occurs when dS/da = dU/da.  The sketch below shows these energy rates, or differentials with respect to a.

Griff2.jpg (21736 bytes)

R is the resistance to crack growth (= dS/da) and G is the strain energy release rate (= dU/da).

When fracture occurs, R = G and we can define Gcrit as the critical value of strain energy release, and equate this to R.  Hence Gcrit represents the fracture toughness of the material.  In plane stress the Griffith equation is:

where, to get the fracture stress in MPa (the standard SI engineering unit), the critical strain energy release rate is in N/m, E is in N/m2, and a is in m.  This provides an answer in N/m2 (Pa), which needs to be divided by 106 to get the standard engineering unit of MPa.  In plane strain:

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