Rasmus ÿstergaard forside 100%.indd - Solid Mechanics
Rasmus ÿstergaard forside 100%.indd - Solid Mechanics
Rasmus ÿstergaard forside 100%.indd - Solid Mechanics
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310 R.C. Østergaard, B.F. Sørensen<br />
Fig. 6 The<br />
load-independent phase<br />
angle ω as function of the<br />
elastic mismatch parameter<br />
for a number of different<br />
thickness ratios. The arrow<br />
indicate the value<br />
corresponding to a<br />
symmetric, homogeneous<br />
DCB specimen loaded by an<br />
axial force<br />
Fig. 7 The shear stress<br />
contours<br />
σ12 H/P = 0.1, 0.05, 0.01<br />
for a sandwich specimen<br />
with η = 1, β =−0.2 and<br />
= 0.5, 0, 05 and 0.005,<br />
respectively<br />
ω [ ◦ ]<br />
from a FEM solution with the CSDE method. First, the<br />
method determines the load combination that results in<br />
the largest deviation between Ganaand Gtrue and then<br />
<br />
it calculates an relative error ξ = Gana−Gtrue<br />
<br />
<br />
for this<br />
Gtrue<br />
combination of the loads. Details on the procedure is<br />
found in Appendix C. Figure 8a–d shows curves for the<br />
intact length of the specimen, (L − a)/H, that gives an<br />
error ξ = 0.05.<br />
The curves show that for >0.01, the length of<br />
the intact part of the sandwich specimen must be larger<br />
than 10H to ensure that the error, ξ, stays below 5%.<br />
This holds for all analyzed values of η ≤ 8. For an<br />
elastic mismatch = 0.001, (L − a) must be larger<br />
to ensure low errors on G. For instance, a sandwich<br />
specified by η = 1, = 0.001 and β = 0anerror<br />
ξ = 5% is found for (L − a)/H = 27.<br />
It was found that the error, ξ, is strongly dependent<br />
on (L − a)/H and a small change of (L − a) changes<br />
123<br />
90<br />
80<br />
70<br />
60<br />
50<br />
40<br />
30<br />
20<br />
10<br />
η = 10 η = 8<br />
η = 4<br />
β = 0<br />
β = −0.3<br />
η = 1<br />
η = 0.2<br />
0<br />
0.001 0.01 0.1 1<br />
Σ<br />
η = 0, Σ= 1<br />
ω = 49.1◦ ξ significantly. Increasing (L − a) with 2H, typically<br />
results in an error that is practically zero; vice versa,<br />
reducing the length with 2H results in large deviations<br />
on G.<br />
As seen in Fig. 7 the stress field also elongates slightly<br />
towards the cracked end of the specimen (x1 =−a).<br />
However, an investigation showed that errors above 1%<br />
does not appear for a/H > 4.<br />
5 Example: a method for measuring interfacial<br />
fracture toughness of sandwich specimens under<br />
mixed mode loadings<br />
It is well known from experiments and modeling works<br />
that the fracture toughness of weak interfaces can depend<br />
on the mode mixity (Cao and Evans 1989;<br />
Wang and Suo 1990; Liechti and Chai 1992;