Journal of Applied Mathematics and Physics, 2014, 2, 411-417
Published Online May 2014 in SciRes. http://www.scirp.org/journal/jamp
How to cite this paper: Xu, R., Hou, J.L., Wang, L., Yu, Y.F., Wei, J.X. and Li, C.F. (2014) Fluid Flow and Heat Transfer Chara-
teristics in a 180-deg Round Turned Channel with a Perforated Divider. Journal of Applied Mathematics and Physics, 2,
Fluid Flow and Heat Transfer Charateristics
in a 180-deg Round Turned Channel with a
Rui Xu, Jinliang Hou, Li Wang, Yanfei Yu, Jiaxing Wei, Changfeng Li*
School of Energy and Power Engineering, Jiangsu University, Zhenjiang, China
Email: *cfli@ujs. edu.cn
Received March 2014
This study provided a new configuration of the 180-deg round turned channel with a perforated
divider, as well as numerically investigated the effect of perforations, including the diameter of
perforation and the angel of perforation, on the fluid flow and heat transfer. The numerical results
appeared in good agreement with previous experimental data under the same operating condi-
tions. The results indicated that large size and positive angle of perforation changed the fluid flow
pattern and the local Nusselt-number distribution fundamentally. It is noteworthy that a more
uniform distribution of Nusselt-number was achieved by increasing the diameter of perforation.
180-deg Turned Channel, Perforated Divider, Heat Transfer, Computational Fluid Dynamic
To improve the thermal efficiency, gas-turbine blades are being designed to operate at increasingly higher
working temperatures. Without cooling design, overly high temperature will lead to the deformation, inaccuracy,
and even damage of the power machine. Leading coolant into the internal passages of the blade is widely used in
the power machine design. Jeng et al. - proposed the configuration of intermediate divider with multiple
perforations in the 180-deg turned channel. The coolant in the first duct entered the second duct ahead of time
through perforations due to the bypass effect, so that the temperatures of upstream and downstream hot wall
surfaces were relatively consistent, to avoid local high temperature at the wall surface of downstream channel.
In addition, the perforations had additional perturbation effect on the air flow, the bypass air flew through the
perforations mix with the main flow, that may improve the overall heat transfer capacity. Flow visualization
technique and steady state heat transfer experimentation were used to investigate the fluid flow and heat transfer
characteristics of 180-deg round turned channel with perforated divider . The experimental results indicated
that large size and positive angle of perforations influenced local Nusselt number distribution significantly, and
the overall heat transfer declined as the perforation size increased, especially when the perforation was at posi-
tive angle. However, when the perforation size was small, the overall heat transfer was higher than that without
R. Xu et al.
perforations by about 10%, and the influence of perforation angle was insignificant.
In addition to the experimental studies mentioned above, several studies have been made to numerically pre-
dict the flow and heat transfer in 180-deg turned channel. Iacovides et al. did a review of computer fluid dy-
namic applied to the internal gas-turbine cooling . Rigby et al.  use d the
turbulent model to simu-
late heat transfer and fluid flow phenomenon in a statio na r y straight duct with ribs no rmal to the mainstream
flow. Prakash and Zerkle  used high Reynolds
model to study three d imens ion fluid flow and heat
transfer between two ribs in a straight duct. Its Reynolds-number attained as high as 30,000 to 100,000 and the
wall functio n was adopted to figure out the near wall effects.
This study conduct numerical research based on RANS methods to investigate the flow and heat transfer of
the 180-deg round turned channel with perforated divider. The Realizable
turbulent model is adopted,
since it has a better performance than the standard
model when confronted complex flow condition, such
as secondary flow, flow sepa r atio n, jet impingement and so on. Numerical results provide more detailed fluid
flow structure and local Nusselt-number distribution than the former experimental data, which can be used for
industrial cooling design.
2. Numerical Analysis
The detailed size of this physical model is identical to that of former experiment . And the flow is governed
by Reynolds averaged Navier-Stokes (RANS) equations and the energy equation. In the Cartesian tensor system
these equations can be written as follows:
∂ ∂∂ ′′
is air velocity,
stands for dynamic visc osity, specific heat and coefficient of thermal
conductivity, respectively. T and P is the temperature and pressure. The Reynolds-averaged approach to turbu-
lence modeling requires that the Reynolds stresses,
in Equation (2) need to be modeled. The Boussi-
nesq hypothesis relates the Reynolds stresses to the mean velocity gradients as seen in the equation below:
where k is the turbulent kinetic energy, as defined by
is the Kronecker delta. The Realizable
model, which is an example of the two-equation models that use the Boussinesq hypothesis, was selected
for closure of the RANS equations. And the
transport equations are as follows:
() )] ()
whe r e,
R. Xu et al.
is not a constant, and its expression is much more complicated
which can be found in ref .
All the equations above were discretized by the Second Order Upwind numerical scheme, decoupling with the
SIMPLE algorithm and solved using a finite volume method (FVM) . The solutions were considered to be
converged when the normalized residual values were less than 10−5 for all variables but the energy equation,
which is set to 10−6.
The dimensionless parameters of interest in the present work are the Reynolds number, friction factor, local
and averaged Nusselt number, Colburn factor, which are defined by the following equations:
In this study, the commercial software FLUENT was adopted to execute the computing work. Enhanced wall
treatment in this software was selected to handle the near wall effects. The working fluid was air at ordinary
temperature and pressure (300 K, Pr = 0.707), whose physical properties being kept constant throughout the
whole computation. I mpermeable boundary and no-slip wall conditions have been implemented over the duct
walls as well as a uniform heat flux ranging from 3000 W/m2 to 20,000 W/m2 according to the flow inlet veloc-
ity. Pressure-outlet was selected for the outflow condition. Due to the employment of the enhanced wall treat-
ment, which contain a two-layer model to calculate the flow directly from the core turbulent region to the sub-
layer viscous region, the grid near the wall should be refined according to the various Reynolds numbers so as to
keep the first cell’s dimensionless wall distance
3. Results and Discussion
Figure 1 compares the averaged Nusselt number and local Nusselt number distribution of the present numerical
study with those of experimental data under the same operating conditions. It is found that the numerical result
have a good agreement with the experi mental data. As it shows in Figure 1( b) , the 180-deg turned channel can
be divided into three sections: the first duct, the turn region and the second duct.
Figure 1. Comparison with previous experimental results : (a) averaged Nusselt-number
as a function of Re; (b) local Nusselt-number distribution along the flow direction
R. Xu et al.
3.2. Flow St ru ct u re
Figure 2 dep icts the flow structure of the half-hei ght (z = 1/2 Dh) main stream plane and three different trans-
verse planes for the non-perforation system. The arrows, colored by temperature, indicate the flow direction. It
can be found that the near wall fluid have a higher te mperature. Figure 2(a) shows an obvious vortex above the
tip of the rectangular. Most of the air impinged on the outer wall, after that the cool air would flow near the out-
er zone due to the inertia. Figure 2(c) indicates a strong secondary flow in the middle of the turn region, which
contains a pair of counter rotating vortex near the top and bottom wall.
Figure 3 shows the flow structure for various perforation sizes and angles. When the perforation diameter is
Figure 2. Flow structure for the non-perforation configuration: (a) z = 10
mm; (b) x = 140 mm, y = 0 - 20 mm; (c) y = 30 mm; (d) x = 140 mm, y = 40 -
(a) (b) (c) (d)
Figure 3. Fluid flow structure for: (a) d/Dh = 1/4, θ = 0-deg; (b) d/Dh = 3/4, θ =0-deg; (c) d/Dh =
3/4, θ = +30-deg; (d) d/Dh = 1/4, θ = −30-deg.
R. Xu et al.
small (d = 5 mm), as it shows in Fig ur e 3(a), and only a small amount of air passed through the perforation.
Thus the effect of perforation on the fluid flow of the second duct was weak. However, when the perforation
diameter increased to 15 mm and the angle kept the same, it had more amount of bypass air flowing through
perforations into the second duct and a vortex existed in each perforation, as depicted in Figure 3(b) . When the
angle of perforation changed from 0-deg to +30-deg and the perforation diameter kept large, most of air would
flow through the first two perforations to the second duct, as it shows in Fig ur e 3(c). Besides, when the bypass
flow was adverse to the main flow in the second duct, a more chaos flow state appeared. It can be found in Fig-
ure 3(d) that only a small part of air flowed through perforations even though the perforation diameter was
3.3. Heat Transfer
Figure 4 shows the contours of wall surfaces Nusselt number of the non-perforation configuration. At the first
duct, the distribution of Nusselt number declined along the main flow direction due to the thermal developing
flow. In downstream of the turn region and upstream of the second duct, Nusselt numbers roused remarkably,
due to the secondary flow brought by the 180-deg bend.
Figure 5 displays the contours of wall surface Nusselt number for differ ent configurations at Re = 13,000.
The contours shows great differences from the non-perforation one when the size of the perforations was big. In
the case of small perforation diameter, as depicted by Figure 5(a), the contours of Nusselt number were gener-
ally the same as that of the non-perforation one. When the diameter increased to 15 mm, it is obvious from Fig-
ure 5(b) that the extreme high Nusselt number zones located on the bottom and outer wall disappeared. This
was resulted from the fact that bigger perforation size allowed more amounts of bypass flow as well as de-
creased the amount of corresponding main flow passing through the turn region. In the case of negative perfora-
tion angle, as it displays in Figure 5(c) , the Nusselt number contours of the bottom surface also keeps uniform.
Figure 6 represents ratio of Nu/Nu0 as a function of Re, where Nu0 stands for the averaged Nusselt number of
the non-perforation one. The results indicated that when the size of perforation was big and perforation angle
was non-negative, the averaged Nusselt numbers for the perforation ones were smaller than that of the non-per-
Fluid flow and heat transfer characteristics in a 180-deg round turned channel with perforated divider are nu-
merically investigated for Re = 1609 to 13,000. Three perforations of different sizes (d/Dh = 1/4 and 3/4) and
angles (θ = −30-deg, 0-deg and +30-deg) were located on the divider with equal interval. The numerical results
had a good agreement with previous experimental data under the same operating conditions. The results indi-
cated that the big size and positive angle of perforation influenced the flow behavior as well as the distribution
of local Nusselt number remarkably. Furthermore, the heat transfer results demonstrated that small size of per-
foration (d/D h = 1/4) led to slight improvement of the averaged Nusselt number and certain configuration (d/Dh
= 3/4, θ = 0-deg) would result in a more uniform distribution of local Nusselt number.
Figure 4 . Distribution of local Nusselt number (Nux) for the non-perforation configuration.
R. Xu et al.
Figure 5. Distribution of local Nusselt number (Nux) for: (a) d/Dh = 1/4, θ = 0-deg ; (b) d/Dh
= 3/4, θ = 0-deg ; (c) d/Dh = 1/4, θ = −30-deg.
Figure 6. Variation of Nu/Nu0 with Reynolds
The authors would like to thank the National Natural Science Foundation of China (11072091) and Key Sci-
Tech Project from Ministry of Education, China (210078) for financially supporting this research.
 Jeng, T.M. , Tzeng, S.C. and Yang, Y.C. (2011) Detailed Measurements of Heat Transfer Coefficients in a 180-Deg
Rectangular Turned Channel with the Perforation Divider. International Journal of Heat and Mass Transfer, 54,
R. Xu et al.
 Jeng, T. M., Tzeng, S.C. and Xu, R. (2013) Fluid Visualization and Heat-Transfer Tests in a 180-Deg Round Turned
Channel with the Perforated Divider. International Communications in Heat and Mass Transfer, 44, 45-51.
 Jeng, T. M., Tzeng, S.C., Chen, Y.C. and Chang, J.H. (2012) Thermal Behavior in a 180-Deg Turned Channel with the
Perforation Divider Under rotational Condition. International Communications in Heat and Mass Transfer, 39, 803-
 Iacovides , H. and Launder, B.E. (1995) Computational Fluid Dynamics Applied to Internal Gas-Turbine Cooling: A
Revie w. International Journal of Heat and Mass Transfer, 16, 454 -470.
 Rigb y, D.L., Steinthorsson, E. and Ameri, A.A. (1997) Numerical Prediction of Heat Transfer in a Channel With Ribs
and Bleed, 1997. ASME J. Turbomach., 97, 431-447 .
 Prakash , C. and Zerkle, R. (1995 ) Prediction of Turbulent Flow and Heat Transfer in a Ribbed Rectangular Duct With
and Without Rotation. ASME J. Turbomach., 177, 255-264. http://dx.doi.org/10.1115/1.2835654
 Shih, T.H. , Liou, W.W. and Shabbir, A. (1995) A New Eddy Viscosity Model for High Reynolds Number Turbulent
Fl ows. Computers Fluids, 24, 227-241. http://dx.doi.org/10.1016/0045-7930(94)00032-T
 Patankar, S.V. (1980 ) Numerical Heat Transfer and Fluid Flow. McGraw-Hill, New York.