[tanate matum] identification of critical parameters of flows in multi-narrow gap coaxial short...
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7/26/2019 [Tanate Matum] Identification of Critical Parameters of Flows in Multi-Narrow Gap Coaxial Short Cylinder
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Identification of Critical Parameters of Flows in Multi-Narrow Gap
Coaxial Short Cylinder
1 1,*
1
The complex flows in Multi-Narrow Gap Coaxial Short Cylinder are the combination of Couetteflow in a four-couple coaxial short cylinders with different radius that comprise the axial bound influences
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10800
*: [email protected],: (662) 913-2500 8101, : (662) 586-9541
4
290 320
:, ,,, ,-, ,
Abstract
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along each set of cylinder. The first set of Multi-Narrow Gap Coaxial Short Cylinder turns with constantangular velocity while the second set is kept unmoving. The characteristics of this flow are the instabilityof flow pattern which occur when the angular velocity of the first set of Multi -Narrow Gap Coaxial Short
Cylinder reaches some critical values. This research studies the critical angular velocity takes place fromthe evolution of the laminar regime to the transition and from the transition regime to the turbulenceregime. With the help of finite volume method, the system of continuity and momentum equation is solvedand the flow behavior based on the turbulence model, Large Eddy Simulation, in Computational FluidDynamic commercial software is visualized through the numerical simulation.Purposely, this research canbe identified the subcritical angular velocity and the supercritical angular velocity which are equal to 290rpm and 320 rpm, respectively. In addition, the flow also changes from Couette flow to Taylor vorticesand from Taylor vortices to wavy vortices when the angular velocities reach the critical values.
Keywords:Coaxial Cylinder, Critical Velocity, Instability,LES,CFD, Couette flow, Taylor vortices flow,wavy vortices flow
1.
3 3
" "
( )
Maurice Marie
Alfred Couette
-
Sir GeoffreyIngram Taylor
" (Taylor vortices)" "
http://en.wikipedia.org/w/index.php?title=Maurice_Marie_Alfred_Couette&redirect=nohttp://en.wikipedia.org/w/index.php?title=Maurice_Marie_Alfred_Couette&redirect=nohttp://en.wikipedia.org/w/index.php?title=Maurice_Marie_Alfred_Couette&redirect=nohttp://en.wikipedia.org/w/index.php?title=Maurice_Marie_Alfred_Couette&redirect=nohttp://en.wikipedia.org/w/index.php?title=Maurice_Marie_Alfred_Couette&redirect=nohttp://en.wikipedia.org/w/index.php?title=Maurice_Marie_Alfred_Couette&redirect=nohttp://en.wikipedia.org/w/index.php?title=Maurice_Marie_Alfred_Couette&redirect=nohttp://en.wikipedia.org/w/index.php?title=Maurice_Marie_Alfred_Couette&redirect=no -
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(subcritical velocity)"
"(Wavy vortices)"
S.T.Wereley[2,3] particle image velocimetry(PIV)
P.S.Marcus[4] shiftt and reflect D. Pirr[5] (DNS)
O.Czarny [6,7] - J.Y.Hwang [8] Wereley and Lueptow
I. Raspo [9] L.A. Bordag [10] S.Kumar [11]
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U
m s P
m s U m s u m s 2m s k g m s 3kg m .rpm y
+
Py m
w 2
N m
2. 2.1
( , , )r z
1 2( , , )
r zU U U U
=
( 1)
( , , )r z
P P P P
=
(2)- 3 4
0U =
(3)21( )dU U U U U
dt
+ = +
(4)
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(Fluctuation) 5 6
U U u= +
(5)
P P p= +
(6)4 5 - 7 8
)( 0U u+ =
(7)
{ }2
)) )
) )
(( (
1( (
U uU u U u
U u U u
d
dt
+ + +
+ +
+
= +
(8)
y+ (wall boundedflow) y + 9 10
Py u y
+= (9)
wu
= (10)
2.2
1
3998.2 kg m =
0.001003 k g m s =
(RAM) (CPU)
1
45 r z 23,200 40 40 100 (Hexahedral) (Structure Grid) 2,320,000 2
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y + 1 1y + = 400
5
1.27 10 m
51.0 10 m 2 r z
3.
ANSYS 12.0 (Pressure basedsolver) - (Pressure-Velocity Coupling) PISO
2 r
(Discretization) PRESTO Bounded Central
Differencing Large Eddy Simulation (LES)
SGS Smagorinsky - Lilly 3
1
( )0,r z
U U U U r
= = = =
(8)
2
( )0r z
U U U U
= = = =
(9)
(No-slip condition)
3
( )0r zU U U U = = = =
(10)
4
1P atm=
(11)
5 Periodic
3
4.
(residuals) - 10 -3
r z
(transient) 4
90 r z
4
32
1
4
3
5
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-0.001, -0.002, -0.003, -0.004, -0.005 5
4 z 90
5 r 90
4.1 -
290 4 5
r z 6
6
- 2 4 7 8
1 3
6 r z 290
7 r z 290
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8
4.2
320 2 4 9
10 shift and reflect 11 4
1 3
5.
9 r z 320
10 r z 320
11
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90 290
290 320 320
6.
(.) (DMIE)
7.
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118
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