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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;

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