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Linear Elastic Fracture Mechanics 53
FIGURE 2.23 Plot of stress intensity solutions from Table 2.4.
Although stress intensity solutions are given in a variety of forms, K can always be related to
the through crack (Figure 2.4) through the appropriate correction factor:
K ( I II III) ,, Y a= σπ (2.47)
where
σ = characteristic stress
a = characteristic crack dimension
Y = dimensionless constant that depends on the geometry and the mode of loading
EXAMPLE 2.4
Show that the K I solution for the single edge notched tensile panel reduces to Equation (2.42) when a << W.
Solution: All of the K I expressions in Table 2.4 are of the form:
P a
K = BW f w
I
where
P = applied force
B = plate thickness
f(a/W) = dimensionless function