Simultaneous measurements of velocity and temperature fluctuations in thermal boundary layer in a drag-reducing surfactant solution flow |
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Authors: | F-C Li D-Z Wang Y Kawaguchi K Hishida |
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Institution: | (1) Center for Smart Control of Turbulence, Turbomachinery Research Group, Institute for Energy Utilization, National Institute of Advanced Industrial Science and Technology, 305-8564 Tsukuba, Japan;(2) School of Mechanical Engineering, Shanghai Jiao Tong University, 1954 Huashan Road, 200030 Shanghai, People s Republic of China;(3) Department of System Design Engineering, Keio University, 223-8522 Yokohama, Japan |
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Abstract: | The mechanism of turbulent heat transfer in the thermal boundary layer developing in the channel flow of a drag-reducing surfactant solution was studied experimentally. A two-component laser Doppler velocimetry and a fine-wire thermocouple probe were used to measure the velocity and temperature fluctuations simultaneously. Two layers of thermal field were found: a high heat resistance layer with a high temperature gradient, and a layer with a small or even zero temperature gradient. The peak value of
was larger for the flow with the drag-reducing additives than for the Newtonian flow, and the peak location was away from the wall. The profile of
was depressed in a similar manner to the depression of the profile of
in the flow of the surfactant solution, i.e., decorrelation between v and compared with decorrelation between u and v. The depression of the Reynolds shear stress resulted in drag reduction; similarly, it was conjectured that the heat transfer reduction is due to the decrease in the turbulent heat flux in the wall-normal direction for a flow with drag-reducing surfactant additives.List of symbols
ensemble averaged value
- (·)+
normalized by the inner wall variables
- (·)
root-mean-square value
-
C
concentration of cetyltrimethyl ammonium chloride (CTAC) solution
-
c
p
heat capacity
-
D
hydraulic diameter
-
f
friction factor
-
H
channel height
-
h
heat transfer coefficient
-
j
H
Colburn factor
-
l
length
-
Nu
Nusselt number, h
-
Pr
Prandtl number, ![equiv](/content/q3hhta83hh996yva/xxlarge8801.gif) ![ugr](/content/q3hhta83hh996yva/xxlarge965.gif) c
p/
-
q
w
wall heated flux
-
Re
Reynolds number, U
b/
-
T
temperature
-
T
b
bulk temperature
-
T
i
inlet temperature
-
T
w
wall temperature
-
T
friction temperature, q
w
/ c
p
u
-
U
local time-mean streamwise velocity
-
U
1
velocity signals from BSA1
-
U
2
velocity signals from BSA2
-
U
b
bulk velocity
-
u
streamwise velocity fluctuation
-
u1
velocity in abscissa direction in transformed coordinates
-
u
friction velocity,
-
v
wall-normal velocity fluctuation
-
v1
velocity in ordinate direction in transformed coordinates
- var(·)
variance
-
x
streamwise direction
-
y
wall-normal direction
-
z
spanwise direction
-
j
junction diameter of fine-wire TC
-
w
wire diameter of fine-wire TC
-
angle of principal axis of joint probability function p(u,v)
-
f
heat conduction of fluid
-
w
heat conduction of wire of fine-wire TC
-
kinematic viscosity
-
local time-mean temperature difference, T
w
–T
-
temperature fluctuation
-
standard deviation
-
density
-
w
wall shear stress |
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Keywords: | |
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