Biomedical Engineering Reference
In-Depth Information
Fig. 10.2
A fiber is brought into contact with a substrate. Depending upon the shape of the fiber
tip, the detachment process can occur either by (
a
) crack propagation (
singular shapes
) equivalent
to an infinite crack external to the contact area or by (
b
) uniform detachment (
optimal shapes
)in
which the stress at pull-off is uniformly distributed and equal to the theoretical adhesion strength
s
th
. The difference between the adhesive strength of these two failure modes vanishes as the size of
the fibril is reduced to below a threshold
R
cr
¼
8
E
Dg
ps
, which is taken as the condition for flaw
2
th
tolerant adhesion
material that allows the contact to fail not by crack propagation, but always by
uniform detachment at the theoretical strength of adhesion, a concept termed as
flaw
tolerance
[
7
,
25
,
26
]. According to this concept, in an ideal flaw tolerant adhesion
system, there should be no crack propagation and coalescence as the contact
interface is pulled apart by uniform detachment.
For a single fiber on substrate, Gao and Yao [
23
] investigated the condition for
flaw tolerant adhesion from the point of view of variations in contact shape. It was
shown that there exist two extreme classes of contact shapes: one class (singular
shapes) gives rise to a singular stress field at pull-off similar to that of an external
crack (Fig.
10.2a
) and the other class (optimal shapes) leads to a uniform stress at
pull-off (Fig.
10.2b
). For singular shapes, the pull-off force can be calculated
according to the Griffith condition [
10
]as
r
8
p
1
=
2
E
W
ad
R
P
crack
¼ pR
2
(10.1)
s
Þ=E
s
1
,
E
f
; E
s
; n
f
; n
s
being the Young's moduli and Poisson's ratios of the fiber and the
substrate, respectively. For a gecko sticking to a solid surface, we assume
E
s
E
f
,
therefore
E
E
f
=ð
1
n
where
W
ad
denotes the work of adhesion and
E
¼½ð
1
n
2
2
f
Þ=E
f
þð
1
n
2
f
Þ
. On the other hand, the pull-off force for optimal
contact shapes (Fig.
10.2b
)is
P
th
¼ pR
2
s
th
(10.2)
where
s
th
is the theoretical adhesion strength. Generally,
P
crack
is much smaller than
P
th
. However, as the size of the fiber is reduced, the value of
P
crack
increases towards
P
th
. At the critical size
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