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  <front>
    <journal-meta />
    <article-meta>
      <title-group>
        <article-title>Numerical Solution of the Crack Problem by the Weighted FEM</article-title>
      </title-group>
      <contrib-group>
        <contrib contrib-type="author">
          <string-name>Viktor A. Rukavishnikov</string-name>
          <xref ref-type="aff" rid="aff0">0</xref>
          <xref ref-type="aff" rid="aff1">1</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Andrew O. Mosolapov</string-name>
          <email>msandrew84@gmail.com</email>
          <xref ref-type="aff" rid="aff0">0</xref>
          <xref ref-type="aff" rid="aff1">1</xref>
        </contrib>
        <aff id="aff0">
          <label>0</label>
          <institution>Computing Center of the Far Eastern Branch of the Russian Academy of Sciences</institution>
          ,
          <addr-line>Kim Yu Chen Str., 65</addr-line>
        </aff>
        <aff id="aff1">
          <label>1</label>
          <institution>Khabarovsk</institution>
          ,
          <addr-line>680000</addr-line>
          ,
          <country country="RU">Russia</country>
        </aff>
      </contrib-group>
      <pub-date>
        <year>2021</year>
      </pub-date>
      <fpage>14</fpage>
      <lpage>16</lpage>
      <abstract>
        <p>In present paper, crack problem in rectangle is considered. Solution of the problem is defined as R -generalized one in special weighted Sobolev set. For calculation of approximate solution, the scheme of the weighted finite element method (FEM) is constructed. Comparison of our method with the classic FEM on model problem is performed. We confirmed experimentally theoretical estimate O (h) of the rate of convergence for constructed method in the norm of the weighted Sobolev space and in weighted energy norm. Crack problem, R -generalized solution, angle singularity, weighted FEM VI International Conference Information Technologies and High-Performance Computing (ITHPC-2021), ORCID: 0000-0002-3702-1126 (Viktor A. Rukavishnikov); 0000-0003-0206-6938 (Andrew O. Mosolapov)</p>
      </abstract>
    </article-meta>
  </front>
  <body>
    <sec id="sec-1">
      <title>1. Introduction</title>
      <p>Two-dimensional Lame equations are usually used as a mathematical model for the crack problem.
This problem is one of so-called problems with singularity which arises from presence of reentrant
angle of 360 (crack) on the boundary. In this case, stresses in the around crack tip become
unbounded, and displacements belong to W 3/2− () , when the Dirichlet or Neumann conditions are
2
applied on both sides of crack, and W 5/4− () in case of conditions of different types,  is an
2
arbitrary small real number. As a result, classic FEM for this problem has convergence rate of only
O(h1/2 ) and O(h1/4 ) respectively in the norm of the spaceW21 () as well as in energy norm.</p>
      <p>
        In papers [1-5] for elliptic problems with singularity caused by degeneration of input data it was
suggested to define the solution as R -generalized one in weighted Sobolev spaces or sets, properties
of R -generalized solution and questions about its existence and uniqueness were deeply studied as
well as properties of weighted Sobolev spaces and sets. For calculation of approximate solution for
such problems, new numerical methods on the base of notion of R -generalized solution were created
and investigated [
        <xref ref-type="bibr" rid="ref1">6-8</xref>
        ]. In the sequel, idea of R -generalized solution was spread to other singular
boundary value problems in electrodynamics, hydrodynamics, theory of elasticity. New numerical
methods for these problems built on the notion of R -generalized solution showed high accuracy and
convergence rate of approximate solution to the exact one competing with known inflexible and more
complicated specialized single-purpose methods [
        <xref ref-type="bibr" rid="ref2 ref3 ref4 ref5 ref6">9-13</xref>
        ].
      </p>
      <p>
        For determination of approximate solution to the crack problem
with high accuracy and
convergence rate O (h) in the norm of the weighted Sobolev space and in weighted energy norm, in
[
        <xref ref-type="bibr" rid="ref7">14</xref>
        ] it was suggested to define solution as R -generalized one; on this base, the scheme of the
weighted FEM was developed and detailed numerical investigation of the model problem was
performed.
      </p>
      <p>2021 Copyright for this paper by its authors.</p>
      <p>In present work we state the crack problem, introduce the notion R -generalized solution, briefly
describe the weighted FEM and bring some numerical results for model problem concerning
experimental confirmation of the theoretical estimates of the convergence rate and absolute error in
the mesh nodes.
2. Problem statement. R -generalized solution</p>
      <p>In two-dimensional domain  with boundary  and crack  c   we consider boundary value
problem of elasticity stated in displacements u = (u1, u2 ) (crack problem):
−(2div( (u)) + ( div u)) = f  x  </p>
      <p>u = q x  .</p>
      <p>
        Let  ' be a closure of  -neighborhood of the point (0, 0) in  :  ' = {x   : x12 + x22  
In  ' we define weight function  ( x) as a distance to the point (0, 0) , and we extend  ( x) to the
rest of  as a constant  . Using weight function  ( x) , we introduce weighted spaces L2, () ,
0
W21, () and sets W21, (, ) , W 12, (, ) , W21,/2 (, ) (see [
        <xref ref-type="bibr" rid="ref7">14</xref>
        ]). Vector analogues for these spaces
and sets we designate with bold letters.
      </p>
      <p>Now we introduce bilinear and linear forms, respectively:
a(u v) =  2 (u) : ( 2 v) +  div u div( 2 v)dx,

l ( v) =   2 f  vdx.</p>
      <p>
We assume that for some real   0 the following inclusions are valid:</p>
      <p>f  L2, (, ), q  W21,/2 (, ).</p>
      <p>Vector-function u = (u ,1 , u ,2 )  W21, (, ) is called R -generalized solution to the problem
(1), (2), if almost everywhere on  boundary conditions (2) are met, and for any vector-function
0
v = (v1, v 2 ) from W 12, (, ) the following integral identity is valid:</p>
      <p>a(u , v) = l(v)
where    is fixed.</p>
      <p>
        Existence and uniqueness of R -generalized solution to the problem (1), (2) is stated in [
        <xref ref-type="bibr" rid="ref8">15</xref>
        ].
      </p>
      <p>Remark. In contrast to definition of weak solution, in the case of R -generalized one bilinear and
linear forms contains weight function in some non-negative power as a factor. This function subdues
singularity of the solution and provide integrals convergence. This allows us to construct numerical
method on meshes without refining toward singularity point with convergence rate O (h) of
approximate solution to the exact one in the norm of weighted Sobolev space and in the weighted
energy norm.
(1)
(2)
(3)</p>
    </sec>
    <sec id="sec-2">
      <title>3. Weighted finite element method</title>
      <p>
        Scheme of the weighted FEM is constructed in [
        <xref ref-type="bibr" rid="ref7">14</xref>
        ]. Here we briefly describe this scheme.
      </p>
      <p>Assume that  is a rectangle with a crack,  = (−0.7, 0.3)  [−1,1] \ [0, 0.3] {0} , c = [0, 0.3]  {0} .
In  we introduce quasiuniform mesh coordinated with crack and designate mesh parameter as h .
Mesh nodes are Pi , i = 1,..., N . For each of them we introduce weighted basis function of the form
 i =  * ( x) i ( x) , i = 1,..., N , where  *  R is a power of weight function,  i ( x) is standard linear
basis function of the FEM.
0</p>
      <p>We designate V h linear span of all basis functions, and V h is a linear span of only internal nodes
Pi , i = 1,..., n .</p>
      <p>We say that the function uh = (uh,1 , uh,2 ) , uh,i  V h , i = 1, 2 is an approximate R -generalized
solution to the problem (1), (2), if uh satisfy boundary conditions (2), and the integral identity
a(uh , vh ) = l(vh )</p>
      <p>0
holds for any vector-function v h = (v1h , vh2 ) , vih  V h , i = 1, 2 .
coefficients d i , i = 1,..., 2n :</p>
      <p>n n
uh,1 =  d 2i−1 i , uh,2 =  d 2i i .</p>
      <p>i=1 i=1
Coefficients d i , i = 1,..., 2n , we will find from the system of linear equations</p>
      <sec id="sec-2-1">
        <title>Components of approximate</title>
        <p>R -generalized solution we expand in basis with unknown
a(uh , ( i , 0)) = l ( i , 0),

a(uh , (0, i )) = l (0, i ), i = 1,..., n.</p>
        <p>Remark. In contrast to the classic FEM, in the weighted FEM basis functions contain weight
function in some power as a factor. This addition factor allows approximate solution to mimic
behavior of exact solution in the neighborhood of singularity point. As a result, we are able to affect
the accuracy of approximate solution. Selecting appropriate parameter  * , as well as  and  , we
can gain theoretical convergence rate O (h ) for approximate R -generalized solution to the exact one
and get absolute error in mesh nodes in 10–100 times less than in the case of approximate generalized
solution.</p>
      </sec>
    </sec>
    <sec id="sec-3">
      <title>4. Numerical analysis of the model problem</title>
      <p>In this section, we describe numerical experiment for model problem using the weighted FEM
presented in section 3. We compare derived approximate R -generalized solution and generalized one
with respect to convergence rate established in different weighted and non-weighted norms,
respectively, and absolute error in mesh nodes.
4.1.</p>
    </sec>
    <sec id="sec-4">
      <title>Model problem</title>
      <sec id="sec-4-1">
        <title>We consider model problem (1), (2) in domain  components of exact solution: described in section 3 with following</title>
        <p>u1 =
</p>
        <p>K I
2</p>
        <p>   
r cos   1 −
 2  </p>
        <p>
 + 
+ sin 2    </p>
        <p>  ,
 2  
u2 =  K 2I r sin  2  1 −  +  + sin 2  2   ,
where  is a polar angle, pole is located in the origin (0, 0) , and polar axis coincide with positive
direction of the O x axis. Lame parameters are  = 576.923 and  = 384.615 , stress intensity factor
K I = 1.611 .
4.2.</p>
      </sec>
    </sec>
    <sec id="sec-5">
      <title>Numerical experiment. Optimal parameters</title>
      <p>
        Numerical experiment was carried out on meshes described in section 3 with mesh parameter
h = 0.062 , 0.031 , 0.0155 , 0.0077 , 0.0038 , 0.0019 . Calculations were performed on each mesh
with different values of parameters  * ,  ,  . Among them, the optimal parameters providing the
best accuracy of approximate R -generalized in relative norm of the weighted Sobolev space and
weighted energy norm solution were found. More detailed description of this process can be found in
[
        <xref ref-type="bibr" rid="ref7">14</xref>
        ]. We also calculated approximate generalized solution using our weighted FEM with  = 0,
 * = 0,  ( x)  1 for comparison with approximate R -generalized one.
4.3.
      </p>
    </sec>
    <sec id="sec-6">
      <title>Convergence rate investigation</title>
      <p>In this section, we briefly describe results concerning convergence rate of approximate R

generalized solution founded on each mesh with appropriate optimal parameters and comparison with
convergence rate of approximate generalized solution. For approximate R -generalized solution,
convergence was calculated in relative norm  of the weighted Sobolev space and in relative
weighted energy norm E . For approximate generalized solution, convergence was calculated in
relative norm  of the Sobolev space and in relative energy norm  E . These results are visually
presented on figure 1a and 1b respectively. As we can see, appropriate parameters  * , as well as 
and  allowed approximate R -generalized solution to gain theoretical convergence rate O (h) ,
whereas approximate generalized solution converges with only O(h1/2 ) speed.</p>
      <p>a)
b)
represents  , red circled line represents E ) and for approximate generalized solution (1b, blue
squared line represents  , blue crossed line represents  E ). Solid black lines represent convergence
rate O (h) .
4.4.</p>
    </sec>
    <sec id="sec-7">
      <title>Absolute error investigation</title>
      <p>For approximate R -generalized solution and approximate generalized solution absolute error in
mesh nodes was also investigated. Here in Table 1 we present percentage of mesh nodes, where
absolute errors of first component of R -generalized and generalized solutions do not exceed limit
value 10 −7 .
generalized ( n1 ) solutions do not exceed limit value 10 −7</p>
      <p>h
n1 , %
n1 , %
4.5.</p>
    </sec>
    <sec id="sec-8">
      <title>Conclusions</title>
      <p>Numerical analysis of the model problem allowed us to conclude the following:
1. Introducing of R -generalized solution allowed us to subdue the influence of singularity
caused by the crack to the accuracy of approximate solution.
2. For parameters  * ,  and  there are optimal values producing an approximate R
generalized solution with best convergence rate and minimal absolute error.
3. Approximate R -generalized solution with optimal parameters  * ,  and  converges to the
exact one with the rate O (h) in norm of the weighted Sobolev space and weighted energy norm,
whereas approximate solution converges only with the rate O(h1/2 ) .
4. In majority of mesh nodes, approximate R -generalized solution has absolute error in 10-100
times less than approximate generalized solution.
5. Obtained results demonstrate advantages of weighted FEM over classic FEM which required
meshes with refining towards singularity point for achieving the same convergence rate. In
comparison with known specialized numerical methods for crack problem, weighted FEM is much
simpler and do not produce ill-conditioned systems of linear algebraic equations.</p>
    </sec>
    <sec id="sec-9">
      <title>5. Acknowledgements</title>
      <p>This work was supported by the Russian Science Foundation, grant no. 21-11-00039,
https://rscf.ru/en/project/21-11-00039/.</p>
      <p>The results were obtained using the equipment of Shared Resource Center "Far Eastern Computing
Resource" IACP FEB RAS (https://cc.dvo.ru) and Shared Services Center “Data Center of FEB RAS”
(Khabarovsk). Authors would like to thank students E.E. Potaenko and A.A. Guseinov for their
assistance in conducting of numerical experiments.
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