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  <front>
    <journal-meta />
    <article-meta>
      <title-group>
        <article-title>Crank-Nicolson Scheme for Space Fractional Heat Conduction Equation with Mixed Boundary Condition</article-title>
      </title-group>
      <contrib-group>
        <aff id="aff0">
          <label>0</label>
          <institution>Rafał Brociek Institute of Mathematics Silesian University of Technology Kaszubska 23</institution>
          ,
          <addr-line>44-100 Gliwice</addr-line>
          ,
          <country country="PL">Poland</country>
        </aff>
      </contrib-group>
      <fpage>41</fpage>
      <lpage>45</lpage>
      <abstract>
        <p>-This paper presents Crank-Nicolson scheme for space fractional heat conduction equation, formulated with Riemann-Liouville fractional derivative. Dirichlet and Robin boundary condition will be considered. To illustrate the accuracy of described method some computational examples will be presented as well.</p>
      </abstract>
    </article-meta>
  </front>
  <body>
    <sec id="sec-1">
      <title>I. INTRODUCTION</title>
      <p>
        In recent years the applications of mathematical models
using the fractional order derivatives are very popular in
technical science. Different types of phenomena in physics,
biology, viscoelasticity, heat transfer, electrical engineering,
control theory, fluid and continuum mechanics can be modeled
by using the fractional order derivatives [
        <xref ref-type="bibr" rid="ref6">6</xref>
        ], [
        <xref ref-type="bibr" rid="ref21">23</xref>
        ], [
        <xref ref-type="bibr" rid="ref10">10</xref>
        ],
[
        <xref ref-type="bibr" rid="ref19">19</xref>
        ], [
        <xref ref-type="bibr" rid="ref28">33</xref>
        ]. For example in paper [20] mathematical models of
supercapacitors are considered. Authors investigated models
based on electrical circuits in the form of RC ladder networks.
These models are described using fractional order differential
equations. Often we are not able to solve these models in
an analytical way, so it is important to develop approximate
methods of solving differential equations of fractional order.
      </p>
      <p>
        Murio in paper [21] presents the implicit finite
difference approximation for the time fractional diffusion equations
with homogeneous Dirichlet boundary conditions, formulated
by Caputo derivative. In paper [
        <xref ref-type="bibr" rid="ref1">1</xref>
        ], implicit finite difference
method was used to solve time fractional heat conduction
equation with Neumann and Robin boundary conditions. In these
case also, the Caputo derivative was used. In paper [30] authors
describes approximated solution of the fractional equation with
      </p>
    </sec>
    <sec id="sec-2">
      <title>Dirichlet and Neumann boundary conditions.</title>
      <p>
        Paper [
        <xref ref-type="bibr" rid="ref7">7</xref>
        ] describes numerical method for diffusion
equation with Dirichlet boundary conditions. To discretization
fractional derivative authors used finite difference method
and Kansa method. Paper [
        <xref ref-type="bibr" rid="ref11">11</xref>
        ] presents numerical solution
of model describe by fractional differential equation with
space fractional derivative and Dirichlet boundary conditions.
Fractional derivative used in this model was Riemann-Liouville
derivative. Authors used finite volume method.
      </p>
      <p>
        Also Meerschaert and Tadjeran dealt with fractional
differential equations [
        <xref ref-type="bibr" rid="ref13">13</xref>
        ], [
        <xref ref-type="bibr" rid="ref12">12</xref>
        ], [
        <xref ref-type="bibr" rid="ref14">14</xref>
        ], [35]. Paper [35] describes
Copyright c 2016 held by the author.
numerical solution of space fractional diffusion equation with
boundary condition of the first kind, and in paper [
        <xref ref-type="bibr" rid="ref12">12</xref>
        ]
authors presents finite difference method for two-dimensional
fractional dispersion equation. In both papers, as the fractional
derivative, the Riemann-Liouville derivative was used.
      </p>
      <p>
        In this paper we present numerical solution of space
fractional heat conduction equation. To the equation the Dirichlet
and Robin boundary condition was added. In order to solve the
equation, the Crank-Nicolson scheme was used. To illustrate
the accuracy of described method some computational
examples will be presented as well. The aim to achieve numerical
solution of considered model is application it to solve inverse
problems. Numerical solution of described model is called
solution of direct problem. In the process of solving inverse
problem, it is required to solve the direct problem many times.
More about inverse problems of fractional order can be found
in papers [
        <xref ref-type="bibr" rid="ref2">2</xref>
        ], [
        <xref ref-type="bibr" rid="ref3">3</xref>
        ], [
        <xref ref-type="bibr" rid="ref23 ref4">4</xref>
        ], [
        <xref ref-type="bibr" rid="ref5">5</xref>
        ]. In these papers, swarm optimization
algorithms are introduced. More about intelligent algorithms
and its application can be found in [24], [25], [26], [27], [28].
      </p>
    </sec>
    <sec id="sec-3">
      <title>II. FORMULATION OF THE PROBLEM We discuss the following space fractional heat conduction equation</title>
      <p>c %
(1)
defined in area D = f(x; t) : x 2 [a; b]; t 2 [0; T )g, where
(x) is thermal conductivity coefficient, c and % denote the
specific heat and density. We assume that (x) &gt; 0 and 2
(1; 2]. The initial condition is also posed
u(x; 0) = f (x);
x 2 [a; b];
as well as the homogeneous Dirichlet and Robin boundary
conditions</p>
      <p>u(a; t) = q(t);
(x)
u1);
t 2 [0; T );
t 2 [0; T );
where h describes the heat transfer coefficient and u1 is the
ambient temperature.
(2)
(3)
(4)</p>
      <p>
        Fractional derivative with respect to space, which occurs in
equation (1), will be the Riemann-Liouville fractional
derivative [
        <xref ref-type="bibr" rid="ref21">23</xref>
        ], [
        <xref ref-type="bibr" rid="ref8">8</xref>
        ] determined as follows
=
(n
1
a
x
where 2 (n 1; n] and ( ) is the Gamma function [
        <xref ref-type="bibr" rid="ref29">34</xref>
        ]. In
case of 2 (1; 2), the equation (1) describes super-diffusive
process [
        <xref ref-type="bibr" rid="ref15">15</xref>
        ], [
        <xref ref-type="bibr" rid="ref16">16</xref>
        ], and for = 2, we get the classical heat
conduction equation.
      </p>
      <p>III.</p>
    </sec>
    <sec id="sec-4">
      <title>NUMERICAL SOLUTION</title>
      <p>In this section we describe numerical solution of equation
(1) using the finite difference method. Let N; M 2 N be
the size of grid in space and time, respectively. We denote
grid steps x = (bNa) and t = T =M . Therefore, we get
following grid</p>
      <p>S = (xi; tk); xi = i x; tk = k t; i = 0; 1; : : : ; N;
k = 0; 1; 2; : : : ; M :
We assume the following notation i = (xi); gik =
g(xi; tk); fi = f (xi); hk = h(tk). Values of approximate
function in points (xi; tk), we denoted by Uik.</p>
      <p>
        In order to approximate fractional derivative (5), we used
right-shifted Gru¨nwald formula [
        <xref ref-type="bibr" rid="ref17">17</xref>
        ]
=
(
1
      </p>
      <p>lim
) N!1 r
1 XN
j=0
(j )
(j + 1)
where N 2 N and r = x a</p>
      <p>N . We denote
! ;j =
(
(j )
) (j + 1)</p>
      <p>Discretize the equation (1) and using approximation of
fractional derivative, we get
U k+1
i
t</p>
      <p>U k
i =</p>
      <p>i
2c%( x)
i+1
X ! ;j Uik+j1+1 +
j=0
i+1
X ! ;j Uik j+1
j=0
gk+ 12
+ i
c%</p>
      <p>Now, we approximate boundary condition of the third kind,
so we obtain</p>
      <p>UNk =</p>
      <p>N UNk 1 +</p>
      <p>xhku1
N +
xhk
u(s; t)(x
ds; (5)
where</p>
      <p>Having regard to both boundary condition, the equation (9)
may be written in matrix form
(1 + x)x3e t;</p>
      <p>U k = [U1k; U2k; : : : ; UNk 1]T ;
Gk+ 12 t =
h g1k+ 12 t ; : : : ; gNk+ 122 t</p>
      <p>;
c%
c%</p>
      <p>N +
gNk+ 121 t
c%
+</p>
      <p>N 1 tu1
2( x)</p>
    </sec>
    <sec id="sec-5">
      <title>IN 1 is the identity matrix of size N A1 and A2 are defined as follows</title>
      <p>i = 1; 2; : : : ; N
1;
j = 1; 2; : : : ; N</p>
      <p>1;
xhk
xhk +</p>
      <p>xhk+1
N +
xhk+1
i
;</p>
      <p>Solving systems of equations defined by (11), we obtain
approximate values of temperatures in points of grid (6).</p>
      <p>In paper [35] authors presents proof of unconditionally
stability of presented method in case of homogeneous Dirichlet
boundary condition. Doing similar proof it can be proven that
described in this paper method is unconditionally stable.</p>
    </sec>
    <sec id="sec-6">
      <title>IV. EXPERIMENTAL RESULTS In this section we presents numerical examples of described method.</title>
    </sec>
    <sec id="sec-7">
      <title>Example 1: Let consider equation (1), defined in area</title>
      <p>D = f(x; t) : x 2 [0; 1]; t 2 [0; 1]g;
with following data
= 1:7;
(x) =
(2:2)x2:8;</p>
      <p>c = % = 1; u1 = 50;</p>
    </sec>
    <sec id="sec-8">
      <title>To equation we added an initial condition</title>
    </sec>
    <sec id="sec-9">
      <title>Exact solution of this problem is function</title>
      <p>u(x; 0) = x3;</p>
      <p>x 2 [0; 1]:
u(x; t) = x3e t:
Maximal and average absolute errors will be defined by
formulas
max = 0miaxN juik
1 k M</p>
      <sec id="sec-9-1">
        <title>Uikj;</title>
        <p>avg =
1
(N + 1)(M + 1)
N M
X X juik
i=0 k=0</p>
      </sec>
      <sec id="sec-9-2">
        <title>Uikj:</title>
        <p>With increase in the first dimension N of the grid, a
fixed second dimension M , errors decrease. For example, for
M = 100 and N = 100; 200; 300 absolute errors not exceed
6:17 10 3; 3:09 10 3; 2:06 10 3. Increasing the dimension
of the grid with respect to time for a fixed dimension N
insignificantly impact on errors of approximate solution.</p>
        <p>Distribution of errors in points of the grid is presented on
figure 1.</p>
        <p>Fig. 1. Distribution of errors (N = M = 100) (example 1)</p>
        <p>Grid N
10
10
20
50
100
100
100
200
300</p>
        <p>M
Fig. 4. Distribution of errors for approximate solution (a) and approximate
solution (points), exact solution (solid line) (b) in time t = 1 (N = M = 100)
(example 2)</p>
        <p>Just as it did in the previous examples, we will examine
the errors depending on the density of the grid. In table III
errors of approximate solutions are presented.</p>
      </sec>
    </sec>
    <sec id="sec-10">
      <title>CONCLUSION</title>
      <p>In this paper numerical solution of space heat conduction
equation is presented. To the equation Robin and Neumann
boundary conditions were added. Author used Crank-Nicolson
scheme, and right-shifted Gru¨ nwald formula for approximation
fractional Riemann-Liouville derivative. To illustrate the
accuracy of presented method three examples are presented. In each
example results are good. With an increase in the density of
the grid, errors of approximate solution decreases.</p>
    </sec>
  </body>
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