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<article xmlns:xlink="http://www.w3.org/1999/xlink">
  <front>
    <journal-meta />
    <article-meta>
      <title-group>
        <article-title>Computer investigation 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>
        </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>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Elena V. Matveeva</string-name>
          <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, Khabarovsk, 680000</addr-line>
          ,
          <country country="RU">Russia</country>
        </aff>
        <aff id="aff1">
          <label>1</label>
          <institution>Far Eastern State Transport University</institution>
          ,
          <addr-line>Serysheva Str., 47, Khabarovsk, 680021</addr-line>
          ,
          <country country="RU">Russia</country>
        </aff>
      </contrib-group>
      <abstract>
        <p>In present paper we consider crack problem in rectangle. Solution of the problem we define as   -generalized one in the weighted Sobolev set. For calculation of approximate solution we construct the scheme of the weighted finite element method (FEM). We perform comparison of our method with the classic FEM on two model problems. Theoretical estimate of the convergence rate  (ℎ) for constructed method in the norm of the Sobolev weight space is confirmed experimentally.</p>
      </abstract>
      <kwd-group>
        <kwd>eol&gt;crack problem</kwd>
        <kwd>angle singularity</kwd>
        <kwd>-generalized solution</kwd>
        <kwd>weighted finite element method</kwd>
      </kwd-group>
    </article-meta>
  </front>
  <body>
    <sec id="sec-1">
      <title>1. Introduction</title>
      <p>generalized solution.
natural. It is not required to refine mesh or preliminary separate singularity as multiplicative term.</p>
      <p>In the present paper for the crack problem a notion of   -generalized solution in special weighted
set is introduced. Such definition of the solution allowed us to construct the weighted FEM with a
convergence rate  (ℎ) in the norm of the weighted Sobolev space. A comparison of the constructed
method with the classic FEM is carried out. Theoretical estimation of the convergence rate for the
constructed method derived in [14] is confirmed in numerical experiment for two model problems. It is
twice as much than for the classic FEM. At the same time, in the most of mesh nodes the absolute error
for the approximate   -generilized solution in a several decimal orders less than for the approximate
2. Weighted spaces and sets.</p>
      <p>-generalized solution
following boundary value problem of elasticity stated in displacements (crack problem):
 Ω
Let Ω = (−0.7, 0.3) × [−1, 1] ⧵ [0, 0.3] × {0} be a two-dimensional domain with a crack  Ω = [0, 0.3] × {0},
+ and  Ω</p>
      <p>Assume that the domain Ω is a homogeneous isotropic body and strains are small. Consider the
− are the crack sides, point (0, 0) is a crack tip. Denote  Ω the boundary of Ω  Ω ⊂  Ω
,
.
− (2 
( ( )) +</p>
      <p>
        ( div  )) =  ,  ∈ Ω,
  =   ,  = 1, 2,  ∈  Ω.
(
        <xref ref-type="bibr" rid="ref1">1</xref>
        )
(
        <xref ref-type="bibr" rid="ref2">2</xref>
        )
Here  = ( 1,  2) is a displacement field,  ( ) is a strain tensor,  = ( 1,  2) is a distributed body force,
√
  ,  = 1, 2 are components of a surface force vector,  and  are Lamé parameters.
      </p>
      <p>Denote by Ω′ closure of the  -neighborhood of the point (0, 0) in the domain Ω
( 12 +  22) ≤  }. In Ω</p>
      <p>′ we introduce a weight function  ( ) as a distance to the point (0, 0)
it to the rest of Ω with constant  . Using  ( ), we introduce weighted space  2, (Ω) consisting of
: Ω′ = { ∈ Ω ∶
and extend
Lebesque measurable functions  with finite norm
‖ ‖ 2, (Ω) =
  ,
2
 ∈  ,  ≥ 0. Through
 21, (Ω,  ) we denote the set of functions  that meet the following conditions:</p>
      <p>− ,  ∈ Ω′,
(a)  ≤  1
(b) || 
|
| ≤  1
  |
(c) |‖ ‖ 2, (Ω⧵Ω′) ≥  2,  2 = const,</p>
      <p>+1 − −1,  ∈ Ω′,  = 1, 2,  1 = const,
with finite norm
‖ ‖ 21, (Ω) = ‖ ‖22, (Ω) + ‖‖
(
‖  ‖
‖ 
‖
‖
2
1 ‖ 2, (Ω)
+ ‖‖
‖ 
‖  ‖
2 ‖ 2, (Ω))
For the vector function  = ( 1,  2) corresponding norm is calculated by formula
‖
‖
2
2
√
∫  2</p>
      <p>The set consisting of traces of functions  ∈  21, (Ω,  ) on  Ω we denote by  21,/2( Ω,  ):
Norm in this set is defined by formula</p>
      <p>2
‖ ‖ 21, (Ω) = (‖ 1‖ 21, (Ω) + ‖ 2‖ 21, (Ω))
 21,/2( Ω,  ) = { ∶  =  | Ω,  ∈  21, (Ω,  )}.</p>
      <p>‖ ‖ 21,/2( Ω, ) = inf ‖ ‖ 21, (Ω).</p>
      <p>
        | Ω=
equations (
        <xref ref-type="bibr" rid="ref1">1</xref>
        ) and boundary conditions (
        <xref ref-type="bibr" rid="ref2">2</xref>
        ) are satisfied:
      </p>
      <p>The subset of set 
21, (Ω,  ) that contains functions with zero trace on  Ω we denote by  ̊ 1
2, (Ω,  ).</p>
      <p>The set of functions  ∈  2, (Ω) satisfying conditions (a) and (c) we denote by  2, (Ω,  ).
We assume that for some real number  &gt;</p>
      <p>
        0 the following inequalities for the right hand sides of
  ∈  2, (Ω,  ),   ∈  21,/2( Ω,  ),  = 1, 2.
(
        <xref ref-type="bibr" rid="ref3">3</xref>
        )
We introduce bilinear and linear forms, respectively:
 ( ,  ) = ∫ 2 ( ) ∶  ( 2
= ( , 1,  , 2) with components  ,
∈ 
21, (Ω,  ),  = 1, 2, is called  
-generaliand for any vector-function  = ( 1,  2),   ∈  ̊ 21, (Ω,  ),  = 1, 2, the integral identity
zed solution of the problem (
        <xref ref-type="bibr" rid="ref1">1</xref>
        ), (
        <xref ref-type="bibr" rid="ref2">2</xref>
        ) if on  Ω boundary conditions (
        <xref ref-type="bibr" rid="ref2">2</xref>
        ) are satisfied almost everywhere,
 ( ,  ) =  ( )
holds for any fixed value of  ≥  .
3. The scheme of the weighted FEM
nodes we designate {  } =1
 , and {  }
      </p>
      <p>we designate ℎ and call mesh parameter.</p>
      <p>
        =
for the problem (
        <xref ref-type="bibr" rid="ref1">1</xref>
        ), (
        <xref ref-type="bibr" rid="ref2">2</xref>
        ).
      </p>
      <p>We construct the scheme of the weighted FEM for calculation of approximate   -generalized solution</p>
      <p>We perform quasiuniform triangulation  ℎ of the domain Ω coordinated with the crack  Ω . For
this, we decompose Ω into the set of rectangles by horizontal and vertical straight lines 
=   , 
  ∈ [−0.7, 0.3],  
∈ [−1, 1]. Each rectangle we divide into two triangles by diagonal.</p>
      <p>=   ,
Obtained
triangles 
we call finite elements and their vertices are nodes   ,  = 1, … ,  . The set of internal
is the set of boundary nodes. The longest side of all triangles
For each node   we introduce weighted basis function   ( ) = 
 ∗ ( )  ( ),  = 1, … ,  , ∗ ∈  ,

where   ( ) is a function linear on each finite element 
and
  ( ) is equal 1
in  
and equal 0 in all
other nodes. Linear span of all built basis function we designate  ℎ. Linear span of basis function
associated with internal nodes we designate  ̊ ℎ.</p>
      <p>
        Vector-function  ℎ = ( ℎ, 1,  ℎ, 2) with components  ,
ℎ
(
        <xref ref-type="bibr" rid="ref2">2</xref>
        ) on  Ω, and for any vector-function  ℎ = ( 1ℎ,  2ℎ),  ℎ ∈  ̊ ℎ,  = 1, 2, integral identity
generalized solution of the problem (
        <xref ref-type="bibr" rid="ref1">1</xref>
        ), (
        <xref ref-type="bibr" rid="ref2">2</xref>
        ) if its components  ℎ, ,  = 1, 2 satisfy boundary conditions
∈  ℎ,  = 1, 2, is called approximate  
 ( ℎ,  ℎ) =  ( ℎ)
holds.
      </p>
      <p>Components of approximate   -generalized solution we write in the form

 ( ℎ, (0,   )) =  (0,   ),  = 1, … , .</p>
      <p>Unknown coeficients   ,  = 1, … , 2 can be found from the system of linear algebraic equations
Remark. The diference of the weighted FEM is the weight function  ( ) raise to some power  ∗ in
the finite element basis. This allowed us to approximate behavior of the solution near the singularity
point better. Parameter  ∗ as well as radius  of the  -neighborhood in definition of the weight
function  ( ) and its power  in definition of the   -generalized solution are governing parameters
of the constructed weighted FEM. Varying these parameters, we are able to afect accuracy of the
approximate   -generalized solution. When we choose parameters close to the optimal ones, we get
the best accuracy and maximum convergence rate of the constructed FEM that corresponds to the
theoretical rate  (ℎ).
4. Computer investigation of the model problems
In present section we adduce computer investigation of two model problems using weighted FEM
constructed in section 3. The results were obtained using the equipment of Shared Resource Center
"Far Eastern Computing Resource" IACP FEB RAS (https://cc.dvo.ru) and of Shared Services Center
“Data Center of FEB RAS” (Khabarovsk). Computation of approximate   -generalized solution were
realized by the program "Proba-IV", automatic startup of calculation series and sequent analysis of
results were carried out by the software package [15].</p>
      <p>The common algorithm of investigation is the following:</p>
      <p>of sets of their fixed values.</p>
      <p>
        hands of equation and boundary conditions (
        <xref ref-type="bibr" rid="ref2">2</xref>
        ).
1. Selection of the exact solution  , substitution to the equation (
        <xref ref-type="bibr" rid="ref1">1</xref>
        ) and computation of the right
method. To do this, on each mesh we realized the following:
2. Calculation of approximate   -generalized solution by the weighted FEM on the series of meshes
with decreasing mesh parameter ℎ and with diferent values of governing parameters of the
a) Definition of ranges for governing parameters  ,  ,  ∗, their increasing steps and creation
c) Collection of the derived results.
      </p>
      <p>ated set of values of governing parameters  ,  ,  ∗.
b) Computation of the approximate   -generalized solution corresponding to the each
cred) Analysis of results and detection of the optimal parameters set that minimize the
computational error in the norm of the weighted space 
21, (Ω).
3. Experimental evaluation of the convergence rate of approximate   -generalized solution by the
weighted FEM calculated with optimal values of governing parameters  , , ∗ found in listbox


2d), comparison with the convergence rate of the approximate generalized solution derived by
4. Comparison of the absolute error in the mesh nodes of approximate   -generalized and
generthe classic FEM.</p>
      <p>alized solutions.
4.1. Model problems
Problem 1. For the problem 1 we choose the vector  with only singular components:
 
Dependence of relative error   for approximate   -generalized solution derived with indicated optimal
parameters  ,  ,  ∗, and of relative error  for approximate generalized solution on the mesh parameter ℎ, model</p>
      <p>Problem 2. For the problem 2 we choose the vector  with both singular and regular components:
 
√
 
√</p>
      <p>2</p>
      <p>Lamé parameters for both problems are  = 578.923,  = 384.615Pa, stress intensity factor   =
4.2. Investigation of the convergence rate
In the present subsection for two model problems we adduce results concerning convergence rate of
norm of the weighted space  21, (Ω) when parameter  =  = 2.2,  =  = 0.062 by formula
the approximate   -generalized solution calculated by the weighted FEM with optimal parameters.
For derived approximate   -generalized solutions  ℎ the error was calculated in the relative weighted
  =
 =
‖ −  ℎ‖</p>
      <p>21, (Ω)
‖ ‖ 21, (Ω)
‖ −  ℎ‖ 21(Ω)
‖  ‖ 21(Ω)
.
.
by formula</p>
      <p>For approximate generalized solutions  ℎ the error was calculated in the norm of the space  21(Ω)
solution, and  (ℎ) for approximate   -generalized one.</p>
      <p>On the Figure 1 we present graphs of   and  in the log scales.</p>
      <p>For the model problem 1 in Table 1 for meshes with diferent parameter ℎ we adduce values of   ,
corresponding optimal parameters  , ,  ∗, values of  and their ratios  for adjacent meshes.
Ad
duced results confirm theoretical estimations of convergence rate  (ℎ0.5) for approximate generalized
Results on the convergence rate for model problem 2 are presented in Table 2 and Figure 2.
.3
.1
.3e–1
.1e–1
.3e–2

h</p>
      <p>0.031
0.062
1.3
0.1
0.0155
0.046
1.2
0.1
0.0077
0.023
1.2
0.1</p>
      <p>0.0038
0.0116
1.6
0.2
line represents convergence rate  (ℎ).
 
Dependence of relative error   for approximate   -generalized solution derived with indicated optimal
parameters  ,  ,  ∗, and of relative error  for approximate generalized solution on the mesh parameter ℎ, model
0.0019
0.0058
1.6
0.2
0.062
0.062
2.0
0.1
line represents convergence rate  (ℎ).</p>
      <p>ℎ
 11,, %%</p>
      <p>ℎ
 2 ,, %%
 11,, %%</p>
      <p>ℎ
 2 ,, %%
 2
Values of  1 , 1 (in percents of total number of nodes) on meshes with diferent parameter ℎ, model problem 1.
Values of  2 , 2 (in percents of total number of nodes) on meshes with diferent parameter ℎ, model problem 1.
Values of  1 , 1 (in percents of total number of nodes) on meshes with diferent parameter ℎ, model problem 2.
Values of  2 , 2 (in percents of total number of nodes) on meshes with diferent parameter ℎ, model problem 2.
0.031
4.3. Investigation of absolute error in mesh nodes
In nodes   ,  = 1, … , 
on meshes with diferent parameter
ℎ for components of approximate  
, , ∗ and for components of
apgeneralized solution obtained with optimal values of parameters 


proximate generalized solutions we calculated the absolute diferences between them and components
in Table 4.</p>
      <p>|
|
of exact solution:  
= |  (  ) −  , (  )|</p>
      <p>ℎ
  of nodes where the absolute errors  
|,
|
 and | 
= ||  (  ) −  ℎ(  )||,  = 1, 2. We also counted the numbers   ,</p>
      <p>, respectively, are less than the limit value Δ = 5 ⋅ 10−8.</p>
      <p>For model problem 1, in Table 3 we adduce values of  1 ,  1
on meshes with diferent parameter ℎ
.</p>
      <p>Results for second component of approximate   -generalized and generalized solution are presented
|
On Figure 3 and Figure 4 for model problem 1 we depict distribution in the domain Ω of   1,   1 and
Values of  1 ,  1</p>
      <p>and  2 ,  2 for model problem 2 are presented in Table 5 and Table 6 respectively.
Distribution in the domain Ω of   1,   1 and   2,   2 for model problem 2 is fully similar to the model
ℎ = 0.0077
ℎ = 0.0077</p>
    </sec>
    <sec id="sec-2">
      <title>5. Conclusion</title>
      <p>Computer investigation of the crack problem realized by the weighted FEM allows us to draw
following conclusions:
• Theoretical convergence rate  (ℎ) of the approximate   -generalized solution by the weighted
FEM with optimal governing parameters to the exact one in the norm of the weighted space
 21, (Ω) were experimentally confirmed. This is twice as much than convergence rate of the
approximate generalized solution.
• In most mesh nodes, absolute error of approximate   -generalized solution by the weighted</p>
      <p>FEM in several decimal orders less than absolute error of approximate generalized solution.</p>
    </sec>
    <sec id="sec-3">
      <title>Acknowledgments</title>
      <p>The reported study was supported by RSF according to the research project No. 21-11-00039.
[11] V. A. Rukavishnikov, A. O. Mosolapov, E. I. Rukavishnikova, Weighted finite element method
for elasticity problem with a crack, Computers and Structures 243 (2021) 106400. doi:10.1016/
j.compstruc.2020.106400.
[12] V. A. Rukavishnikov, A. V. Rukavishnikov, New numerical method for the rotation form of the</p>
      <p>Oseen problem with corner singularity, Symmetry 11 (2019) 54. doi:10.3390/sym11010054.
[13] V. A. Rukavishnikov, O. P. Tkachenko, Dynamics of a fluid-filled curvilinear pipeline, Applied</p>
      <p>Mathematics and Mechanics 39 (2018) 905–922. doi:10.1007/s10483-018-2338-9.
[14] V. A. Rukavishnikov, Weighted FEM for two-dimensional elasticity problem with corner
singularity, Lecture Notes in Computational Science and Engineering 112 (2016) 411–419.
doi:10.1007/978-3-319-39929-4_39.
[15] V. A. Rukavishnikov, O. V. Maslov, A. O. Mosolapov, S. G. Nikolaev, Automated software
complex for determination of the optimal parameters set for the weighted finite element method on
computer clusters, Computational Nanotechnology (2015) 9–19.</p>
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