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Figure 4.25 Staggered grid in SIMPLE algorithm: (a) sketch of global grid, (b) control volume for u x ,
(c) control volume for u y , and (d) control volume for p .
a n u y , n =
a l u y , l +
p P
p N )
S v
+
A n
(
(4.174)
l
The approximate velocities u x and u y do not satisfy the continuity equation. Hence,
the pressure correction p and velocity corrections u x and u y are defined as
p =
p n + 1
p
(4.175)
u x =
u n + 1
x
u x ,
u y =
u n + 1
y
u y
(4.176)
Subtracting Eq. (4.173) from Eq. (4.171) and neglecting the term l a l u x , l yields
the u x -equation:
u x , e =
p P
p E )
d e
(
(4.177)
a e .
where d e
=
A e
/
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