Biomedical Engineering Reference
In-Depth Information
Fig. 16.8
Core-shell composite Young's modulus (
n ¼
6) compares favorably to layered
composites theoretical prediction. The close agreement is indicative of integration of the mem-
brane shell with scaffold core. Shell thicknesses: 23, 45, 78, and 155
m. Error bars: Mean
SD.
m
(Reproduced, with permission, from Caliari et al. [
1
])
After separate mechanical characterization of aligned CG scaffolds and CG
membranes, CG scaffold-membrane composites were fabricated and characterized
using membranes ranging in thicknesses from 23
m(1%
2
wrapped twice around scaffold). These scaffolds demonstrated dramatically
increased tensile moduli over CG scaffold controls (no membrane shell) with a 36-
fold increase observed for the 155
m(0.5%1
)to155
m
m
mmembrane thickness. Experimental results were
compared to predictions from layered composites theory. Layered composites theory
has previously been used to accurately predict the tensile properties of multicompo-
nent materials based on the relative size of the individual components and their
separate moduli [
1
]. CG core-shell composite Young's modulus
ðE
composite
Þ
can be
predicted by the rule of mixtures as a function of scaffold core Young's modulus
ðE
scaffold
Þ
, membrane shell Young's modulus
E
membrane
,compositeradius(
r
), and
membrane thickness (
t
)[
1
]:
m
!
þ E
membrane
1
ð
r
t
Þ
!
2
2
ðr tÞ
E
composite
¼ E
scaffold
(16.1)
r
2
r
2
Experimental results correlate well with theoretical predictions, especially for
composites with the two thicker membranes (78, 155
m
m) (Fig.
16.8
). The close
Search WWH ::
Custom Search