Biomedical Engineering Reference
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Then we define the approximate solution as a couple U h D .v h ;p h / 2 W h Q h
such that v h satisfies approximately conditions ( 5.4 ), (a), (b), (c)(i) and the identity
a.U h ;U h ;V h / D f.V h /; for all V h D .' h ;q h / 2 X h Q h :
(5.20)
The couple .X h ;Q h / of the finite element spaces has to satisfy the Babuška-
Brezzi (BB) inf-sup condition (see, e.g., [ 35 , 36 ]or[ 99 ]), i.e., we assume that there
exists a constant LJ>0such that
.p; rv/
krvk L 2 ./ LJkpk L 2 ./ ;
sup
v 2 X h
8p 2 Q h :
(5.21)
In practical computations we assume that the domain is a polygonal approx-
imation of the region occupied by the fluid at time t n C 1 . The spaces W h ;X h ;Q h
are defined over a triangulation
T h of the domain , formed by a finite number of
closed triangles K 2 T h with the following properties:
(a) D S K 2 T h K,
(b) the intersection of two different elements K;K 0 2 T h is either empty or a
common edge or a common vertex of these elements,
(c) the vertices lying on @ belong to @ t n C 1 ,
(d) the end points of I ; O ,and Wt are vertices of some elements K 2 T h .
We shall denote by h K the length of the maximal side and we assume the index h
is chosen as h D max K 2 T h h K . The spaces W h ;X h ,andQ h are formed by piecewise
polynomial functions. In our computations, the well-known Taylor-Hood P 2 =P 1
conforming finite elements are used for the velocity/pressure approximation. This
means that p h is a linear function and v h is a quadratic vector-valued function on
each element K 2 T h , i.e., the spaces W h , X h ,andQ h are defined by
H h Df' 2 C./I 'j K 2 P 2 .K/ for each K 2 T h g;
W h D ŒH h 2 ;
X h D W h \ X;
(5.22)
Q h D ǚ ' 2 C./I 'j K 2 P 1 .K/ for each K 2 T h ;
where P k .K/ denotes the space of all polynomials on K of degree less or equal to
k.
The standard Galerkin discretization ( 5.20 ) may produce approximate solutions
suffering from spurious oscillations for high Reynolds numbers. In order to avoid
this drawback, the stabilization via streamline-diffusion/Petrov-Galerkintechnique
is applied (see, e.g., [ 34 , 53 ]). The stabilization terms are defined as
ı K 3
L h .U ;U;V/D X
K 2 T h
T v/ C .v z n C 1 / r v
2t v r.rv Cr
 
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