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47

h

௜௝௢

ൌ ln

ܨ

௜௝

ln

ܨ

௜௝ ௙

can be used instead, and typical diameter of a hole and its eccentricity are denoted by

R:ൌ ܽ ൅ ܾ 2 , ݁: ൌ ܽ െ ܾ ܽ ൅ ܾ .

A1-3. Strain hardening was assumed to be described by Ramberg-Osgood rule, i.e.

ߪ

ߪ

ߝ

(3)

where

1

is equivalent stress at

ߝ

ൌ 1

and as before

ߝ

ൌ 2 3⁄

ߝ ݎݐ

ᇱଶ

is equivalent total

strain, respectively. Moreover, Mises yield surface and associativity of flow rule was

accepted even at fracturing. As two special cases of the above hardening model he takes:

n

= 0, as obvious non-hardening case, and

n

= 1, which he claims to be equation

corresponding to linear viscoelastic behaviour.

A1-4. Rotation of principal axes of stresses is assumed to be negligible during stress

history, which means that only principal stresses and strains considered (as mentioned at

the beginning of this subsection the analysis is not intended to describe shears but only

normal strains).

A1-5. Plastic zone covers all the considered body, and thermal effects are neglected.

Analysis

1

.

McClintock first derived change of his damage measure, Eq. (2), for circular cylin-

drical parallel holes in non-hardening plastic material (

ߪ

ൌ ܿ݋݊

,ݐݏ

i.e. n = 0).

Assuming, moreover, absence of plastic volume change for a representative circular

cylinder (Fig. 1.b) and integrating radial equilibrium equation for axisymmetric

generalized plane strain he obtained following analytical solution, /23/ - Eq. (11):

ln ܴ ܴ

ߝ

ҧ√3 2

sinh

ቈ √3 2

ߪ

ߪ

ߪ

ത ቉ ൅

ߝ

ߝ

2

(4)

2. On the other hand, for a linear viscoelastic material obeying the evolution equation

ߝ

ൌ 1 2

T'

(5)

where



#

=

const

is viscosity coefficient, under the condition of constant stress deviator

we have

ߪ

ഥ ൌ

ߪ

ݐ

3

#

⁄ .

The corresponding solutions, according to /17/, now read

ln ܴ ܴ

ൌ 3

ߝ

ҧ

ߪ

ߪ

ߪ

ത ൅

ߝ

ߝ

2

(6)

݁ ൌ

ߪ

ߪ

ߪ

ߪ

൅ ൬݁

ߪ

ߪ

ߪ

ߪ

൰ ݁

ݔ

݌ ൤ െ3

ߝ

ҧ 2

ߪ

ߪ

ߪ

ത ൨

(7)

3. Taking Eqs. (1) and (5) as two limiting cases of the power hardening Eq. (3),

corresponding to

n

=0 and

n

=1, respectively, next interpolation is introduced in /23/

ln

ܴ ܴ

ൌ ߳ҧ√3 2ሺ1 െ ݊ሻ

ݏ

݄݅݊ ቈ √3ሺ1 െ ݊ሻ 2

ߪ

ߪ

ߪ

ത ቉ ൅

ߝ

ߝ

2

(8)

݁ ൌ

ߪ

ߪ

ߪ

ߪ

൅ ൬݁

ߪ

ߪ

ߪ

ߪ

൰ ݁

ݔ

݌ ቆ െ√3

ߝ

ҧ 1 െ ݊

ݏ

݄݅݊ ቈ √3ሺ1 െ ݊ሻ 2

ߪ

ߪ

ߪ

ത ቉ቇ

(9)

Which, reduces to Eqs. (4), (6) - (7) in the mentioned limiting cases. By means of

identity

ܾ ൌ ܴሺ1 െ ݁ሻ

and of logarithmic (true) strain

ߝ

ൌ lnሺ݈

݈

௕଴

⁄ ሻ

from Eq. (2)