GTBL042-09 GTBL042-Callister-v3 October 4, 2007 11:53
2nd Revised Pages
9.5 Principles of Fracture Mechanics • 297
ρt
σ 0
σ 0
X X'
x'x
2 a
a
Position along X–X'
(b)
σ 0
σm
Stress
x x'
(a)
Figure 9.8 (a) The geometry of surface and internal cracks. (b) Schematic stress profile
along the lineX–X′in (a), demonstrating stress amplification at crack tip positions.
which is simply a measure of the degree to which an external stress is amplified at
the tip of a crack.
By way of comment, it should be said that stress amplification is not restricted to
these microscopic defects; it may occur at macroscopic internal discontinuities (e.g.,
voids), at sharp corners, and at notches in large structures.
Furthermore, the effect of a stress raiser is more significant in brittle than in duc-
tile materials. For a ductile material, plastic deformation ensues when the maximum
stress exceeds the yield strength. This leads to a more uniform distribution of stress in
the vicinity of the stress raiser and to the development of a maximum stress concen-
tration factor less than the theoretical value. Such yielding and stress redistribution
do not occur to any appreciable extent around flaws and discontinuities in brittle
materials; therefore, essentially the theoretical stress concentration will result.
Using principles of fracture mechanics, it is possible to show that the critical stress
σcrequired for crack propagation in a brittle material is described by the expression
σc=
(
2 Eγs
πa
) 1 / 2
(9.3)
Critical stress for
crack propagation in
a brittle material
where
E=modulus of elasticity
γs=specific surface energy
a=one half the length of an internal crack
All brittle materials contain a population of small cracks and flaws that have a
variety of sizes, geometries, and orientations. When the magnitude of a tensile stress
at the tip of one of these flaws exceeds the value of this critical stress, a crack forms