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Weld ResultsYan Zhan
SUNY Stony Brook
June 13rd, 2013
1
Outline
• Studied Parameters
• Results Analysis
– Contours Plots For the Weld Region
– Axial Velocity Profile at Different Locations Near theWeld
– Plots of Turbulent Kinetic Energy and MomentumThickness Near the Weld
– Line Plot Goes From Inlet To Outlet
2
Studied Parameters
Name (Unit) Equation
Wall Shear Stress (𝑘𝑔/(𝑚 ∙ 𝑠2) ) 𝜏𝑤 = 𝜇
𝜕𝑈
𝜕𝑦𝑦=0
Friction Velocity (𝑚/𝑠)
𝑢𝜏 = 𝜏 𝜌
Turbulent Kinetic Energy (𝑚2/𝑠2)
𝑘 =1
2( 𝑢′ 2 + 𝑣′ 2 + (𝑤′)2)
Turbulent Dissipation Rate (𝑚2/𝑠3) 𝜖 ≡
𝜇
𝜌
𝜕𝑢′𝑖𝜕𝑥𝑘
𝜕𝑢′𝑖𝜕𝑥𝑘
Turbulence Intensity (%) 𝐼 ≡
𝑢′
𝑈𝑚𝑒𝑎𝑛=
2𝑘/3
𝑈2 + 𝑉2 + 𝑊2
Momentum Thickness (𝑚) 𝛿𝜃 =
𝑈
𝑈𝑚𝑎𝑥
𝑎
0
1 −𝑈
𝑈𝑚𝑎𝑥𝑑𝑟
3
Weld Region
4
Flow Flow 5
Flow Flow
6
7
X=0.0429 X=0.0435
X=0.045 X=0.05
8
X=0.0385 X=0.039
X=0.04065 (weld center) X=0.0423
9
X=0.025
X=0.03
X=0.035
X=0.038
10
Planes in the Vicinity of the Weld
Upstream place X=0.0430405
Downstream place X=0.0380405
Z = 0 (α = 0°)
𝛼 ↑
11
Upstream place X=0.0430405
𝜶 = 𝟎°
12
Downstream place X= 0.0380405
𝜶 = 𝟎°
13
At the Exit
α = 0°
14
Momentum Thickness At the Vicinity of the Weld
90o
60o
30o
0o
330o
300o270o
210o
120o
150o
180o
240o
0
1
2
3
90o
60o
30o
0o
330o
300o270o
210o
120o
150o
180o
240o
0
1
2
3
Upstream Plot Downstream Plot
15
Exit Plot
90o
60o
30o
0o
330o
300o270o
210o
120o
150o
180o
240o
0
1
2
3
16
Lines Go From Inlet to Outlet
Bottom Line
Top Line
17
S
Wa
llS
he
ar
Str
ess
(kg
/m*s
)
0 5 10 150
0.5
1
1.5
2
top
bottom
S: distance to the pipe inlet along the center line 18
s ~ 13 at weld
S
fric
tio
nve
locity
(m/s
)
0 5 10 150
0.002
0.004
0.006
0.008
0.01
0.012
top
bottom
19
S
Tu
rbu
len
tK
ine
tic
En
erg
y(m
2/s
2)
0 5 10 15
0
1E-05
2E-05
3E-05
4E-05
top
bottom
20
S
Tu
rbu
len
tD
issip
atio
nR
ate
(m2/s
3)
0 5 10 15
0
2000
4000
6000
8000
10000
12000
14000
16000
top
bottom
21
S
Aix
alV
elo
city
(m/s
)
0 5 10 15 20
0
5E-07
1E-06
1.5E-06
2E-06
2.5E-06
top
bottom
22