Crack Paths 2006
110 1000 100 0 (a) m
0.002 λ = ∞ Torsion
tulbenggtahge wall hickness
0.000
0.001
0.003 Transition Strains Energy, εt =0.0011 Area, εt =0.0 8
0.004
tube gage l n th
50μmshear crack de ection esolution
)
m )
λ=3
tube wall hickness
1100 1000
(b)
100
TransitionStrains Energy,εt=0.0019
Area, εt =0.0011
50μmshear crack
detection resolution
0.000
0.001 Equivalent Strain Amplitude, Δε/2 0.002 0.003
0.004
Equivalent Strain Amplitude, Δε/2
tubegage length
50μmshearcrack
m )
λ=3/2
tube wall hickness
Transition Strains
Energy, εt =0.0039
Area, ε t =0.0014
detection resolution
(2)
(c)
1 1010100
Detected Crack
0.000
0.001
0.002
0.003
0.004
Equivalent Strain Amplitude, Δε/2
λ=0 Uniaxial
m
m
tube gage l n th ube w ll hickness
50μmshear crack detection resolution
tube gage tulbne wthll hickness
110 1000 )
)
(d)
Transition Strains Energy, εt = .0079 Area, εt =0.0 1 λ=3/4
100
0.000
0.001
0.002
0.003 0.007 0.008
10 100 1000
(e)
1000
TransitionStrainsEnergy,εt=0.0165
Area, ε t =0.0025
0.001 Equivalent Strain Amplitude, Δε/2 0.002
Equivalent Strain Amplitude, Δε/2
0.000
0.003 0.016 0.017
Figure 4. Experimental observations and predictions of maximumshear crack lengths
(before crack growth changes to maximumtensile planes). For strains which
exceed the transition strain (εt), models predict a shear crack that grows until it
spans the gage length (2c = 30mm).
plane and then back again to growth on a shear plane – in these cases it is the initial shear
crack half-length at the change in cracking modethat is plotted. With the exception of a
single test (λ = 3/2, Δ¯εeff/2 = 0.0008) all of the tests plotted at the 50μmdetection limit
had initial shear cracks that were not detected. While the experimental data in the figure
has a significant amount of scatter, it does show that the material exhibits increasingly
longer shear cracks as shear the strain amplitude and the biaxial strain ratio increase.
Each of the two crack growth mode transition models predicts that above a certain
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