28.08.2013 Views

Rasmus ÿstergaard forside 100%.indd - Solid Mechanics

Rasmus ÿstergaard forside 100%.indd - Solid Mechanics

Rasmus ÿstergaard forside 100%.indd - Solid Mechanics

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

Interface crack in sandwich specimen 315<br />

Fig. B.1 Mesh used in the<br />

analysis<br />

intensity factor, respectively. Analogously, k2 and k4<br />

are determined with P = 0 and M = 1.<br />

The imaginary and the real parts of K are<br />

<br />

ℑ(K ) = G 16 cosh2 1/2<br />

πɛ<br />

sin (ψ − ɛ ln H)<br />

c1 + c2<br />

and<br />

<br />

ℜ(K ) = G 16 cosh2 1/2<br />

πɛ<br />

cos (ψ − ɛ ln H),<br />

c1 + c2<br />

respectively. G and ψ are determined by the CSDE<br />

method described in Appendix B.<br />

In order to characterize the deviation on the energy<br />

release rate between a long sandwich specimen where<br />

the homogeneous strain state is present and one with<br />

a more complex strain field (e.g. caused by a too short<br />

uncracked beam length), the following error measure<br />

is introduced<br />

<br />

<br />

ξ = <br />

|K |<br />

<br />

2 num −|K |2ana |K | 2 <br />

<br />

<br />

. (C.2)<br />

num<br />

Here |K | num is the modulus of K determined numerically<br />

by the CSDE method and |K | ana is the modulus<br />

of K determined analytically according to the results<br />

in Sect. 3.<br />

Having determined the k’s numerically and introducing<br />

¯λ = PH<br />

M , it is found that<br />

Knum = (k1 ¯λ + k2) + i(k3 ¯λ + k4) M<br />

and the modulus of Knum squared can then be written<br />

as<br />

|K | 2 num =<br />

<br />

(k1 ¯λ + k2) 2 + (k3 ¯λ + k4) 2<br />

M 2 , (C.3)<br />

which we will rewrite in the form<br />

|K | 2 num = B ¯λ 2 + C ¯λ + D, (C.4)<br />

P<br />

where<br />

B = k 2 3 + k2 1<br />

(a)<br />

(b)<br />

C = 2(k3k4 + k1k2)<br />

D = k 2 4 + k2 2 .<br />

Using (16) and (6), an analytical expression based<br />

on the strain fields given in Appendix A for the modulus<br />

of the complex stress intensity factor is found<br />

|K | 2 ana = (b¯λ 2 + c¯λ + d)M 2<br />

(C.5)<br />

b = q 1<br />

H 3<br />

η<br />

U<br />

c = q 1<br />

H 3<br />

2sinγ<br />

√<br />

UVη2 d = q 1<br />

H 3<br />

1<br />

η 3 V ,<br />

where q = c2 cosh2 (πɛ)<br />

. c1+c2<br />

For fixed α, β, η and a/H the error, ξ, depends on<br />

(L − a) and ¯λ. In order to determine the error for a<br />

certain length, the worst case load combination, ¯λc, is<br />

determined. ¯λc is found by differentiating (C.2) and<br />

= 0. The derivative of (C.2)is<br />

setting ∂ξ<br />

∂ ¯λ<br />

∂ξ<br />

∂ ¯λ =−(dB − bD) ¯λ 2 + (2 cB − 2 bC) ¯λ + cD − dC<br />

<br />

B ¯λ 2 + C + Dλ 2 Equating this to zero gives two values of ¯λc<br />

<br />

bC − cB ± 2 b<br />

¯λc = 2C 2 − 2 bCcB + c2 B2 − dBcD+ d2 BC + bD2c − bDdC<br />

.<br />

dB − bD<br />

Inserting ¯λc into (C.4) and (C.5) gives|K | 2 num and<br />

|K | 2 ana , respectively. Inserting those values into (C.2)<br />

gives ξ.<br />

123

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!