This paper was converted on www.awesomepapers.org from LaTeX by an anonymous user.
Want to know more? Visit the Converter page.

Concurrent consideration of cortical and cancellous bone within continuum bone remodelling

\nameIna Schmidta, Areti Papastavroua, and Paul Steinmannb CONTACT Ina Schmidt Author. Email: [email protected] aFaculty of Mechanical Engineering, Nuremberg Tech, Keßlerplatz 12, 90489 Nuremberg, Germany; bChair of Applied Mechanics, University of Erlangen-Nuremberg, Egerlandstraße 5, 91058 Erlangen, Germany
Abstract

Continuum bone remodelling is an important tool for predicting the effects of mechanical stimuli on bone density evolution. While the modelling of only cancellous bone is considered in many studies based on continuum bone remodelling, this work presents an approach of modelling also cortical bone and the interaction of both bone types. The distinction between bone types is made by introducing an initial volume fraction. A simple point-wise example is used to study the behaviour of novel model options, as well as a proximal femur example, where the interaction of both bone types is demonstrated using initial density distributions. The results of the proposed model options indicate that the consideration of cortical bone remarkably changes the density evolution of cancellous bone, and should therefore not be neglected.

keywords:
bone remodelling; cortical bone; cancellous bone; density change; finite element method

1 Introduction

Tubular bone is characterised by cortical bone surrounding the bone marrow in the shaft and the cancellous bone at the proximal and distal ends. Due to its special microstructure composed of beams and plates (trabeculae), cancellous bone is also denoted as spongy bone. Depending on environmental changes, such as mechanical loading, bone can adapt its internal microstructure by altering the density and trabecular orientation. Remodelling of cancellous bone was first formulated by (Wolff 1892) and is referred to as Wolff’s law of bone remodelling. Based on continuum mechanics and the finite element method, simulation approaches to bone remodelling were developed, see (Cowin and Hegedus 1976), (Huiskes et al. 1987), (Weinans et al. 1992), (Harrigan and Hamilton 1993), (Jacobs et al. 1995) and many more. Most of these studies address exclusively the adaptation of cancellous bone. Even if the focus is also on the adaptation of cortical bone, it is typically considered separately from spongy bone, see (Carter and Beauprè 2010). One of the few approaches involving the interaction of both bone types was investigated by (Hambli 2014) and (Barkaoui et al. 2019) based on the cellular activities of bone. Another proposal was developed by (Nutu 2018) based on the model of (Huiskes et al. 1987) for dental implants.

This work aims to simulate bone density changes of cancellous and cortical bone as well as their interplay based on a continuum bone remodelling approach. Unlike spongy bone, the bone fibrils of cortical bone are densely packed, which is why this lamellar structure is also called compact bone. Remodelling of cortical bone can occur along the endosteal and periosteal surface as well as within the channels. The surface area per unit volume is considerably reduced compared to cancellous bone and therefore remodelling requires more time with less change in density. In order to adapt to the load case, the main mechanism considered here is the adjustment of the microstructural density. Whereas a change in bone geometry will not be considered, the simulation of bone adjustments in the endosteal area such as trabecularisation and thinning of the inner compact bone in old age is made possible.

Based on previous studies, see (Kuhl and Steinmann 2003), (Liedtke et al. 2017) (Papastavrou et al. 2020a) and (Papastavrou et al. 2020b), an initial volume fraction is introduced in this work, which is defined as the ratio between initial nominal density and true density and therefore allows a distinction between the two bone types. The influence of this new parameter and the associated modelling of spongy and compact bone will be studied in this context.

In the following, the quantities {}\{\circ\}, which take into account the effective mixture of solid bone material and the (empty) pore space are referred to as nominal quantities, whereas true quantities based on the properties of the solid (bone) material are denoted as {}s\{\circ\}^{s}. Furthermore we distinguish between the initial value {}\{\circ\}^{\star} of a quantity (at time zero), and its current (time-evolving) value {}(t)\{\circ\}(t). The latter should not be confused with the actual configuration, which refers to the geometric description of the deformed continuum body.

This contribution is organised as follows. The governing and constitutive equations including the proposed modification are detailed in Section 2. The performance is illustrated by numerical problems in Section 3. Section 4 provides a concluding discussion.

2 Continuum framework of bone remodelling

With a view on its continuum modelling, bone is here considered as a porous material consisting of a solid skeleton and (empty) pore space, see Fig. 1. In the following, the underlying equations of continuum bone remodelling are briefly re-iterated, see also (Kuhl and Steinmann 2003) and (Holzapfel 2001) for additional details.

2.1 Kinematics

The kinematic description is characterised by the deformation map 𝝋\boldsymbol{\varphi} that maps the referential placement 𝐗\mathbf{X} of a physical particle in the material (reference) configuration 0\mathcal{B}_{0} at time t0t_{0} to its actual placement 𝐱\mathbf{x} in the spatial (actual) configuration t𝔼3\mathcal{B}_{t}\subset\mathbb{E}^{3} at time t+t\in\mathbb{R}_{+}

𝐱=𝝋(𝐗,t):0×+t.\mathbf{x}=\boldsymbol{\varphi}(\mathbf{X},t):\mathcal{B}_{0}\times\mathbb{R}_{+}\to\mathcal{B}_{t}\>. (1)

The referential gradient 0\nabla_{0} of the nonlinear deformation map denotes the deformation gradient 𝐅\mathbf{F}, it maps from the material tangent space T0T\mathcal{B}_{0} to the spatial tangent space TtT\mathcal{B}_{t}

𝐅=0𝝋(𝐗,t):T0Tt.\mathbf{F}=\nabla_{0}\boldsymbol{\varphi}(\mathbf{X},t):T\mathcal{B}_{0}\to T\mathcal{B}_{t}\>. (2)

The determinant of the deformation gradient is the Jacobian J=det𝐅>0J=\det\mathbf{F}>0 and relates the volume elements between the two configurations. The right and left Cauchy-Green tensor 𝐂=𝐅T𝐅\mathbf{C}=\mathbf{F}^{T}\cdot\mathbf{F} and 𝐛=𝐅𝐅T\mathbf{b}=\mathbf{F}\cdot\mathbf{F}^{T} are introduced as characteristic strain measures.

In the following, the expression {}¯˙=t{}|X\dot{\overline{\{\circ\}}}=\partial_{t}\{\circ\}|_{X} is used for the material time derivative of a quantity {}\{\circ\} at fixed material placement 𝐗\mathbf{X}. The presented formulation refers completely to the material configuration. Therefore, 0{}\nabla_{0}\{\circ\} and Div{}\mbox{Div}\{\circ\} denote the (referential) gradient and divergence of any field {}\{\circ\} with respect to the material placement 𝐗\mathbf{X}. A density quantity {}\{\circ\} may be expressed per unit volume {}0\{\circ\}_{0} or per unit mass {}\{\circ\}, both related via the current referential nominal density ρ0\rho_{0} as {}0=ρ0{}\{\circ\}_{0}=\rho_{0}\{\circ\}.

2.2 Balance equations

The balance of linear momentum is given by

Div𝐏=𝟎\mbox{Div}\mathbf{P}=\mathbf{0} (3)

with 𝐏=𝐏(0𝝋,ρ0,)\mathbf{P}=\mathbf{P}(\nabla_{0}\boldsymbol{\varphi},\rho_{0},...) the Piola stress tensor. Since the time scale of inertial effects is significantly smaller than that of the remodelling process, the inertial term is neglected herein (Frost 1987). The loads applied during locomotion typically correspond to a multiple of gravity. Therefore, body forces are usually not considered in bone remodelling as they are not the dominant stimulus (Jacobs et al. 1995).

The balance of mass is given by

ρ0˙=R0\dot{\rho_{0}}=R_{0} (4)

where R0R_{0} is the scalar-value mass source term. As the actual nominal density ρt=ρ0/J\rho_{t}={\rho_{0}}/{J} is time-dependent also due to the coupling with the Jacobian, it is useful to capture the evolution of the referential nominal density ρ0\rho_{0}. The relative change in (referential) nominal density ρ0~\tilde{\rho_{0}} is defined in terms of the initial nominal density ρ0\rho_{0}^{\star} as

ρ0~=ρ0ρ0ρ0.\tilde{\rho_{0}}=\frac{\rho_{0}-\rho_{0}^{\star}}{\rho_{0}^{\star}}. (5)

Therefore, density gain results for values ρ0~>0\tilde{\rho_{0}}>0 whereas density loss is obtained for 1<ρ0~<0-1<\tilde{\rho_{0}}<0.

Refer to caption
Figure 1: Homogenised macro scale with nominal density ρ0(t)\rho_{0}(t) versus heterogeneous micro scale with true density ρ0s\rho_{0}^{s}

2.3 Nominal versus true mass densities

We distinguish between the homogenised macro scale with nominal (time-evolving, referential) density ρ0=ρ0(t)(0,ρ0s]\rho_{0}=\rho_{0}(t)\in(0,\rho_{0}^{s}] occupying the (time-independent, referential) volume element dV\,\mbox{d}V and the heterogeneous micro scale with true (time-independent, referential) density ρ0s\rho_{0}^{s} of the solid skeleton material occupying the (time-evolving, referential) partial volume element dVs=dVs(t)(0,dV]\,\mbox{d}V^{s}=\,\mbox{d}V^{s}(t)\in(0,\,\mbox{d}V], see Fig. 1. The (time-evolving, referential) volume fraction of solid skeleton material thus follows as

ν0=ν0(t):=dVs(t)dV=ρ0(t)ρ0s(0,1].\nu_{0}=\nu_{0}(t):=\frac{\,\mbox{d}V^{s}(t)}{\,\mbox{d}V}=\frac{\rho_{0}(t)}{\rho_{0}^{s}}\in(0,1]. (6)

The (referential) volume fraction ν0(t)\nu_{0}(t) indicates how much space within a (referential) volume element dV\,\mbox{d}V at the macro scale is occupied by solid skeleton material, thus 1ν0(t)1-\nu_{0}(t) denotes the (referential) volume fraction of the (empty) pore space.

At time t=0t=0 the corresponding initial values for the (referential) volume fraction ν0(0)\nu_{0}(0), the (referential) partial volume element dVs(0)\,\mbox{d}V^{s}(0) and the nominal (referential) density ρ0(0)\rho_{0}(0) are related via

ν0:=dVsdV=ρ0ρ0s(0,1].\nu_{0}^{\star}:=\frac{\,\mbox{d}V^{s\star}}{\,\mbox{d}V}=\frac{\rho_{0}^{\star}}{\rho_{0}^{s}}\in(0,1]. (7)

and are denoted the initial (referential) volume fraction ν0:=ν0(0)\nu_{0}^{\star}:=\nu_{0}(0), the initial (referential) partial volume dVs:=dVs(0)\,\mbox{d}V^{s\star}:=\,\mbox{d}V^{s}(0) and the initial nominal (referential) density ρ0:=ρ0(0)\rho_{0}^{\star}:=\rho_{0}(0), respectively. Typically, ν0\nu_{0}^{\star} is significantly higher for cortical bone as compared to cancellous bone.

Furthermore, we may distinguish between the nominal relative (referential) density and its true counterpart

ρ0(t)ρ0ν0(t)ν0(0,)versusρ0(t)ρ0sν0(t)(0,1]\frac{\rho_{0}(t)}{\rho_{0}^{\star}}\equiv\frac{\nu_{0}(t)}{\nu_{0}^{\star}}\in(0,\infty)\quad\mbox{versus}\quad\frac{\rho_{0}(t)}{\rho_{0}^{s}}\equiv\nu_{0}(t)\in(0,1] (8)

when phenomenologically modelling the homogenised mechanical properties of bone based on its skeleton structure at the micro scale, i.e. its microstructure. In the following, the present contribution aims to rationalise various modelling options stemming from this distinction.

2.4 Nominal versus true free energy densities

Bone possesses a microstructure characterised by the spatially heterogeneous distribution of solid skeleton and pore space. The resulting structural bone properties of the heterogeneous solid skeleton at the micro scale may then be homogenised into nominal bone properties of the effective material at the macro scale.

A simplistic, however efficient and effective homogenisation rule – typically employed for cellular materials – relates the true material parameters of the solid skeleton at the micro scale to the corresponding effective, nominal parameters of the homogenised material at the macro scale via a power NN of the initial (referential) volume fraction ν0\nu_{0}^{\star}. Let for example λs\lambda^{s} and μs\mu^{s} denote the Lamé parameters of the solid skeleton material. Then, the homogenised, effective bone material is characterised by the nominal material parameters

λ=[ν0]Nλsandμ=[ν0]NμswithN={1,n}.\lambda^{\star}=[\nu_{0}^{\star}]^{N}\lambda^{s}\quad\mbox{and}\quad\mu^{\star}=[\nu_{0}^{\star}]^{N}\mu^{s}\quad\mbox{with}\quad N=\left\{1,n\right\}\>. (9)

Typically, the concrete values assumed for the homogenisation exponent NN capture different microstructures and homogenisation approaches. In this contribution, either the most elementary volumetric mixture rule with N=1N=1 or a relation with N=nN=n shall be considered. The latter is particularly motivated by the proposal of (Gibson 2005) postulating a dependence of the nominal Young’s modulus of a homogenised (linear elastic) porous material on the Young’s modulus of the solid skeleton material via a power of the true relative density.

In what follows we assume the concept of strain equivalence as also employed in damage mechanics. To elucidate this aspect more concretely, we employ, without loss of generality, a (referential) volume-specific Neo-Hookean true free energy density for the solid skeleton material

Ψ0s=12λsln2J+12μs[𝐅:𝐅32lnJ].\Psi_{0}^{s}=\frac{1}{2}\lambda^{s}\ln^{2}J+\frac{1}{2}\mu^{s}\left[\mathbf{F}:\mathbf{F}-3-2\ln J\right]. (10)

Note that strain equivalence postulates identical ’strain’ at the macro and the micro scale. Thus, based on the nominal material parameters, the corresponding (referential) volume- specific initial nominal free energy follows from its true counterpart as

Ψ0=[ν0]NΨ0s.\Psi_{0}^{\star}=[\nu_{0}^{\star}]^{N}\Psi_{0}^{s}\>. (11)

Concretely, the (referential) volume-specific Neo-Hookean initial nominal free energy reads in terms of the nominal Lamé parameters as

Ψ0=12λln2J+12μ[𝐅:𝐅32lnJ].\Psi_{0}^{\star}=\frac{1}{2}\lambda^{\star}\ln^{2}J+\frac{1}{2}\mu^{\star}\left[\mathbf{F}:\mathbf{F}-3-2\ln J\right]\>. (12)

The initial microstructure evolves with time due to remodelling into the current microstructure, thus necessitating to express the (referential) volume-specific current nominal free energy density Ψ0\Psi_{0} in terms of its initial counterpart.

To this end, again motivated by (Gibson 2005), when taking the microstructure of cellular materials into account, the (referential) volume-specific current nominal free energy density Ψ0\Psi_{0} is determined by weighting its initial nominal counterpart Ψ0\Psi_{0}^{\star} with a power nn of the nominal relative density

Ψ0=[ρ0ρ0]nΨ0.\Psi_{0}=\left[\frac{\rho_{0}}{\rho_{0}^{\star}}\right]^{n}\Psi_{0}^{\star}\>. (13)

Then the Piola stress entering the equilibrium equation derives from the (referential) volume-specific current nominal free energy density Ψ0\Psi_{0} as

𝐏:=Ψ0𝐅=[ρ0ρ0]nΨ0𝐅=:[ρ0ρ0]n𝐏\mathbf{P}:=\frac{\partial\Psi_{0}}{\partial\mathbf{F}}=\left[\frac{\rho_{0}}{\rho_{0}^{\star}}\right]^{n}\frac{\partial\Psi_{0}^{\star}}{\partial\mathbf{F}}=:\left[\frac{\rho_{0}}{\rho_{0}^{\star}}\right]^{n}\mathbf{P}^{\star} (14)

and expands concretely for the Neo-Hookean case with the initial Piola stress

𝐏=λlnJ𝐅t+μ[𝐅𝐅t].\mathbf{P}^{\star}=\lambda^{\star}\ln J\,\mathbf{F}^{-t}+\mu^{\star}[\mathbf{F}-\mathbf{F}^{-t}]\>. (15)

Incorporating the (referential) volume-specific Neo-Hookean true free energy density Ψ0s\Psi_{0}^{s} eventually renders Ψ0\Psi_{0} in terms of the power nn of the true relative density and the power NnN-n of the initial (referential) volume fraction

Ψ0=[ρ0ρ0s]n[ν0]NnΨ0s=[ν0]n[ν0]NnΨ0s.\Psi_{0}=\left[\frac{\rho_{0}}{\rho_{0}^{s}}\right]^{n}[\nu_{0}^{\star}]^{N-n}\,\Psi_{0}^{s}=[\nu_{0}]^{n}[\nu_{0}^{\star}]^{N-n}\,\Psi_{0}^{s}\>. (16)

The exponent nn is typically set to n=2n=2 for trabecular bone with low nominal density and to n>2n>2 for denser cancellous bone, compare to (Rho et al. 1993) and (Gibson 2005).

Setting finally the homogenisation exponent NN in particular to N=nN=n results in an expression for the (referential) volume-specific current nominal free energy density Ψ0\Psi_{0} in terms of its true counterpart and the true relative density

Ψ0=N=n[ρ0ρ0s]nΨ0s=[ν0]nΨ0s.\Psi_{0}\stackrel{{\scriptstyle N=n}}{{=}}\left[\frac{\rho_{0}}{\rho_{0}^{s}}\right]^{n}\Psi_{0}^{s}=[\nu_{0}]^{n}\Psi_{0}^{s}\>. (17)

Correspondingly, the Piola stress expands in this case as

𝐏=N=n[ρ0ρ0s]nΨ0s𝐅=:[ρ0ρ0s]n[λslnJ𝐅t+μs[𝐅𝐅t]].\mathbf{P}\stackrel{{\scriptstyle N=n}}{{=}}\left[\frac{\rho_{0}}{\rho_{0}^{s}}\right]^{n}\frac{\partial\Psi_{0}^{s}}{\partial\mathbf{F}}=:\left[\frac{\rho_{0}}{\rho_{0}^{s}}\right]^{n}\big{[}\lambda^{s}\ln J\,\mathbf{F}^{-t}+\mu^{s}[\mathbf{F}-\mathbf{F}^{-t}]\big{]}\>. (18)

Setting N=nN=n tacitly assumes that the geometry of the microstructure is not distorted by the deformation (for example a circular pore remains a circular pore). In contrast, setting NnN\not=n conceptually allows to distinguish between the initial and the (deformation-dependent) current microstructure, thus in general n=n(𝐅)n=n(\mathbf{F}) with N=n(𝐈)N=n(\mathbf{I}).

This contribution shall explore the consequences of two limiting cases by setting NN to either N=1N=1 (volumetric mixture rule) or to N=nN=n (cellular material like homogenisation rule). More sophisticated scenarios with n=n(𝐅)n=n(\mathbf{F}) where N=n(𝐈)N=n(\mathbf{I}) shall not be analysed here.

2.5 Mass density flux

To model changes in the nominal (referential) density ρ0\rho_{0} incurred by mechanical stimuli, the volume-localised mass balance ρ˙0=R0\dot{\rho}_{0}=R_{0} is equipped with a (referential) source term R0R_{0}. Following (Harrigan and Hamilton 1993), the (referential) mass source R0R_{0} is expressed by the (referential) volume-specific current nominal free energy density Ψ0\Psi_{0} and the nominal relative density as

R0=c[[ρ0ρ0]mΨ0Ψ0a].R_{0}=c\left[\left[\frac{\rho_{0}}{\rho_{0}^{\star}}\right]^{-m}\,\Psi_{0}-\Psi_{0}^{a}\right]\>. (19)

Here, the parameter cc controls the speed of density evolution and has dimension of time divided by length squared. The attractor stimulus Ψ0a\Psi_{0}^{a} defines the biological equilibrium (homeostasis) to which the system is driving at constant (mechanical) stimulus. The exponent mm is a material parameter particularising the mechanical stimulus (Harrigan and Hamilton 1993) in terms of the nominal relative density.

The (referential) mass source may alternatively be expressed by the (referential) volume-specific initial nominal free energy density Ψ0\Psi_{0}^{\star} or, likewise, by its true counterpart Ψ0s\Psi_{0}^{s} as

R0=c[[ρ0ρ0]nmΨ0Ψ0a]=c[[ρ0ρ0s]nm[ν0]Nn+mΨ0sΨ0a].R_{0}=c\left[\left[\frac{\rho_{0}}{\rho_{0}^{\star}}\right]^{n-m}\,\Psi_{0}^{\star}-\Psi_{0}^{a}\right]=c\left[\left[\frac{\rho_{0}}{\rho_{0}^{s}}\right]^{n-m}[\nu_{0}^{\star}]^{N-n+m}\,\Psi_{0}^{s}-\Psi_{0}^{a}\right]\>. (20)

We may deduce from this representation that the exponent mm is also crucial for the stability of the density evolution: at homeostasis (R0=0R_{0}=0) ρ0>ρ0\rho_{0}>\rho_{0}^{\star} for Ψ0>Ψ0a\Psi_{0}^{\star}>\Psi_{0}^{a} only if mn>0m-n>0. In conclusion, the exponent mm should be chosen as m>nm>n (Harrigan and Hamilton 1994), (Kuhl and Steinmann 2003).

Setting finally the homogenisation exponent NN in particular to N=nN=n results in alternative expressions for the (referential) mass source

R0=c[[ρ0ρ0s]nm[ν0]mΨ0sΨ0a]=c[[ρ0ρ0]nm[ν0]nΨ0sΨ0a].R_{0}=c\left[\left[\frac{\rho_{0}}{\rho_{0}^{s}}\right]^{n-m}[\nu_{0}^{\star}]^{m}\,\Psi_{0}^{s}-\Psi_{0}^{a}\right]=c\left[\left[\frac{\rho_{0}}{\rho_{0}^{\star}}\right]^{n-m}[\nu_{0}^{\star}]^{n}\,\Psi_{0}^{s}-\Psi_{0}^{a}\right]\>. (21)

3 Simulation and results

The performance of the proposed model options (N=nN=n versus N=1N=1) is demonstrated using classical benchmark problems. The first example considers a unit square specimen as defined by (Kuhl and Steinmann 2003) to study temporal bone density evolution at a single point. Second, we analyse the consequence of the spatial distribution of bone microstructure using a two-dimensional proximal femur head as given by (Carter and Beauprè 2010).

3.1 Investigating the influence of the initial volume fraction

To differentiate between cancellous and cortical bone tissue, the effect of the initial volume fraction shall be examined. For this purpose, a simple unit square sample is studied, which is loaded in tension by a force function that increases stepwise as illustrated in Figure 2.

Refer to caption
Figure 2: Unit square example: specimen and load function

The reference parameters are chosen similar to (Kuhl and Steinmann 2003): true elastic modulus Es=1.0E^{s}=1.0, Poisson’s ratio νs=0.0\nu^{s}=0.0, attractor stimulus Ψ0a=1.0\Psi_{0}^{a}=1.0, parameter m=3m=3 and parameter n=2n=2. The homogenisation exponent is chosen as N=nN=n as motivated by the proposal of (Gibson 2005).

A true density of the solid material ρ0s=2\rho_{0}^{s}=2, similar to (Gibson 2005), is assumed for both bone microstructure types in the following. It is known from measurements that the true density of trabeculae is slightly smaller and the one of cortical bone fibrils slightly larger, see (An and Draughn 2000). However, as the objective of this analysis is to point out the general trend in the evolution of the different tissue microstructures, the assumption of equal true density is sufficient in this context. An initial nominal density of ρ0=0.5\rho_{0}^{\star}=0.5 leading to an initial volume fraction of ν0=ρ0/ρ0s=0.5/2=0.25\nu_{0}^{\star}={\rho_{0}^{\star}}/{\rho_{0}^{s}}={0.5}/{2}=0.25 is chosen as representative of cancellous bone. A comparatively high value of ν0=ρ0/ρ0s=1.8/2=0.9\nu_{0}^{\star}={\rho_{0}^{\star}}/{\rho_{0}^{s}}={1.8}/{2}=0.9 is set for the volume fraction representing compact bone.

Refer to caption
Figure 3: Unit square example: evolution of relative change in nominal density and absolute nominal density with a variation in the initial volume fraction representing cortical and spongy bone

As shown in Figure 3, a small initial volume fraction (gray line) leads to rapid bone growth while a high value (black line) causes no density change in the first load step. Only after increasing the load in the second step, and thus increasing the mechanical stimulus, an adaptation of bone density can be observed.

Cortical bone in the model therefore requires a significantly higher stimulus and grows less in relative terms. But despite its rapid growth, the absolute density of cancellous bone still remains at a lower level.

3.2 Investigating the effect of exponent mm and the attractor stimulus

Due to its small surface area in relation to the volume, cortical bone adapts to the load conditions much slower and less than spongy bone. Considering the mass source term in Equation 19, it appears that there are three parameters which can influence the behaviour of bone adaptation. By reducing the parameter cc, the speed of density evolution can be slowed down, but after a sufficiently long time the result always converges towards the same saturation level. Therefore, a parameter adjustment of the exponent mm and the attractor stimulus Ψ0a\Psi_{0}^{a} shall be considered for cortical bone with ν0=0.9\nu_{0}^{\star}=0.9 and N=n=2N=n=2.

In order to satisfy the stability criterion, the exponent mm must be selected greater than nn, see (Harrigan and Hamilton 1993). Thus, m=3m=3, m=2.5m=2.5 and m=10m=10 are investigated as depicted in Figure 4.

Refer to caption
Figure 4: Unit square example: evolution of relative change in nominal density and absolute nominal density with variations of mm for cortical bone

As can be seen, reducing the exponent leads to an increase in density growth (dashed line). In contrast, choosing a large value for the exponent mm tends to slow down the density evolution (dotted line).

One possibility to simulate the significantly reduced density evolution of compact bone compared to spongy bone would therefore be setting a relatively high exponent mm.

A variation of the attractor stimulus is analysed in Figure 5.

Refer to caption
Figure 5: Unit square example: evolution of relative change in nominal density and absolute nominal density with variations of the attractor stimulus for cortical bone

The dotted line in Figure 5 based on a relatively high attractor stimulus displays low density results. Bone growth can not be achieved until the third load level. Reducing the attractor stimulus (dashed line) results in an overall increased gain in nominal density.

Since cortical bone should neither grow nor absorb faster than cancellous bone, in the following, the same attractor stimulus will be assumed for both microstructure types.

3.3 Investigating the interaction between cancellous and cortical bone

To analyse the local distribution of cortical and cancellous bone and their interaction, a two-dimensional proximal femur head is examined.

Three typical load cases representing the midstance phase of gait, extreme abduction and adduction are applied to the model as reported in (Carter and Beauprè 2010). In the calculations bi-linear element expansions with a 2x2 Gauss quadrature rule are used. The mesh, see Figure 6 (left), consists of 13317 elements and 13602 nodes. The parameters are set as follows: Poisson’s ratio νs=0.2\nu^{s}=0.2, attractor stimulus Ψ0a=0.01\Psi_{0}^{a}=0.01, exponent n=2n=2 and true solid material density ρ0s=2.0\rho_{0}^{s}=2.0.

An initial nominal cortical density of ρ0=1.825\rho_{0}^{\star}=1.825, leading to an initial volume fraction of ν0=ρ0/ρ0s=1.825/2=0.9125\nu_{0}^{\star}={\rho_{0}^{\star}}/{\rho_{0}^{s}}={1.825}/{2}=0.9125 is set for cortical bone (elements at the external boundary), and ρ0=0.55\rho_{0}^{\star}=0.55 with ν0=ρ0/ρ0s=0.55/2=0.275\nu_{0}^{\star}={\rho_{0}^{\star}}/{\rho_{0}^{s}}={0.55}/{2}=0.275 for cancellous bone. To avoid an abrupt unrealistic change between elements of different microstructure types, a small transition zone between both regions is created using a sigmoid function, see Figure 6 (middle).

Four different models are studied and compared in the following, all using the homogenisation exponent N=n=2N=n=2. Selected parameters and thus the difference between the four models are illustrated in Table 3.3.

\tbl

non-dimensionalised reference parameters of the four proxima femur models with N=n=2N=n=2 ν0{\nu_{0}^{\star}} of cancellous bone ν0{\nu_{0}^{\star}} of cortical bone mm of cancellous bone mm of cortical bone Model 1 0.275 3 Model 2 0.275 0.9125 3 3 Model 3 0.275 0.9125 3 10 Model 4 0.275 0.9125 3 18

The first model represents the full spongy bone as reported in previous literature with an initial nominal density of ρ0=0.55\rho_{0}^{\star}=0.55. The second model differentiates between cortical and cancellous bone using the initial volume fraction or rather the initial nominal density distribution as depicted in Figure 6 (middle).

Refer to caption
Figure 6: Femur example: mesh and the distribution of the initial nominal density and the nominal Young’s modulus

With a true elastic modulus of Es=10000E^{s}=10000, which is similarly documented for solid trabecular material by (Rho et al. 1993) and (Yamada et al. 2014), and based on the quadratic relation N=n=2N=n=2 between stiffness and nominal density according to (Gibson 2005), this results in a nominal stiffness of E=756.25E^{\star}=756.25 in the spongy region at an initial nominal density of ρ0=0.55\rho_{0}^{\star}=0.55, which roughly reflects the magnitude of stiffness as reported in (Wirtz et al. 2000) and which is also utilised in the full spongy model. The maximum nominal elastic modulus of cortical bone is approximately E=8327E^{\star}=8327 and thus significantly higher, see Figure 6 (right).

Motivated by the results of section 3.2, the third and fourth model include a variation of the exponent mm. While the exponent is always set to m=3m=3 in the first and second model, the others include an increase within the cortical bone area to a maximum of m=10m=10 in the third and m=18m=18 in the fourth model. The distribution of the exponent mm follows the respective volume fraction which indicates the type of bone microstructure. A slight transition is implemented between the two bone types using an hyperbolic tangent function, see Figure 7.

Refer to caption
Figure 7: Femur example: mesh zoom of femur head and distribution of exponent mm with m=10m=10 and m=18m=18 for cortical bone and m=3m=3 for cancellous bone

The results for the evolution of the nominal density are displayed for each model at different points in time in Figure 8.

Refer to caption
Figure 8: Femur example with N=n=2N=n=2: temporal evolution of absolute nominal density of the full spongy model (top row) and with the differentiation of cancellous and cortical bone (second row) and a variation in mm for cortical bone: m=10m=10 third row, m=18m=18 last row

Comparing the first two rows, it becomes clear that the pattern of density evolution has changed remarkably. The density growth in the femoral head and neck is significantly less intense when taking cortical bone into consideration. Density loss increases and slightly shifts in the intertrochanter region, which leads to an obvious change in density pattern. In areas with subliminal stress like the medial femur head, cortical bone decomposes slightly and at the same time ensures a less distinct density reduction in the adjacent spongy region.

Increasing the exponent mm in cortical bone (see row 3,4) suppresses its resorption and cortical bone remains, although weaker and thinner. Density loss of cancellous bone in the intertrochanter region is reduced and an increase in density in the femoral neck, albeit small, can be observed compared to the second model.

In summary, it appears that cortical bone acts as a kind of stiffer shell. Therefore, the interior of the femur head bears less load and cancellous bone does not adapt its density as much as in the first, full spongy model.

3.4 Investigating the impact of the homogenisation exponent N

Finally, the alternative volumetric mixture rule with N=1N=1 shall be examined. We first re-analyse the simple square example as described in section 3.1 with a variation in the initial volume fraction and homogenisation exponent N=1N=1, whereby all the other parameters remain unchanged. The temporal evolution of the nominal density is shown in Figure 9.

Refer to caption
Figure 9: Unit square example: evolution of relative change in nominal density and absolute nominal density with N=1 and a variation in the initial volume fraction representing cortical and spongy bone

Comparing the results of N=1N=1 with those of section 3.1 in Figure 3, it can be seen that density growth is reduced for an initial volume fraction of ν0=0.25\nu_{0}^{\star}=0.25 (gray lines), whereas a reduction in density growth for an initial volume fraction of ν0=0.9\nu_{0}^{\star}=0.9, which even leads to a small density loss in the first load step, is hardly visible (black lines).

The reason for this difference lies in the modified relationship between stiffness and nominal density from quadratic to linear. Whereas the initial nominal stiffness has quadrupled (1/0.251/0.25) at an initial volume fraction of ν0=0.25\nu_{0}^{\star}=0.25, the initial volume fraction of ν0=0.9\nu_{0}^{\star}=0.9 yields only a factor of 1.111=1/0.91.111=1/0.9.

Keeping this in mind, we again consider the proximal femur model, similar to section 3.3. Setting the true elastic modulus to Es=10000E^{s}=10000 yields an initial nominal stiffness of E=2750E^{\star}=2750 for spongy bone with ν0=0.275\nu_{0}^{\star}=0.275 via the linear relationship, which is far too high. Reducing the Young’s modulus of the solid material to Es=2750E^{s}=2750 results in the same EE^{\star} for cancellous bone as in section 3.3, see Figure 10. However, the stiffness for cortical bone becomes much too small.

Refer to caption
Figure 10: Femur example: distribution of nominal Young’s modulus with exponent N=1N=1 and Es=2750E^{s}=2750 (left) versus N=n=2N=n=2 and Es=10000E^{s}=10000 (right)

Nevertheless, Figure 11 shows the results of the four different models including the full spongy model, the distinction between cancellous and cortical bone with m=3m=3, and two variations of the exponent mm for cortical bone, all calculated with a true elastic modulus of Es=2750E^{s}=2750 and an homogenisation exponent of N=1N=1. Since the true Young’s modulus has been properly adjusted and thus the nominal stiffness as well as all the other parameters in the full spongy model correspond to those of section 3.3, the result is the same as can be seen in the first rows of Figure 11 and 8.

When comparing the different homogenisation exponents for the second model, we note the significantly higher density growth in the area of the femoral neck, but also an increased bone loss in the area of the medial femoral head. Furthermore, the pattern of density evolution more closely resembles that of the full spongy model, especially in the area of the greater trochanter. This effect is enhanced when increasing the exponent mm for cortical bone, see Figure 11 row 3 and 4. In this scenario, cortical bone decomposes much more in subliminally loaded regions with N=1N=1, especially with a small exponent mm.

Refer to caption
Figure 11: Femur example with N=1N=1: temporal evolution of absolute nominal density without (top row) and with cortical bone and a variation in mm for cortical bone: m=3m=3 second row, m=10m=10 third row, m=18m=18 last row

Overall, the application of the volumetric mixture rule with a homogenisation exponent of N=1N=1 leads to a nominal density distribution that is more similar to the full-spongy model. However, ensuring a stiffness-density ratio for cancellous bone as motivated by literature will not simultaneously achieve a realistic ratio in the cortical area. A further possible option would therefore be a separate definition of an individual true Young’s modulus for cortical bone, but will not be examined in this survey.

4 Discussion and conclusion

In this study the classical open-system model for bone remodelling by (Kuhl and Steinmann 2003) is modified to account for the initial nominal density distribution especially at the end of long bones, where two microstructure types, the spongiosa and the compacta can be found. A distinction is made between the two bone microstructure types by means of the initial volume fraction under the precondition that the same true bone material is assumed for both types. The model was applied to a one-dimensional benchmark problem and the two-dimensional proximal femur head, which is a representative biomechanical problem. We demonstrated that the additional modelling of cortical bone influences the density evolution of cancellous bone and should therefore be considered in future patient-specific simulations.

It should be emphasised that this is a first approach to take the local initial density distribution, the remodelling of cancellous and cortical bone and their interaction into account. Still, realistic material parameters have to be defined via analyses of clinical data, as well as more exact modelling of the boundary conditions and the influence of muscles tendons and ligaments in everyday and extreme loading scenarios.

Disclosure statement

None of the authors has a financial or personal relationship with other people or organizations that could inappropriately bias his/her work.

References

  • An and Draughn (2000) An YH, Draughn RA. 2000. Mechanical testing of bone and the bone-implant interface. CRC.
  • Barkaoui et al. (2019) Barkaoui A, Kahla RB, Merzouki T, Hambli R. 2019. Numerical simulation of apparent density evolution of trabecular bone under fatigue loading: effect of bone initial properties. Journal of Mechanics in Medicine and Biology. 19:1950041.
  • Carter and Beauprè (2010) Carter DR, Beauprè GS. 2010. Skeletal function and form. Cambridge University Press.
  • Cowin and Hegedus (1976) Cowin SC, Hegedus DH. 1976. Bone remodeling i: theory of adaptive elasticity. Journal of Elasticity. 6:313–326.
  • Frost (1987) Frost HM. 1987. Bone mass and the mechanostat: a proposal. The Anatomical record. 219:1–9.
  • Gibson (2005) Gibson LJ. 2005. Biomechanics of cellular solids. Journal of Biomechanics. 38:377–399.
  • Hambli (2014) Hambli R. 2014. Connecting mechanics and bone cell activities in the bone remodeling process: An integrated finite element modeling. Frontiers in Bioengineering and Biotechnology. 2.
  • Harrigan and Hamilton (1993) Harrigan TP, Hamilton JJ. 1993. Finite element simulation of adaptive bone remodelling: A stability criterion and a time stepping method. International Journal for Numerical Methods in Engineering. 36:837–854.
  • Harrigan and Hamilton (1994) Harrigan TP, Hamilton JJ. 1994. Necessary and sufficient conditions for global stability and uniqueness in finite element simulations of adaptive bone remodeling. International Journal of Solids and Structures. 31:97–107.
  • Holzapfel (2001) Holzapfel GA. 2001. Nonlinear solid mechanics - a continuum approach for engineering. West Sussex, England: John Wiley and Sons.
  • Huiskes et al. (1987) Huiskes R, Weinans H, Grootenboer HJ, Dalstra M, Fudala B, Slooff TJ. 1987. Adaptive bone-remodeling theory applied to prosthetic-design analysis. Journal of Biomechanics. 20:1135–1150.
  • Jacobs et al. (1995) Jacobs CE, Levenston ME, Beauprè GS, Simo JC, Carter DR. 1995. Numerical instabilities in bone remodeling simulations: The advantages of a node-based finite element approach. J Biomechanics. 28/4:449–459.
  • Kuhl and Steinmann (2003) Kuhl E, Steinmann P. 2003. Theory and numerics of geometrically non-linear open system mechanics. Int J Numer Meth Engng. 58(11):1593–1615.
  • Liedtke et al. (2017) Liedtke H, McBride A, Sivarasu S, Roche S. 2017. Computational simulation of bone remodelling post reverse total shoulder arthroplasty. arXiv preprint arXiv:170508324.
  • Nutu (2018) Nutu E. 2018. Role of initial density distribution in simulations of bone remodeling around dental implants. Acta of bioengineering and biomechanics. 20:23–31.
  • Papastavrou et al. (2020a) Papastavrou A, Schmidt I, Deng K, Steinmann P. 2020a. On age-dependent bone remodeling. Journal of Biomechanics. 103:109701.
  • Papastavrou et al. (2020b) Papastavrou A, Schmidt I, Steinmann P. 2020b. On biological availability dependent bone remodeling. Computer methods in biomechanics and biomedical engineering. 23:432–444.
  • Rho et al. (1993) Rho JY, Ashman RB, Turner CH. 1993. Young’s modulus of trabecular and cortical bone material: Ultrasonic and microtensile measurements. Journal of Biomechanics. 26:111–119.
  • Weinans et al. (1992) Weinans H, Huiskers R, Grootenboer HJ. 1992. The behavior of adaptive bone-remodeling simulation models. J Biomechanics. 25:1425–1441.
  • Wirtz et al. (2000) Wirtz DC, Schiffers N, Pandorf T, Radermacher K, DieternWeichert, Forst R. 2000. Critical evaluation of known bone material properties to realize anisotropic fe-simulation of the proximal femur. Journal of Biomechanics. 33:1325–1330.
  • Wolff (1892) Wolff J. 1892. Das gesetz der knochentransformation. Berlin: Hirschwald.
  • Yamada et al. (2014) Yamada S, Tadano S, Fukuda S. 2014. Nanostructure and elastic modulus of single trabecula in bovine cancellous bone. Journal of Biomechanics. 47:3482–3487.