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IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 1
COMPARISON OF CFD SIMULATION OF HOT AND COLD FLUID
MIXING IN T-PIPE BY PLACING NOZZLE AT DIFFERENT PLACES
K.Venkateswara Rao1
, V.V.RamaKrishna2
, V. Subrahmanyam3
1
M.Tech Scholar, Department of Mechanical Engineering, Kakinada Institute of Technology and Science, Divili,
Andhra Pradesh, India
2
Assistant Professor, Department of Mechanical Engineering, Kakinada Institute of Technology and Science, Divili,
Andhra Pradesh, India
3
Ph.D Scholar, Department of Mechanical Engineering, J.N.T.U. Kakinada, Andhra Pradesh, India
Abstract
The project deals with the computational fluid dynamics analysis of mixed flow of hot and cold water in T- pipes and it is mainly
concentrated on analytical approach to the areas where Pipes (used for flow) are mostly susceptible to damage. The simulation is
done on T-pipe by placing the nozzle at three different places, to know the pressure, temperature and velocity contours throughout
the flow and comparison was made. These T- pipes are mostly used in nuclear reactor cooling system to reduce the heat in the
nuclear reactors by mixing hot and cold water, where the mixing will takes place efficiently. And mixed flow at the outlet will take
heat from the inlet also due to convective heat transfer loss; the temperature at the boundaries of the T- pipe will be reduced. The
2D model of the pipe is made by GAMBIT and analysis is to be carried out by using K-Epsilon in FLUENT software. The models
are first generated using the data and then various velocity, temperature and pressure contours are to be drawn and graphed to
analyze the flow through the pipe.
Keywords: Gambit, Fluent, K-Epsilon model.
--------------------------------------------------------------------***----------------------------------------------------------------------
1. INTRODUCTION
Pipe networks are mainly used for transportation of fluids
from one place to another. In addition to pipes, the network
also consists of elbow, T-junctions, bends, contractions,
expansions, valves, meters, pumps, turbines and many other
components. All these components cause loss in pressure
due to change in momentum of the flow caused due to
friction and pipe components. This means conversion of
flow energy in to heat due to friction or energy lost due to
turbulence.
Flow analysis is very important in nuclear power plant
cooling systems to know how the variations are taking place
with respect to the cross section. These T- pipes are used in
nuclear power plant cooling systems to reduce the heat in
the nuclear reactors by mixing hot water with cold water in
the T- pipes where the mixing will takes place efficiently
and mixed flow at the outlet take the heat from the inlet and
releases out at temperature to atmospheric temperature.
Turbulent mixing of fluid of different temperature in T-
junction geometries became of significant importance in the
field of nuclear reactor safety, since it can lead to highly
transient temperature fluctuations at the adjacent pipe walls,
cyclic thermal stresses in the pipe walls and consequently to
thermal fatigue and failure of the pipe line. Mixing fluid of
different temperature in T-junction geometries became of
significant importance in the field of nuclear reactor safety.
2. PROCEDURE AND GEOMETRY
The current study used FLUENT software, to solve the
balance equation using control volume approach. These
equations are solved by converting the complex partial
differential equations into simple algebraic equations. In the
GAMBIT software, a fine meshing is done by using
successive ratio and later given the boundary conditions for
the geometry and for the media.
The geometry was done in the GAMBIT with
measurements; pipe diameter is 50mm, radius of the pipe
25mm and length of the pipe 500mm. Defining required
boundaries like inlet, outlet and wall of the geometry and
mesh under tetrahedron. Defining the boundary conditions
for the water. The velocity at inlet of the cold fluid is 4m/sec
and at outlet is 2m/sec and the gravitational acceleration of
9.81 m/s2 in downward flow direction was used.
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 2
Fig-2.1: first model of tee pipe.
Fig-2.2: second model of tee pipe.
Fig-2.3: third model of tee pipe.
Fig-2.4: forth model of tee pipe.
3. SOLUTION STRATEGY
The simulation is done in the FLUENT based upon the
governing equations. The steps followed in the fluent are
define Model, define Material, define cell zone, boundary
condition, solve, iterate, and analyze results. The convergent
of the solution is shown in below fig 3.1.
Fig-3.1: iterations of solution.
3.1 Continuity Equation
Continuity Equation also called conservation of mass. The
overall mass balance is
Input – output = accumulation
Assuming that there is no storage the Mass input = mass
output.
However, as long as the flow is steady (time-invariant),
within this tube, since, mass cannot be created or destroyed
then the above equation will be
m1
.
= m1
.
(1)
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 3
dm1
dt
=
dm1
dt
(2)
ρA1u1 = ρA2u2 (3)
A1v1 = A2v2 (4)
3.2 Momentum Equation and Bernoulli Equation
It is also called equation of motion .According to Newton’s
2nd law (the time rate of change of momentum of the fluid
particles within this stream tube slice must equal to the
forces acting on it).
F = mass* acceleration
Consider a small element of the flowing fluid as shown
below, Let
dA : cross-sectional area of the fluid element,
dL : Length of the fluid element,
dW : Weight of the fluid element,
u : Velocity of the fluid element,
P : Pressure of the fluid element.
Assuming that the fluid is steady, non-viscous (the frictional
losses are zero) and incompressible (the density of fluid is
constant).
The forces on the cylindrical fluid element are,
Pressure force acting on the direction of flow (PdA).
Pressure force acting on the opposite direction of flow
[(P+dP)dA].
A component of gravity force acting on the opposite
direction of flow (dW sin θ).
Hence, Total force = gravity force + pressure force
The pressure force in the direction of low
Fp = PdA – (P+dP) dA = – dPdA (5)
The gravity force in the direction of flow
Fg = – dW sin θ {W=m g = ρ dA dL g}.
= – ρ g dA dL sin θ {sin θ = dz / dL}.
= – ρ g dA dz. (6)
The net force in the direction of flow
F = m a {m = ρ dA dL .
= ρ dA dL a.
= ρ dA u du. (7)
We have
ρ dA u du = – dP dA – ρ g dA dz {÷ ρ dA }
dP/ ρ + udu + dz g = 0 --------- Euler’s equation of motion.
Bernoulli’s equation could be obtain by integration the
Euler’s equation.
∫dP/ ρ + ∫udu + ∫dz g = constant.
P/ ρ + u2/2 + z g = constant.
ΔP/ ρ + Δu2/2 + Δz g = 0 -- Bernoulli’s equation.
4. RESULTS
4.1 Results of First Model
Fig-4.1.1: pressure contours.
Fig-4.1.2: velocity contours.
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 4
Fig-4.1.3: temperature contours.
Fig-4.1.4: turbulence contours.
Table-4.1.1: results of flow analysis.
S.No Parameters Min. Max.
1 Pressure(Pascal) -43875.04 2921.139
2 Velocity(m/s) 0 7.472435
3 Temperature(K) 300 395
4 Turbulent(m2
/s2
) 0.218194 5.456457
Table-4.1.2: results of mass flow rate.
Mass Flow Rate (kg/s)
Interior -21023.578
Inlet_C 119.78401
Inlet_H 59.892004
Outlet -179.67601
Wall 0
4.2 Results of Second Model
Fig-4.2.1: pressure contours.
Fig-4.2.2: velocity contours.
Fig-4.2.3: temperature contours.
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 5
Fig-4.2.4: turbulence contours.
Table-4.2.1: results of flow analysis.
S.No Parameters Min. Max.
1 Pressure(Pascal) -77467.77 25588.5
2 Velocity(m/s) 0 10.52352
3 Temperature(K) 300 395
4 Turbulent(m2
/s2
) 0.1677168 7.973526
Table-4.2.2: results of mass flow rate.
Mass Flow Rate (kg/s)
Interior -4658.3701
Inlet_C 199.64001
Inlet_H 59.892004
Outlet -259.53202
Wall 0
4.3 Results of Third Model
Fig-4.3.1: pressure contours.
Fig-4.3.2: velocity contours.
Fig-4.3.3: temperature contours.
Fig-4.3.4: turbulence contours.
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 6
Table-4.3.1: results of flow analysis.
S.No Parameters Min. Max.
1 Pressure(Pascal) -77065.7 6913.483
2 Velocity(m/s) 0 10.16165
3 Temperature(K) 300 395
4 Turbulent(m2
/s2
) 0.2659736 9.080444
Table-4.3.2: results of mass flow rate.
Mass Flow Rate (kg/s)
Interior -4485.8018
Inlet_C 119.78401
Inlet_H 99.820006
Outlet -219.60401
Wall 0
4.4 Results of Forth Model
Fig-4.4.1: pressure contours.
Fig-4.4.2: velocity contours.
Fig-4.4.3: temperature contours.
Fig-4.4.4: turbulence contours.
Table-4.4.1: results of flow analysis.
S.No Parameters Min. Max.
1 Pressure(Pascal) -59552.35 2714.012
2 Velocity(m/s) 0 10.43727
3 Temperature(K) 300 395
4 Turbulent(m2
/s2
) 0.1806357 5.066483
Table-4.4.2: results of mass flow rate.
Mass Flow Rate (kg/s)
Interior -3245.6271
Inlet_C 119.78401
Inlet_H 59.892004
Outlet -179.67601
Wall 0
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 7
5. CONCLUSIONS
From the above analysis it is found out that flow will change
greatly in t-pipe due to different cross section and also
because of hot and cold water mixing process. Temperature,
pressure and velocity variations occur at the outlet from the
cold and hot water inlets. Hot water will possess a high
average kinetic energy and cold water will possess low
average kinetic energy, the mixture will have an average
kinetic energy of an intermediate value. Initially hot water
and cold water mixes up to some extent as the cross section
goes on increasing mixing hot and cold water takes place
completely then the temperature of the mixed flow reduces.
As the hot water and cold water enters at different velocities
of mixed flow will be increased as pressure decreases.
Pressure for mixed flow at the outlet will be reduced
because of the cross section variation at the joining point of
hot and cold water and also high velocities will cause more
pressure drop. Turbulence is created at the inter section
point of the T-pipe because the cross section at that point
has changed suddenly and also the velocity at that point has
increased suddenly due to the mixing of hot and cold water
at that point.
REFERENCES
[1]. Large eddy simulation of hot and cold fluids mixing in a
T-junction for predicting thermal fluctuations, Wie-yu Zhu,
Tao Lu, Pie-xue Jiang Zhi-jun Guo Kuishing Wang,
November 2009,volume 30, Issue 11, pp 1379-1392.
[2]. Simulation of turbulent and thermal mixing in T-
junctions using urans and scale-resolving turbulence models
in Ansys cfx, Th. Frank, M.Adlakha, C. Lifante, H.M.
Prasser, F.Menter, ANSYS Germany GmbH,
Staudenfeldweg 12, D-83624 Otterfing, Germany ETH
Zürich, Dept. Energy Technology, Zürich, Switzerland.
[3]. A coupled CFD-FEM strategy to predict thermal fatigue
in mixing tees of nuclear reactors, M.H.C. Hannink, A.K.
Kuczaj, F.J. Blom, J.M. Church and E.M.J. Komen.
[4]. Thermal mixing of two miscible fluids in a T- shaped
micro channel, Bin Xu, Teck Neng Wong, Nam-Trung
Nguyen, Zhizhao Che, John Chee Kiong Chai, Dec 2010;
4(4): 044102. Published online Oct 1, 2010.
[5]. Assessment of thermal fatigue in mixing tee by fsi
analysis, myung jo jhung, Research Management
Department, Korea Institute of Nuclear Safety 62 Gwahak-
ro, Yuseong-gu, Daejeon, 305-338, Korea, Received April
12, 2012 , Accepted for Publication June 27, 2012.
[6]. Large-eddy simulation of fluid flow and heat transfer in
a mixing tee junction, Tao Lu, Yongwei Wang, Kuisheng
Wang, Chinese Journal of Mechanical Engineering
November 2012, Volume 25, Issue 6, pp 1144-1150.
[7]. A coupled CFD-FEM strategy to predict thermal fatigue
in mixing fluids of nuclear reactors, M.H.C. Hannink, A.K.
Kuczaj, F.J. Blom, J.M. Church and E.M.J. Komen.
[8]. ANSYS, Inc., 2010, ANSYS CFX-Solver Theory Guide
and ANSYS CFX-Solver Manager User’s Guide,
Canonsburg, PA.
[9]. ANSYS, Inc., 2010, Theory Reference for ANSYS and
ANSYS Workbench Release 13.0, Canonsburg, PA.
[10]. Bannantine, J.A., Comer, J.J., Hand rock, J.L., 1989,
Fundamentals of Metal Fatigue Analysis, Prentice Hall,
New Jersey.
BIOGRAPHIES
1. K.Venkateswara Rao completed
schooling from TWAB High school,
West Godavari district with 84%
marks. Completed B.Tech degree from
Madhira institute of technology and
Sciences with 71%. Now pursuing
M.Tech from Kakinada Institute of
Technology and Science,
Tirupathi(V), Divili, East Godavari
Dist., A.P., India
2. Mr. V.V.Rama Krishna completed
his B.Tech. from JNTUHyderabad
and M.Tech. from Godavari Institute
of Technology & Engineering,
Rajahmundry. He has 3 years of
Industrial and 5 years of teaching
experience. Now he is working as
Asst. Professor in Kakinada Institute
of Technology & Science, Divili and
doing research in Thermal Engineering.
3.Mr. V.Subrahmanyam working as
Assoc. Professor and Head of
Mechanical Engineering Department
in KITS-Divili Engineering college,
Andhra Pradesh, India. He has 15
years of teaching experience in various
reputed engineering colleges. He
guided so many B.Tech and M.Tech
projects. He has three publications in
reputed international journals. He is doing research in Nano-
Technology and Thermal Engineering.

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Comparison of cfd simulation of hot and cold fluid mixing in t pipe by placing nozzle at different places

  • 1. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 1 COMPARISON OF CFD SIMULATION OF HOT AND COLD FLUID MIXING IN T-PIPE BY PLACING NOZZLE AT DIFFERENT PLACES K.Venkateswara Rao1 , V.V.RamaKrishna2 , V. Subrahmanyam3 1 M.Tech Scholar, Department of Mechanical Engineering, Kakinada Institute of Technology and Science, Divili, Andhra Pradesh, India 2 Assistant Professor, Department of Mechanical Engineering, Kakinada Institute of Technology and Science, Divili, Andhra Pradesh, India 3 Ph.D Scholar, Department of Mechanical Engineering, J.N.T.U. Kakinada, Andhra Pradesh, India Abstract The project deals with the computational fluid dynamics analysis of mixed flow of hot and cold water in T- pipes and it is mainly concentrated on analytical approach to the areas where Pipes (used for flow) are mostly susceptible to damage. The simulation is done on T-pipe by placing the nozzle at three different places, to know the pressure, temperature and velocity contours throughout the flow and comparison was made. These T- pipes are mostly used in nuclear reactor cooling system to reduce the heat in the nuclear reactors by mixing hot and cold water, where the mixing will takes place efficiently. And mixed flow at the outlet will take heat from the inlet also due to convective heat transfer loss; the temperature at the boundaries of the T- pipe will be reduced. The 2D model of the pipe is made by GAMBIT and analysis is to be carried out by using K-Epsilon in FLUENT software. The models are first generated using the data and then various velocity, temperature and pressure contours are to be drawn and graphed to analyze the flow through the pipe. Keywords: Gambit, Fluent, K-Epsilon model. --------------------------------------------------------------------***---------------------------------------------------------------------- 1. INTRODUCTION Pipe networks are mainly used for transportation of fluids from one place to another. In addition to pipes, the network also consists of elbow, T-junctions, bends, contractions, expansions, valves, meters, pumps, turbines and many other components. All these components cause loss in pressure due to change in momentum of the flow caused due to friction and pipe components. This means conversion of flow energy in to heat due to friction or energy lost due to turbulence. Flow analysis is very important in nuclear power plant cooling systems to know how the variations are taking place with respect to the cross section. These T- pipes are used in nuclear power plant cooling systems to reduce the heat in the nuclear reactors by mixing hot water with cold water in the T- pipes where the mixing will takes place efficiently and mixed flow at the outlet take the heat from the inlet and releases out at temperature to atmospheric temperature. Turbulent mixing of fluid of different temperature in T- junction geometries became of significant importance in the field of nuclear reactor safety, since it can lead to highly transient temperature fluctuations at the adjacent pipe walls, cyclic thermal stresses in the pipe walls and consequently to thermal fatigue and failure of the pipe line. Mixing fluid of different temperature in T-junction geometries became of significant importance in the field of nuclear reactor safety. 2. PROCEDURE AND GEOMETRY The current study used FLUENT software, to solve the balance equation using control volume approach. These equations are solved by converting the complex partial differential equations into simple algebraic equations. In the GAMBIT software, a fine meshing is done by using successive ratio and later given the boundary conditions for the geometry and for the media. The geometry was done in the GAMBIT with measurements; pipe diameter is 50mm, radius of the pipe 25mm and length of the pipe 500mm. Defining required boundaries like inlet, outlet and wall of the geometry and mesh under tetrahedron. Defining the boundary conditions for the water. The velocity at inlet of the cold fluid is 4m/sec and at outlet is 2m/sec and the gravitational acceleration of 9.81 m/s2 in downward flow direction was used.
  • 2. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 2 Fig-2.1: first model of tee pipe. Fig-2.2: second model of tee pipe. Fig-2.3: third model of tee pipe. Fig-2.4: forth model of tee pipe. 3. SOLUTION STRATEGY The simulation is done in the FLUENT based upon the governing equations. The steps followed in the fluent are define Model, define Material, define cell zone, boundary condition, solve, iterate, and analyze results. The convergent of the solution is shown in below fig 3.1. Fig-3.1: iterations of solution. 3.1 Continuity Equation Continuity Equation also called conservation of mass. The overall mass balance is Input – output = accumulation Assuming that there is no storage the Mass input = mass output. However, as long as the flow is steady (time-invariant), within this tube, since, mass cannot be created or destroyed then the above equation will be m1 . = m1 . (1)
  • 3. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 3 dm1 dt = dm1 dt (2) ρA1u1 = ρA2u2 (3) A1v1 = A2v2 (4) 3.2 Momentum Equation and Bernoulli Equation It is also called equation of motion .According to Newton’s 2nd law (the time rate of change of momentum of the fluid particles within this stream tube slice must equal to the forces acting on it). F = mass* acceleration Consider a small element of the flowing fluid as shown below, Let dA : cross-sectional area of the fluid element, dL : Length of the fluid element, dW : Weight of the fluid element, u : Velocity of the fluid element, P : Pressure of the fluid element. Assuming that the fluid is steady, non-viscous (the frictional losses are zero) and incompressible (the density of fluid is constant). The forces on the cylindrical fluid element are, Pressure force acting on the direction of flow (PdA). Pressure force acting on the opposite direction of flow [(P+dP)dA]. A component of gravity force acting on the opposite direction of flow (dW sin θ). Hence, Total force = gravity force + pressure force The pressure force in the direction of low Fp = PdA – (P+dP) dA = – dPdA (5) The gravity force in the direction of flow Fg = – dW sin θ {W=m g = ρ dA dL g}. = – ρ g dA dL sin θ {sin θ = dz / dL}. = – ρ g dA dz. (6) The net force in the direction of flow F = m a {m = ρ dA dL . = ρ dA dL a. = ρ dA u du. (7) We have ρ dA u du = – dP dA – ρ g dA dz {÷ ρ dA } dP/ ρ + udu + dz g = 0 --------- Euler’s equation of motion. Bernoulli’s equation could be obtain by integration the Euler’s equation. ∫dP/ ρ + ∫udu + ∫dz g = constant. P/ ρ + u2/2 + z g = constant. ΔP/ ρ + Δu2/2 + Δz g = 0 -- Bernoulli’s equation. 4. RESULTS 4.1 Results of First Model Fig-4.1.1: pressure contours. Fig-4.1.2: velocity contours.
  • 4. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 4 Fig-4.1.3: temperature contours. Fig-4.1.4: turbulence contours. Table-4.1.1: results of flow analysis. S.No Parameters Min. Max. 1 Pressure(Pascal) -43875.04 2921.139 2 Velocity(m/s) 0 7.472435 3 Temperature(K) 300 395 4 Turbulent(m2 /s2 ) 0.218194 5.456457 Table-4.1.2: results of mass flow rate. Mass Flow Rate (kg/s) Interior -21023.578 Inlet_C 119.78401 Inlet_H 59.892004 Outlet -179.67601 Wall 0 4.2 Results of Second Model Fig-4.2.1: pressure contours. Fig-4.2.2: velocity contours. Fig-4.2.3: temperature contours.
  • 5. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 5 Fig-4.2.4: turbulence contours. Table-4.2.1: results of flow analysis. S.No Parameters Min. Max. 1 Pressure(Pascal) -77467.77 25588.5 2 Velocity(m/s) 0 10.52352 3 Temperature(K) 300 395 4 Turbulent(m2 /s2 ) 0.1677168 7.973526 Table-4.2.2: results of mass flow rate. Mass Flow Rate (kg/s) Interior -4658.3701 Inlet_C 199.64001 Inlet_H 59.892004 Outlet -259.53202 Wall 0 4.3 Results of Third Model Fig-4.3.1: pressure contours. Fig-4.3.2: velocity contours. Fig-4.3.3: temperature contours. Fig-4.3.4: turbulence contours.
  • 6. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 6 Table-4.3.1: results of flow analysis. S.No Parameters Min. Max. 1 Pressure(Pascal) -77065.7 6913.483 2 Velocity(m/s) 0 10.16165 3 Temperature(K) 300 395 4 Turbulent(m2 /s2 ) 0.2659736 9.080444 Table-4.3.2: results of mass flow rate. Mass Flow Rate (kg/s) Interior -4485.8018 Inlet_C 119.78401 Inlet_H 99.820006 Outlet -219.60401 Wall 0 4.4 Results of Forth Model Fig-4.4.1: pressure contours. Fig-4.4.2: velocity contours. Fig-4.4.3: temperature contours. Fig-4.4.4: turbulence contours. Table-4.4.1: results of flow analysis. S.No Parameters Min. Max. 1 Pressure(Pascal) -59552.35 2714.012 2 Velocity(m/s) 0 10.43727 3 Temperature(K) 300 395 4 Turbulent(m2 /s2 ) 0.1806357 5.066483 Table-4.4.2: results of mass flow rate. Mass Flow Rate (kg/s) Interior -3245.6271 Inlet_C 119.78401 Inlet_H 59.892004 Outlet -179.67601 Wall 0
  • 7. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 7 5. CONCLUSIONS From the above analysis it is found out that flow will change greatly in t-pipe due to different cross section and also because of hot and cold water mixing process. Temperature, pressure and velocity variations occur at the outlet from the cold and hot water inlets. Hot water will possess a high average kinetic energy and cold water will possess low average kinetic energy, the mixture will have an average kinetic energy of an intermediate value. Initially hot water and cold water mixes up to some extent as the cross section goes on increasing mixing hot and cold water takes place completely then the temperature of the mixed flow reduces. As the hot water and cold water enters at different velocities of mixed flow will be increased as pressure decreases. Pressure for mixed flow at the outlet will be reduced because of the cross section variation at the joining point of hot and cold water and also high velocities will cause more pressure drop. Turbulence is created at the inter section point of the T-pipe because the cross section at that point has changed suddenly and also the velocity at that point has increased suddenly due to the mixing of hot and cold water at that point. REFERENCES [1]. Large eddy simulation of hot and cold fluids mixing in a T-junction for predicting thermal fluctuations, Wie-yu Zhu, Tao Lu, Pie-xue Jiang Zhi-jun Guo Kuishing Wang, November 2009,volume 30, Issue 11, pp 1379-1392. [2]. Simulation of turbulent and thermal mixing in T- junctions using urans and scale-resolving turbulence models in Ansys cfx, Th. Frank, M.Adlakha, C. Lifante, H.M. Prasser, F.Menter, ANSYS Germany GmbH, Staudenfeldweg 12, D-83624 Otterfing, Germany ETH Zürich, Dept. Energy Technology, Zürich, Switzerland. [3]. A coupled CFD-FEM strategy to predict thermal fatigue in mixing tees of nuclear reactors, M.H.C. Hannink, A.K. Kuczaj, F.J. Blom, J.M. Church and E.M.J. Komen. [4]. Thermal mixing of two miscible fluids in a T- shaped micro channel, Bin Xu, Teck Neng Wong, Nam-Trung Nguyen, Zhizhao Che, John Chee Kiong Chai, Dec 2010; 4(4): 044102. Published online Oct 1, 2010. [5]. Assessment of thermal fatigue in mixing tee by fsi analysis, myung jo jhung, Research Management Department, Korea Institute of Nuclear Safety 62 Gwahak- ro, Yuseong-gu, Daejeon, 305-338, Korea, Received April 12, 2012 , Accepted for Publication June 27, 2012. [6]. Large-eddy simulation of fluid flow and heat transfer in a mixing tee junction, Tao Lu, Yongwei Wang, Kuisheng Wang, Chinese Journal of Mechanical Engineering November 2012, Volume 25, Issue 6, pp 1144-1150. [7]. A coupled CFD-FEM strategy to predict thermal fatigue in mixing fluids of nuclear reactors, M.H.C. Hannink, A.K. Kuczaj, F.J. Blom, J.M. Church and E.M.J. Komen. [8]. ANSYS, Inc., 2010, ANSYS CFX-Solver Theory Guide and ANSYS CFX-Solver Manager User’s Guide, Canonsburg, PA. [9]. ANSYS, Inc., 2010, Theory Reference for ANSYS and ANSYS Workbench Release 13.0, Canonsburg, PA. [10]. Bannantine, J.A., Comer, J.J., Hand rock, J.L., 1989, Fundamentals of Metal Fatigue Analysis, Prentice Hall, New Jersey. BIOGRAPHIES 1. K.Venkateswara Rao completed schooling from TWAB High school, West Godavari district with 84% marks. Completed B.Tech degree from Madhira institute of technology and Sciences with 71%. Now pursuing M.Tech from Kakinada Institute of Technology and Science, Tirupathi(V), Divili, East Godavari Dist., A.P., India 2. Mr. V.V.Rama Krishna completed his B.Tech. from JNTUHyderabad and M.Tech. from Godavari Institute of Technology & Engineering, Rajahmundry. He has 3 years of Industrial and 5 years of teaching experience. Now he is working as Asst. Professor in Kakinada Institute of Technology & Science, Divili and doing research in Thermal Engineering. 3.Mr. V.Subrahmanyam working as Assoc. Professor and Head of Mechanical Engineering Department in KITS-Divili Engineering college, Andhra Pradesh, India. He has 15 years of teaching experience in various reputed engineering colleges. He guided so many B.Tech and M.Tech projects. He has three publications in reputed international journals. He is doing research in Nano- Technology and Thermal Engineering.