Although
the normal indentation approach has overcome the disadvantages of
surface curvature and roughness encountered in the lateral indentation
on
fibers,
the influence of matrix emerges as the primary issue of affecting the
normal indentation measurement. The finite stiffness of matrix makes
the “matrix effect” prominent in the measured indentation force–displacement behavior, that is, the measured property is a mixture of the
fiber
and matrix properties even at relatively shallow penetration depths [19]. Hence, the classic indentation theory [14]
based on bulk materials (which is also the default option on many
commercial nanoindenters) can cause error if one would use that to
extract the
fiber
properties without careful considerations. In previous experiments of the normal indentation on
fibers
[7] and [18],
the important contribution of matrix compliance was not considered
although in some cases the indentation depths were on the same order of
fiber/
hair thickness, which may result in error of the reported
fiber
properties since it is expected that at such deep penetration the matrix effect may not be negligible.
While the substrate effect on the thin film indentation problem has been studied extensively [19], [20] and [21], the study of the matrix effect of normal indentation on a
fiber
bounded by a matrix is still lacking. To fulfill the potential of the
normal indentation technique, a theoretical framework needs to be
established to understand and then subtract off the matrix effect from
the measurement, and to obtain the intrinsic mechanical properties of
the micro- and
nano-fiber.
In addition, the developed method can be extended to measure the mechanical properties of
fibers
in a
fiber
-reinforced composite material, without separating
fiber
from the matrix – such convenience in sample preparation may be
important in tissue engineering, where it is very time consuming and
challenging to extract a single
fiber
from its matrix.
1.2. Basic principle of normal indentation on
fiber:
using the matrix effect
With reference to Fig. 1(a), a
fiber
of radius R is embedded in an otherwise semi-infinite matrix, and we assume perfect bonding between the
fiber
and matrix. During a normal indentation test on the center of the cross-section of the
fiber
(Fig. 1(a)), the relationship between indentation load (P) and indentation depth (δ) can be continuously measured with the penetration of a hard indenter tip into the specimen (Fig. 1(b)). Note that due to the complicated stress and strain fields resulting from finite deformation, the P–δ
curve is only implicitly related with the material elastoplastic
properties as well as the material/system structure (e.g. the presence
of interface in the
fiber/
matrix
system) – the functional relationships need to be established such that
through a reverse analysis, the most important and intrinsic elastic
and plastic parameters of the
fiber
can be derived from the experimental data [15].
Although theoretically, one could keep the indentation depth much smaller than the
fiber
radius, so as to avoid the matrix effect and then apply the conventional closed-form formulae based on the Oliver–Pharr method [14], such approach might encounter difficulties for micro- and
nano-fibers
for the following reasons: (1) very shallow nanoscale indentation
experiment often relies on a state-of-the-art commercial nanoindenter
that is not accessible to many users, it is more desirable to develop a
technique that could work for a much less expensive microindenter; (2)
the matrix/substrate effect on elastic property measurement persists at
very small depth especially when the matrix is compliant [19] and [20],
and thus even smaller indentation depth may be required; (3) if a
nanoscale indent is required to avoid the matrix effect in a very thin
fiber,
uncertainties such as surface roughness, adhesion, irregular indenter geometry and size effects may become dominant [21]
which makes the modeling very hard. To circumvent such nanoscale
effects, an indentation test with moderate penetration depth is needed
(so as to apply the well-developed continuum mechanics approach), which
would inevitably induce the matrix effect. The primary goal of this
paper is then to understand the matrix effect and obtain the intrinsic
fiber
properties with the presence of (or assistance of) the matrix effect.
Due
to the lack of analytical solution of the indentation problem involving
finite deformation and two-phase materials, numerical simulations based
on the finite element method (FEM) will be applied to establish
explicit relationships between the mechanical properties of the
fiber
and matrix (such as the elastic modulus and yield stress) and the indentation response (such as the shape factors of the P–δ curve). Inspired by the study of the substrate effect of nanoindentation on thin films [19], [20] and [21], the contribution of matrix is enhanced with increasing δ in the present study. That is, the curvature of the measured P–δ
curve is different at distinct indentation depths, and the matrix
effect can provide sufficient information for determining the
elastoplastic properties of
fiber.
In the following, we will first vary the
fiber
and matrix properties in a wide range, such that during the forward
analysis with FEM simulations, the explicit relationships can be
established between the material properties and the indentation
response at different representative indentation depths (which
correspond to different matrix effects). An effective reverse analysis
is established such that, once the matrix modulus is known or measured,
the elastic modulus and yield stress of the
fiber
can be readily identified from the measured indentation P–δ
curve. The robustness of the technique is verified through numerical
indentation experiments and an error sensitivity analysis. In addition,
parallel experiments on human hair and glass
fibers
are carried out to examine the proposed indentation method, and the results (extracted
fiber
properties) agree well with the reference properties. The framework
proposed in this study may provide an effective approach to measure the
elastoplastic properties of micro- and
nano-fibers.
2. Computation method
2.1. Modeling and basic assumptions
For the
fiber/
matrix system show in Fig. 1(a), the
fiber
is simplified as an elastic-perfectly plastic material. Such assumption is valid for ceramic/glass and high-strength metal
fibers
[22], [23], [24], [25] and [26], in addition, most polymer materials have negligible hardening effect [27] and [28]; moreover, for these materials their tensile and compressive behaviors are almost symmetric, allowing the determination of
fiber’s
elastoplastic properties from indentation test (which is
compression-dominant). The matrix is homogeneous and isotropic, and it
is assumed to deform elastically – such assumption is valid for the
model epoxy matrix (which is also used in parallel experiments
described below) and for the range of
fiber
properties and indentation depths studied in this paper (see below),
where our FEM simulation results verified that at the maximum
penetration, the peak Mises stress induced in epoxy is insufficient to
cause matrix yielding.
Since the matrix is much larger than the
fiber,
the matrix’s Young’s modulus, Em, can be easily measured by using the uniaxial tension test. Alternatively, the Oliver–Pharr method [14]
may be employed to obtain the stiffness of matrix through indentation
(where the matrix can be taken as a bulk material) which is also used
in our parallel experiment in this paper. If the matrix mechanical
property is known, there are only two unknown material parameters: the
fiber’s
Young’s modulus, Ef and the
fiber’s
yield stress, σf,
which can be mathematically determined by using two independent
equations. Meanwhile, more equations may be employed and such
redundancy may help to improve the numerical reverse analysis result
through optimization. The Poisson’s ratio, normally regarded as a minor
factor during indentation [19], is set to be 0.3 for both
fiber
and matrix.
To simplify the analysis, the indenter tip is assumed as a rigid cone with a half apex angle α=70.3°, which has the similar ratio of cross-section area to indentation depth as the widely used Berkovich indenter [15].
It has been reported that the conical indentation has almost the same
loading and unloading curves (with less than 1% difference in general)
as the pyramidal indentation as long as both types of indenters have
the same ratio of cross-section area to indentation depth [15]; therefore, conical indenter will be used in this study to take advantage of axisymmetry (see Section 2.3). Coulomb’s friction law is applied between indenter and
fiber
surface with a friction coefficient of 0.1. The friction is a minor
factor in indentation as long as the friction coefficient is small,
which has been verified by our FEM analysis and other groups [15]. We assume perfect bonding between the
fiber
and matrix during the experiment.
2.2. Basic functional forms based on dimensional analysis
Fig. 1(b) shows a typical P–δ curve, where Pm and δm
are the maximum indentation load and indentation depth, respectively.
From the principle of dimensional analysis, the dimensionless curvature
of the loading curve can be expressed as:
(1)
which may be regarded as shape factors reflecting the matrix effect at various penetrations (e.g. δ1,δ2,δ3). To solve the
fiber
properties (Ef,σf),
the required two independent equations can be provided by the distinct
matrix effects at different indentation loads/depths with (P1,δ1) and (P2,δ2), see Fig. 1(b) where δ1=δm:
(2)
(3)
The dimensionless indentation depths δ1/R and δ2/R are chosen such that their corresponding matrix effects are distinct (δ1/R=0.25 and δ2/R=0.075 in this paper, see Section 3.1 for justification). F1 and F2 are dimensionless functions that can be determined from extensive FEM simulations in forward analysis, see Section 3.1. Practically, one could use more data points (such as (P3,δ3) in Fig. 1(b))
to establish additional (redundant) functional forms of a different
matrix effect, which can help to improve the accuracy of the reverse
analysis, discussed in Section 3.2.4.
Note that with the current normal indentation framework (where the
fiber
is elastic-perfectly plastic), we do not require the use of unloading P–δ curve from the experiment. In fact this is advantageous based on the following reasons:
(1) Since we do not have to perform unloading at the maximum penetration (δ1/R=0.25 in this study), the
fiber
radius does not need to be pre-determined accurately and a moderate scatter of
fiber
radius is allowed. One can indent sufficiently deep to make sure that the maximum depth is above 1/4 of the radii of all
fibers,
without the need to withdraw the indenter at a particular moment. This
extends the applicability of the proposed technique and would be
particular welcome for automated test.
(2) In a nanoindentation
test, stress relaxation is often observed at the maximum load when
unloading just occurs, since both the strain and the strain rate are
very large just beneath the indenter (and the loading rate is usually
finite during the experiment). The sudden withdraw of indenter may
cause oscillations in the measurement and holding at the maximum load
may also lead to uncertainty in the measured quantities. In addition,
the initial portion of unloading is prone to thermal drift. All these
factors require extra attention during the collection of unloading data
[29], [30] and [31] in particular if the indentation depth is very small.
(3) In many established theoretical and numerical indentation techniques, a rigid indenter is used [14], [15], [19], [20], [21] and [25]
whereas in practice, a diamond indenter tip is employed. It is well
known that the unloading behavior is strongly affected by the
compliance of indenter tip [14]. Therefore, in order to apply the developed indentation method based on the rigid indenter, a real P–δ
curve measured from experiment must be converted to that measured by a
rigid indenter – for example, our previous work on thin film
indentation [21] utilizes the unloading work in the indentation analysis, which requires the full information of the unloading P–δ
curve with a rigid indenter, and if the diamond tip contribution is not
properly removed from the experimental data, plus any of the
above-mentioned error due to the nonelastic effects in the unloading P-δ curve, a large error may occur based on error sensitivity analysis [21] and an careless user may make mistakes [32]. Since the diamond tip compliance has much less influence on the loading P–δ
curve (especially at moderate indentation depth adopted in this paper),
it is more convenient to circumvent such difficulty by using the
arguably more reliable loading P–δ curve measured from an experiment.
2.3. Finite element analysis
The FEM simulations are carried out using commercial code ABAQUS [33]. The
fiber
is assumed to be a perfect cylinder and the indentation load is applied along the center axis of
fiber.
With these assumptions, the
fiber
and matrix can be simplified as a 2D axisymmetric system instead of
using three-dimensional model and the computational cost can be
significantly reduced (note that if the
fiber’s
cross-section significantly deviates from circular, or if the indentation load is severely off from the
fiber’s
center axis, then 3D model/analysis must be carried out). The
fiber
is meshed with about 20,000 4-node axisymmetric elements with reduced
integration, and the matrix includes about 15,000 elements with the
same type. The mesh density is designed such that the mesh is more
refined near to the indenter tip along both the axial and the radial
directions. In order to accurately capture the contact radius, the mesh
size is refined in the contact area to make sure more than 200
fiber
elements are in contact with the indenter tip when δ2/R=0.075. The matrix radius is set to be 50 times larger than the
fiber
radius to simulate the semi-infinite “substrate”, and the
fiber
length is taken as 50 times of the
fiber
radius – these dimensions ensures that the matrix is semi-infinite. The
degree of freedom along axial direction of nodes on the bottom of the
fiber
and matrix is fixed to represent the boundary condition when the sample is mounted on a rigid substrate.
In the present numerical experiments, the ratio of Ef/σf
is varied from about 20 to 3000 to cover a wide range of
engineering/biomaterials during the forward analysis, including human
hair and optical
fiber.
Although epoxy is selected as a representative matrix material in the
parallel experiment (the typical epoxy modulus is about 1–5 GPa), the
ratio of Ef/Em
is also varied in a wide range from about 2 to 150, such that the
established framework may be applied to a wide combinations of
fiber/
matrix systems.
2.4. Experiment
To verify the methodology developed in this study, nanoindentations were performed on the cross-section of human hair and glass
fiber
using a Triboscope (Hysitron Inc.) in conjunction with a Veeco
Dimension 3100 AFM system (Veeco Metrology Group). The human hair and
glass
fiber
were embedded into a special epoxy (302-3M, Epoxy Technology Inc.),
which produces no heat or thermal expansion during cure and thus does
not create any stress into the
fibers.
The sample was then cut with a cutting surface perpendicular to the
fiber
using a water-cooled, low speed diamond saw and mechanically ground and
polished using abrasive and powders down to 50 nm. Nanoindentations
were performed on the polished cross-sections of human hairs and glass
fibers
using different indentation forces, with the indentation along the axial direction of the
fibers.
For the determination of reference mechanical properties of the
fibers,
small peak indentation forces (
for human hair and
for glass
fiber)
were first used to generate a shallow penetration depth into the
fibers
(δ/R=0.004 for human hair and δ/R=0.01 for glass
fiber)
so that the matrix effects can be ignored. The indentation loading
curves at moderate depths were then used as an input to derive the
mechanical properties of
fiber
using the established framework, with the detailed results given in Section 4.
Since our method requires the matrix modulus to be known a priori,
nanoindentations were also carried out on the epoxy matrix with a
nominal peak force of
to determine its mechanical properties. For all the indentation tests,
the peak indentation force was applied in 5 s and then totally released
in the same time after 5 s holding at the peak force except a fast
unloading (2 s) for epoxy matrix to minimize the creep effect (note
that the technique proposed in this paper for determining
fiber
properties does not require unloading).
3. Results and discussion
3.1. Forward analysis
Unlike in a homogeneous bulk material where the loading curvature C=P/δ2 is a constant during sharp indentation [15], the stress field and plastic flow beneath the indenter tip will be disturbed by the presence of the matrix in a
fiber/
matrix system, and thus the loading curvature is dependent with the indentation depth (Fig. 1(b)). For a compliant matrix, Ef/Em>1, the loading curvature continuously decreases with the increase of indentation depth; whereas for a stiff substrate, Ef/Em<1,C increases with the increasing δ. In this paper, we choose δ1/R=0.25 and δ2/R=0.075
– for the wide material space adopted in this paper, these two
indentation depths yield sufficiently distinct matrix effects. By
varying Ef/σf from 50 to 3000, and Ef/Em from 2 to 150, the normalized loading curvatures
and
are measured from the numerical indentation experiments, based on which the dimensionless functions F1 and F2 (Eqs. (2) and (3)) are fitted.
Due to the wide range of material properties involved, it is more practical to change Eqs. (2) and (3) to logarithmic form:
(4)
(5)
where ξ=ln(Ef/σf) and η=ln(Ef/Em). The fitting error is less than 1% for the material space considered, with details given in the Appendix A.
The functions f1 and f2 are visualized as two three-dimensional continuous surfaces in Fig. 2: their difference denotes the distinct matrix effect at δ1/R=0.25 and δ2/R=0.075. The normalized loading curvatures increase as Ef/σf decreases or Ef/Em increases. The presence of matrix has a remarkable effect on the normalized indentation load when Ef/σf is large (i.e. more plastic materials), whereas the matrix effect is smaller for materials with smaller Ef/σf (more elastic materials). At the maximum penetration, the plastic flow is still constrained in the small
fiber
and thus the plastic
fibers
are more sensitive to the presence of matrix. In addition, a larger difference between the
fiber/
matrix
elastic moduli will take more advantage of the matrix effect. These two
functions relate the indentation response with the
fiber
elastoplastic properties as well as
fiber/
matrix elastic mismatch; once calibrated via FEM, they can be employed in the reverse analysis for determining the
fiber
properties, discussed next.