Crack Paths 2012
Assuming a uniform distribution for the fibres, the peak stress due to the fibre crack
bridging is [2]:
¸¸¹·¨¨©§ 22 0 1 1 fef f f f f S W K where f = snubbing coefficient (usually ranging from 0.7 to 0.9), 2 DL
0 W = frictional bond
(7)
V
0
f L 2 = fibre length,
f K = volume fraction of fibres.
stress,
f D = fibre diameter,
depends on the angle
Dˆ
between the fibre
If unidirectional fibres are examined,
0 V
direction and the truss direction in the lattice:
ˆ 0
K
W
L
(8)
D
2
f
f f
f
V
D
e
0
The peak stress due to the fibre crack bridging in the truss of the lattice normal to a
0 ) 2 ( 3 V A (el.g.
V
putative ModeI crack plane is equal to
see, in Eq. 4, the stress
0
in the truss (1) when x is the loading axis).
The characteristic cracking strain values of the crack bridging curve due to fibres can
be determined by smearing the crack opening along the length of the truss, namely:
> @ f f f D E L w U W 1 0 2 0 (with
>@fffEEKKU 1
lw0
, lwfu f u , , H , where
)
0 H
is the crack opening at the peak stress of the crack bridging law due to fibres, and
f f u L w ,
is the ultimate crack opening of the bridging law due to fibres.
C O M P A R I SBOENT W E EN NU M E R I C ANLDE X P E R I M E N TR AE SLU L T S
The fracture behaviour of plain and fibre-reinforced concrete coupons under tensile
loading is examined herein by means of the two computational models being compared.
The first one, based on a continuum approach, has been implemented in an in-house
code, whilst the second one, based on a lattice approach, has been implemented in the
subroutine U M A oTf the commercial FEcode ABAQUS.
An experimental campaign related to prismatic Reactive Powder Concrete (RPC)
specimens subjected to tensile stress is examined [18]. The specimens have a total
length equal to 700 m mand cross section of 50x20 m m (Fig. 2). The mechanical
parameters of the R P C concrete are the following: Young modulus
E 50 GPa ,
[19]. The relevant
ultimate tensile strength
0.8 M P a
, fracture energy
f G
30 N/m
tf
%0.2
f K
parameters for unidirectional steel fibres are: fibre volume
, Young modulus
and diameter
f E
210 GPa
, fibre length
2
f L
m m 1 3
f D
mm16.0
, while the limit
matrix-fibre shear stress is equal to
0.2 M P a
. The analysis is performed under
0 W
displacement control by imposing a progressive upward vertical displacement at the top
of the specimens. A plane stress condition is assumed. Five orientations of fibres are
q q q q q 9 0 , 6 0 , 4 5 , 3 0 , 0 M
considered (
) together with the cases of random fibres and of
plain concrete (no fibres).
In Fig. 2, some crack paths of the continuum and the lattice models are shown.
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