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Analytical and Numerical Evaluation of Steady Flow of Blood Through Artery.

N. Sedaghatizadeh1*, A. Barari2, Soheil Soleimani3, M. Mofidi4

1Department of Mechanical Engineering, Iran University of Science and Technology, Narmak, Tehran, Iran

2Department of Civil Engineering, Aalborg University, Sohngårdsholmsvej 57, 9000 Aalborg, Aalborg, Denmark

3Department of Mechanical engineering, Babol University of Technology, Babol, Iran

4Department of Civil Engineering, Sharif University of Technology, Tehran, Iran

*Corresponding Author:
N. Sedaghatizadeh
Department of Mechanical Engineering
Iran University of Science and Technology
Narmak, Tehran
Iran


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Abstract

Steady blood flow through a circular artery with rigid walls is studied by COSSERAT Continuum Mechanical Approach. To obtain the additional viscosities coefficients, feed forward multi-layer perceptron (MLP) type of artificial neural networks (ANN) and the results obtained in previous empirical works is used. The governing filed equations are derived and solution to the Hagen-Poiseuilli flow of a COSSERAT fluid in the artery is obtained analytically by Homotopy Perturbation Method (HPM) and numerically using finite difference method. Comparison of analytical results with numerical ones showed excellent agreement. . In addition microrotation and the velocity profile along the radius are obtained by using both numerical and analytical approaches.

Keywords

Blood flow; artery; Cosserat continuum; viscoelastic response; non-Newtonian

Introduction

Over 20 million people die every year due to blood related diseases [1]. Since the blood flow is an important subject in biomedical and medicine sciences, the behavior of blood in the artery is one of the most important problems in biomechanical engineering. Thus many studies have been performed analytically, numerically and experimentally to determine the blood behavior and its different properties [1-5]. The phenomena which are associated with flow of blood through arteries such as pulsatility of flow, non-Newtonian behaviour of blood as a fluid and flexibility of the arteries wall are very complicated; therefore, theoretical study of blood flow is a very difficult problem to attack. The nonlinear behavior of blood was unknown until the second half of the last century [6]. From the rheological point of view, blood is a water based solution which is the combination of organic and inorganic substances and a variety of suspended cells mainly red cells which strongly affects the dynamic of blood as flood so that blood can be characterized as a non- Newtonian fluid [7, 8].Fig. 1 shows the component of a blood sample [7]. Detailed information can be found in previous literatures [6-8].

Figure 1: Components of a blood sample

Experimental studies revealed that the blood viscosity decreased with an increase in shear rate and that blood has a small yield stress. Some constitutive models have been proposed for blood as a non-Newtonian fluid by several researchers. Casson proposed a model which is applied successfully for analysis of blood flow by Merrill and others later [8]. Biviscosity model is another model, which express that blood behaves as non-Newtonian fluid in small shear rates and Newtonian fluid in large shear rates. Nakamura and Sawada used this model successfully [9,10]. In the case of blood flow because of considerable mechanical properties which is emanate from its microstructure, the theory of simple materials cannot solve the problem, so a more sensitive continuum theory such as nonlocal, micropolar, multipolar, and gradient theories [5,11,12] with higher kinematic status will be applied more successfully. The idea of a material body endowed with both translational and rotational degrees of freedom stems from the seminal work of the Cosserat brothers (Cosserat and Cosserat) [13, 14]. In this continuum, the effect of couples and forces are considered independently from each other which later named micropolar continuum by Eringen [11]. Fluids of this continuum medium can support the couple stress, the body couple and nonsymmetric stress tensor and possess a rotation field, which is independent of the velocity field. The rotation field is no longer equal to the half of the curl of the velocity vector field. Because of the assumption of infinitesimal rotations, we can treat the rotation field as a vector field. The theory, thus, has two independent kinematic variables; the velocity vector V and the spin or microrotation vector ω .

Because of complex rheological behavior of blood flow and the fact that blood contains a variety of cells with a spinning movement that affects the blood flow velocity, we should applied Cosserat continuum model. This model can consider the effects of rotational movement and has the ability to describe the complex fluid flows such as non-Newtonian and turbulent fluid flow [11, 12, 15, and 16]. Recently

Sedaghatizadeh et. al [17] conducted a semi empirical semi numerical study on blood flow through an artery in Cosserat continuum, and revealed that the blood flow exhibits a parabolic trend. They also calculated the non- Newtonian factors exist in governing equations using PSO algorithm and find out that these factors are not constant during a cycle of a heart [17].

Equation of motion in Cosserat continuum

In Cosserat continuum both velocity and rotation vector field are considered at any material point. In order to develop the relation between current state of orthonormal directions attached to each material point and its initial state we have the following.

equation (1)

Where equationand equationare the Kronecker delta and permutation tensor, respectively. The associated Cosserat deformation tensor εij and torsion-curvature tensor kij are written as

equation(2)

equation (3)

where the comma denotes partial differentiation. It is obvious that in the absence of the rotation vector ω , the classical continuum mechanics is recovered

It is assumed that the transfer of interaction between two particles of the continuum through a surface element ni ds occurs by means of both a traction vector ti ds and a moment vector mi ds . Surface forces and couples are represented by the generally nonsymmetric force-stress and couple stress tensor tij and mij , respectively. The balance of linear momentum and angular momentum require that the following equations must be satisfied

equation (4)

equation (5)

Where ρ j,fi and li are the mass density, microinertia, body force per unit mass and body couple per unit mass, respectively, and D Dt denotes the material time derivative. Here we choose linear constitutive equations which describe our material behavior. It can be considered as generalization of Newtonian fluids in the classical Navier-Stockes theory, which are

equation (6)

equation (7)

Where π is the thermodynamic pressure. The linear constitutive equation for nonsymmetric stress tensor (i.e. Cauchy's stress tensor), contains an additional viscosity coefficient kv. The value of kv shows the influence of the microrotation field on the stress tensor. The linear constitutive equation for couple stress also contains three additional viscosity coefficients αv , βv and γv.

At this stage the above equations should be combined to obtain the governing field equations. The field equations for micropolar fluids in the vectorial form are given by conservation of mass (i.e. continuity equation)

equation (8)

Balance of liner momentum

equation (9)

And balance of angular momentum

equation (10)

Problem Definition

Fig. 2 shows a part of the femoral artery of a dog where the measurements were made previously at USC School of Medicine. The pressure drop through the artery is measured using two small branch arteries. To simplify the geometry the vessel (Fig. 2.a) assumed and kept to be relatively straight with mild taper (Fig. 2. b). The flow through a vessel is determined by pressure gradient, which is assumed to be constant in most of the problems with practical importance and the vessel is considered as a pipe with radius of R . The Oz axis overlaps the centerline of pipe. In this case the velocity components and the microrotation velocities become

equation (11)

equation (12)

Figure 2: a) X-ray tracing of portion of the femoral artery of a living dog. Ligated small branch arteries are marked port No. 1 and 2 [8], b) simplified model of artery.

From continuity when ρ = const [6], we have equation By neglecting the body forces and body couples, the equations of motion (i.e., Eqs. (9) and (10)) are reduced to the following form in cylindrical coordinate system.

equation(13)

equation (14)

The above two coupled partial differential equations should satisfy the following boundary and initial conditions

At equation(15)

At equation(16)

where equation is a dissipative boundary condition [11, 18] and 0 ≤n ≤1. This factor is small for a laminar flow and is increases as flow become turbulent.

Analysis of the Homotopy Perturbation Method

Homotopy Perturbation Method (HPM) [19-29] is based on the Homotopy which is an important part of the topology [30-31].

equation (17)

with the following boundary condition:

equation (18)

where A is a general differential operator, B a boundary operator, f (r) a known analytical function and Γ is the boundary of the domain Ω. A can be divided into two parts which are L and N, where L is linear and N is nonlinear. Eq. (17) can therefore be rewritten as follows:

equation (19)

Homotopy perturbation structure is shown as follows:

equation (20)

where,

equation (21)

In Eq. (21),p∈[0,1]is an embedding parameter and μ0 is the first approximation that satisfies the boundary condition. We can assume that the solution of Eq. (21) can be written as a power series in p, as following:

equation (22)

and the best approximation for solution is:

equation (23)

In order to solve Eq. (17) using HPM, we construct the following homotopy; we need an initially condition which is Eq. (18). After constructing the Homotopy Perturbation of Eqs. (13) and (14) and rearranging based on powers of p-terms, we can obtain:

equation (24)

equation (25)

equation (26)

So Vz and wq can be obtained as follows with four terms of approximation as

equation (27)

and

equation (28)

In the above solution, the viscosity coefficients of COSSERAT medium ( kv , αv , βvv) are unknown. Thus the feed forward multi-layer perceptron (MLP) type of artificial neural networks (ANN) can be employed to calculate these coefficients on the basis of experimental data. In this study, the flow field and the results of experiments done in Fachhochschule Frankfurt by Silber [30] on steady blood flow through a dog artery with the diameter of 12 mm, is considered to determine the viscosity coefficients.

Results and Discussion

In this study Homotopy Perturbation and Finite Difference Methods are implemented to study the steady blood flow through a circular artery. Results are compared in Figs. 6 and 7 for both normalized microrotation and velocity, respectively. As it is obvious analytic outcomes are in good agreement with numerical ones.

Numerical solutions of governing coupled Eqs. (13) and (14) with boundary conditions (15) and (16) are obtained by finite difference FORTRAN code. Successive under relaxation (SUR) method is implemented to solve linear algebraic equations and the value of 0.1 is taken for under-relaxation parameter. The governing equations are discretized by applying second-order accurate central difference schemes. Grid independency was verified on different node numbers from 51 to 201 and finally the number of grid points is taken as 101 along the radius of artery. The convergence criterion (maximum relative error in the values of the dependent variables between two successive iterations) was set at10-10.

To obtain the additional viscosities coefficients, feed forward multi-layer perceptron (MLP) type of artificial neural networks (ANN) and the result obtained in [30] is used in this work.

5.1. Modeling using MLP-type neural networks

An example of a MLP type of neural network with one input node, a single hidden layer with two neuron and one output neuron is shown in Fig.3. An additional input called bias with constant value of 1 is added to the previous input node which works as a shift operator. Each input node is related to each neuron in hidden layer by a connecting weight. The sum of the products of the weights and the inputs is calculated by each neuron in hidden layer and then treated by an activation function. The obtained result is then multiplied by the associated weight C3 and again the previous procedure will be repeated in the output neuron. In the present study hyperbolic tangent and linear functions are used as the activation functions in the hidden and output layers respectively.

Figure 3: Architecture of a network with one hidden layer containing two neurons and one neuron in the output layer

The final output of the current network is calculated as

equation(29)

where,

equation (30)

Once the number of layers and the number of neurons in each layer, have been selected, the network's weights must be adjusted to minimize the prediction error made by the network. This is the general role of the training algorithms. In this investigation Back-propagation (BP) method is applied to train the ANN which is the most widely used learning process in neural networks today.

Back-Propagation algorithm

Back-propagation was firstly proposed by Werbos [33] which is based on searching an error surface (error as a function of ANN weights) using the gradient descent algorithm for points with minimum error. Consider a network with one hidden layer and one output neuron as shown in Fig 4. When a set of input data (input vector) are propagated through the network, for the current set of weights there is an output Est . The training of perceptron is a supervised learning algorithm where weights are adjusted to minimize the absolute error between the estimated output Est of network and the desired output Des whenever the estimated output does not match the desired output. If the network error ( NE ) is defined as

Figure 4: A feed forward multi-layer perceptron type of neural network with one hidden layer.

Network Error = Est - Des = NE (31)

The training algorithm should adjust the weights to minimize NE2 . For this purpose an artificial neuron with its basic elements is considered as shown in Fig .5.

Figure 5: Basic elements of an artificial neuron

The neuron consists of three basic components; weights, a summing junction and an activation function. The outputs of n neurons NO1,..., NOn lead in neuron N as the inputs. If neuron N is in the hidden layer then this is the input vector of the network. These outputs are multiplied by the associated weights W1N ,..., WnN.The summing junction adds together all these products to provide the input IN for activation function of neuron N . Then IN passes through the activation function AF ( ) and gives the final output of neuron N , which is NON . To commence the calculations, consider neuron M and weight WMN which connects the two neurons. The equation for weight update is as follows:

equation (32)

where LR is the learning rate parameter and equationis error gradient with reference to the weight WMN. The chain rule gives

equation (33)

since the rest of the inputs to neuron N are independent of the weight WMN we have

equation(34)

Eqs. (32), (33) and (34) give

equation(35)

For the case N is an output neuron we have:

equation(36)

Substituting Eq. (36) into Eq. (35) gives

equation(37)

For hyperbolic tangent and linear activation functions AF'(IN ) and the final form of weight update rule can be written as follows:

equation (38)

equation (39)

When N is a hidden layer neuron

equation (40)

where the subscript on represents the output neuron. In Eq. (40) we have

equation (41)

equation

substituting Eq. (41) into Eq. (40) gives

equation (42)

In Eq. (42),equationis now written as a function ofequationwhich was calculated in Eq. (36). Hence the weight update rule for a hidden layer neuron takes the following form

equation (43)

The most common parameters for evaluation of a neural network’s performance are minimum total squared errors (or RMS error) and minimum total absolute error (or MAE error). MAE and RMS errors are defined as

equation (44)

equation (45)

where n is the number of training data. The number of hidden layers and the neurons in each of them should be determined in a way to minimum the above errors.

The velocity profile along the radius is shown in Fig. 6. The diagram shows that the velocity has a parabolic trend and change from maximum value at center to zero at the wall. Microrotation is illustrated in Fig. 7 and it shows that, it varies linearly along the radius.

Figure 6: Microrotation profile along the radius

Figure 7: Velocity profile along the radius

The maximum values of V and ω (Vmax, ωmax) can be obtained analytically by substituting r = 0 and r = R in Eqs.(27, 28) respectively as follows:

equation (29)

equation (30)

Conclusions

In this study a flow simulation respect to time and dimensionless radius based on Cosserat model for a complex fluid like blood has been performed. ANN is applied to obtain the non-Newtonian coefficients. Using these values, the velocity and rotation profiles are calculated over radius of the artery are obtained. The obtained results show that, the maximum values of velocity occur in the inlet core; while, the maximum values of rotation happen near and on the boundary during systoles and diastoles.

References