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EXPERIMENTAL AND COMPUTATIONAL
ANALYSIS OF HEAT TRANSFER IN A SHELL
AND TUBE HEAT EXCHANGER
Samiullah Qureshi Dr.Abdul Fatah
Abbasi
Qadir Nawaz
Shafique
Sanjay Kumar
Menghwar
Teaching Assistant/
M.E Student
Mech: Engg: Dept.
MUET Jamshoro
Professor
Mech: Engg: Dept.
MUET Jamshoro
Lecturer
Mech: Engg: Dept.:
MUET SZAB Campus
KHP Mir’s
Lab Engineer/
M.E Student
Mech: Engg: Dept.
MUET SZAB Campus
KHP Mir’s
OUTLINE
 Introduction
 Literature review
 Experimental setup
 Simulation and modelling procedure
 Results
 Conclusion
 References
INTRODUCTION
 To exchange heat between two fluids → heat
exchanger
 Different types → Air conditioning , Power production,
Space heating
 Widely used type → shell and tube heat exchanger
 Consist of bundle of tubes enclosed in cylindrical shell
 Efficient & energy saving heat exchanger →
Researchers conducts experimental and numerical
work
INTRODUCTION
 In this study,
 Experimental and CFD Investigation of Parallel and
Counter Flow in STHEx
 CFD Software → ANSYS Fluent
 Simulated result
 Heat Transfer coefficient ,
 Effectiveness
 Compared with Experimental data
 Also effect of mass flow rate → performance of heat
exchanger
 M. Thirumarimurugan et al. [1] developed numerical model in
MATLAB
 Predict outlets temperature
 Simulated results compared
 .Žarko Stevanović et al. [2] → 3-D numerical study
 Fluid flow and heat transfer
 Chen-Kim modification of k − ε model → good agreement with
experimental data
 Optimal flow distribution → reduce pressure drop , enhance heat
transfer
 Ender Ozden, and Ilker Tari [3] conducted → CFD study
 Design of STHEx → baffle spacing, baffle cut
 Simulated results compared → kern and Bell-Delaware methods
LITERATURE REVIEW
EXPERIMENTAL SETUP
 Arm field HT33-XC-304 SHTHx → Heat transfer lab , MUET
 Stainless steel tubes , acrylic transverse baffles and shell
 Water heated in the vessel → electrical heater
 Hot fluid passes through S.S tubes → pump
 Tap water → Cold fluid
 Experiment performed for Counter and parallel flow
 Hot fluid → 𝑚 =0.076 kg/sec , Tin = 60°C
 Cold fluid → 𝑚 =0.036 kg/sec , Tin = 24°C
Heat Exchanger Specification (provided by Armfield limited)
S.No Description Unit Value
1 Shell inner diameter mm 39
2 Shell wall thickness mm 3
3 Tube outer diameter mm 6.35
4 Tube wall thickness mm 0.6
5 Number of Tubes mm 7
6 Shell/Tubes length mm 150
7 Shell inlet/outlet length mm 10
8 Baffle height mm 34.5
9 Baffle Thickness mm 3
EXPERIMENTAL SETUP
SIMULATION AND MODELLING PROCEDURE
Geometry
 Geometry in ANSYS design modeler
 Simplified geometry – 2D
Actual Model
Simplified Model
SIMULATION AND MODELLING PROCEDURE
 Meshing
 Carried out in ANSYS Meshing Client
 Whole fluid domain → Quadrilateral element type
 Initially Coarser meshing → 18330 elements
 Better Result → Fine meshing - 73370 elements
SIMULATION AND MODELLING PROCEDURE
 Models and Governing Equation
 According to system specification , some models need to be
adopted in CFD Software
 In ANSYS Fluent → two built in HEx models
 Heat Exchanger Model:
 DUEL CELL heat exchanger model
 Based on NTU method
 Flow is turbulent → Turbulent model Should be selected
SIMULATION AND MODELLING PROCEDURE
 Governing Equation
 k-ɛ Turbulence Model
 Turbulent kinetic energy k
Ui
𝜕k
𝜕xj
= vT
𝜕 Ui
𝜕xj
+
𝜕 Uj
𝜕xi
𝜕 Ui
𝜕xj
− ϵ +
𝜕
𝜕xj
v +
vT
σk
𝜕k
𝜕xj
 Turbulent dissipation ɛ
Ui
𝜕ε
𝜕xj
= Cε1vT
ε
k
𝜕 Ui
𝜕xj
+
𝜕 Uj
𝜕xi
𝜕 Ui
𝜕xj
− Cε2
ε2
k
+
𝜕
𝜕xj
v +
vT
σε
𝜕ε
𝜕xj
 Turbulent viscosity vT
𝑣 𝑇 = 𝐶𝜇
𝑘2
𝜀
SIMULATION AND MODELLING PROCEDURE
 Governing Equation
 Conservation of Mass:
𝜕ρUj
𝜕xj
= 0
 Momentum :
Uj
𝜕Ui
𝜕xj
= −
1
ρ
𝜕P
𝜕xi
+
1
ρ
𝜕𝜏𝑖𝑗
𝜕xi
 Energy:
𝛻 . V ρE + p = 𝛻. [ keff 𝛻T + (τeff . V)]
BC Type Shell Tube
Intel Mass-flow 0.034 Kg/sec 0.076 Kg/sec
Outlet Pressure outlet 0 0
Wall No slip condition Zero heat flux Zero heat flux
Turbulence Turbulence intensity
Length scale
5.62%
0.007 m
4.24%
0.00036m
Temperature Inlet temperature 297 K 333K
SIMULATION AND MODELLING PROCEDURE
 Boundary Conditions
 Selected according to need of model
T
RESULT
 Parallel Flow
 Temperature contours
→ Shell Side
I
N
L
E
T
O
U
T
L
E
T
→ Tube side
I
N
L
E
T
O
U
T
L
E
T
Experimental Simulated Diff:
Tube side Temp: difference 2.8 2.6 7.14%
Shell side Temp: difference 6.2 5.7 8.06%
Overall HT co-eff: (W/m2.K) 1432 1310 8.55%
NTU 0.201 0.184 8.4%
Effectiveness 0.174 0.162 6.8%
RESULT
 Comparison of simulated and experimental data
 Effect of mass flow rate on Heat Transfer
 Variation in hot mass flow rate
 At 𝒎 𝒉𝒐𝒕 = 0.038 Kg/sec , U = 1091 W/m2.K , Effect: = 0.1335
 With increasing mass flow rate – effectiveness increased
RESULT
20%
21.60%
23.15%
21%
25.80%
27.34%
0%
5%
10%
15%
20%
25%
30%
100% 200% 300%
Increment
Mass Flow Increment
U (W/m2.K) Effectiveness
RESULT
 Counter Flow
 Temperature contours
→ Tube side
I
N
L
E
T
O
U
T
L
E
T
→ Shell side
I
N
L
E
T
O
U
T
L
E
T
RESULT
 Comparison of simulated and experimental data
Variables Experimental Simulated Diff:
Tube side Temp: Difference 3.4 3.15 7.35%
Shell side Temp: difference 7.5 6.92 7.7%
Overall HT coeff: (W/m2.K) 1765 1623 8.05%
NTU 0.248 0.228 8.06%
Effectiveness 0.208 0.196 5.76%
 Effect of mass flow rate on Heat Transfer
 Variation in hot mass flow rate
 At 𝒎 𝒉𝒐𝒕 = 0.038 Kg/sec , U = 1184 W/m2.K , Effect: = 0.143
 With increasing mass flow rate – effectiveness increased
RESULT
37%
42.00% 43.00%
37%
44.00%
46.00%
0%
5%
10%
15%
20%
25%
30%
35%
40%
45%
50%
100% 200% 300%
Increment
Mass Flow Increment
U (W/m2.K) Effectiveness
CONCLUSION
 Effect of Mass Flow rate
 Effectiveness is increased with increase in hot fluid flow
 Increment of effectiveness in counter flow is almost 90%
more than of that in parallel flow for same mass flow
increment
 Effect of Flow Configuration
 Effectiveness in counter flow is almost 20% to 25% more
than of that in Parallel Flow for same mass flow
 CFD Analysis
 Good agreement with experimental data and theoretical
concepts
[1] M. Thirumarimurugan, T.Kannadasan and
E.Ramasamy, Performance Analysis of Shell and
Tube Heat Exchanger Using Miscible System,
American Journal of Applied Sciences 5 (5): 548-552,
2008
[2] Žarko Stevanović , Gradimir Ilić, Nenad Radojković,
Mića Vukić, Velimir Stefanović, Goran Vučković,
Design of shell-and-tube heat exchangers by using
CFD technique – part one: thermo-hydraulic
calculation, FACTA UNIVERSITATIS Series:
Mechanical Engineering Vol.1, No 8, 2001, pp. 1091
– 1105
[3] Ender Ozden, Ilker Tari, Shell Side CFD Analysis of a
Small Shell And Tube Heat Exchanger, Energy
Conversion and Management, 2010: 51;1004-1014
REFERENCE
THANK YOU

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FINAL2 PPT3

  • 1.
  • 2. EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF HEAT TRANSFER IN A SHELL AND TUBE HEAT EXCHANGER Samiullah Qureshi Dr.Abdul Fatah Abbasi Qadir Nawaz Shafique Sanjay Kumar Menghwar Teaching Assistant/ M.E Student Mech: Engg: Dept. MUET Jamshoro Professor Mech: Engg: Dept. MUET Jamshoro Lecturer Mech: Engg: Dept.: MUET SZAB Campus KHP Mir’s Lab Engineer/ M.E Student Mech: Engg: Dept. MUET SZAB Campus KHP Mir’s
  • 3. OUTLINE  Introduction  Literature review  Experimental setup  Simulation and modelling procedure  Results  Conclusion  References
  • 4. INTRODUCTION  To exchange heat between two fluids → heat exchanger  Different types → Air conditioning , Power production, Space heating  Widely used type → shell and tube heat exchanger  Consist of bundle of tubes enclosed in cylindrical shell  Efficient & energy saving heat exchanger → Researchers conducts experimental and numerical work
  • 5. INTRODUCTION  In this study,  Experimental and CFD Investigation of Parallel and Counter Flow in STHEx  CFD Software → ANSYS Fluent  Simulated result  Heat Transfer coefficient ,  Effectiveness  Compared with Experimental data  Also effect of mass flow rate → performance of heat exchanger
  • 6.  M. Thirumarimurugan et al. [1] developed numerical model in MATLAB  Predict outlets temperature  Simulated results compared  .Žarko Stevanović et al. [2] → 3-D numerical study  Fluid flow and heat transfer  Chen-Kim modification of k − ε model → good agreement with experimental data  Optimal flow distribution → reduce pressure drop , enhance heat transfer  Ender Ozden, and Ilker Tari [3] conducted → CFD study  Design of STHEx → baffle spacing, baffle cut  Simulated results compared → kern and Bell-Delaware methods LITERATURE REVIEW
  • 7. EXPERIMENTAL SETUP  Arm field HT33-XC-304 SHTHx → Heat transfer lab , MUET  Stainless steel tubes , acrylic transverse baffles and shell  Water heated in the vessel → electrical heater  Hot fluid passes through S.S tubes → pump  Tap water → Cold fluid  Experiment performed for Counter and parallel flow  Hot fluid → 𝑚 =0.076 kg/sec , Tin = 60°C  Cold fluid → 𝑚 =0.036 kg/sec , Tin = 24°C
  • 8. Heat Exchanger Specification (provided by Armfield limited) S.No Description Unit Value 1 Shell inner diameter mm 39 2 Shell wall thickness mm 3 3 Tube outer diameter mm 6.35 4 Tube wall thickness mm 0.6 5 Number of Tubes mm 7 6 Shell/Tubes length mm 150 7 Shell inlet/outlet length mm 10 8 Baffle height mm 34.5 9 Baffle Thickness mm 3 EXPERIMENTAL SETUP
  • 9. SIMULATION AND MODELLING PROCEDURE Geometry  Geometry in ANSYS design modeler  Simplified geometry – 2D Actual Model Simplified Model
  • 10. SIMULATION AND MODELLING PROCEDURE  Meshing  Carried out in ANSYS Meshing Client  Whole fluid domain → Quadrilateral element type  Initially Coarser meshing → 18330 elements  Better Result → Fine meshing - 73370 elements
  • 11. SIMULATION AND MODELLING PROCEDURE  Models and Governing Equation  According to system specification , some models need to be adopted in CFD Software  In ANSYS Fluent → two built in HEx models  Heat Exchanger Model:  DUEL CELL heat exchanger model  Based on NTU method  Flow is turbulent → Turbulent model Should be selected
  • 12. SIMULATION AND MODELLING PROCEDURE  Governing Equation  k-ɛ Turbulence Model  Turbulent kinetic energy k Ui 𝜕k 𝜕xj = vT 𝜕 Ui 𝜕xj + 𝜕 Uj 𝜕xi 𝜕 Ui 𝜕xj − ϵ + 𝜕 𝜕xj v + vT σk 𝜕k 𝜕xj  Turbulent dissipation ɛ Ui 𝜕ε 𝜕xj = Cε1vT ε k 𝜕 Ui 𝜕xj + 𝜕 Uj 𝜕xi 𝜕 Ui 𝜕xj − Cε2 ε2 k + 𝜕 𝜕xj v + vT σε 𝜕ε 𝜕xj  Turbulent viscosity vT 𝑣 𝑇 = 𝐶𝜇 𝑘2 𝜀
  • 13. SIMULATION AND MODELLING PROCEDURE  Governing Equation  Conservation of Mass: 𝜕ρUj 𝜕xj = 0  Momentum : Uj 𝜕Ui 𝜕xj = − 1 ρ 𝜕P 𝜕xi + 1 ρ 𝜕𝜏𝑖𝑗 𝜕xi  Energy: 𝛻 . V ρE + p = 𝛻. [ keff 𝛻T + (τeff . V)]
  • 14. BC Type Shell Tube Intel Mass-flow 0.034 Kg/sec 0.076 Kg/sec Outlet Pressure outlet 0 0 Wall No slip condition Zero heat flux Zero heat flux Turbulence Turbulence intensity Length scale 5.62% 0.007 m 4.24% 0.00036m Temperature Inlet temperature 297 K 333K SIMULATION AND MODELLING PROCEDURE  Boundary Conditions  Selected according to need of model
  • 15. T RESULT  Parallel Flow  Temperature contours → Shell Side I N L E T O U T L E T → Tube side I N L E T O U T L E T
  • 16. Experimental Simulated Diff: Tube side Temp: difference 2.8 2.6 7.14% Shell side Temp: difference 6.2 5.7 8.06% Overall HT co-eff: (W/m2.K) 1432 1310 8.55% NTU 0.201 0.184 8.4% Effectiveness 0.174 0.162 6.8% RESULT  Comparison of simulated and experimental data
  • 17.  Effect of mass flow rate on Heat Transfer  Variation in hot mass flow rate  At 𝒎 𝒉𝒐𝒕 = 0.038 Kg/sec , U = 1091 W/m2.K , Effect: = 0.1335  With increasing mass flow rate – effectiveness increased RESULT 20% 21.60% 23.15% 21% 25.80% 27.34% 0% 5% 10% 15% 20% 25% 30% 100% 200% 300% Increment Mass Flow Increment U (W/m2.K) Effectiveness
  • 18. RESULT  Counter Flow  Temperature contours → Tube side I N L E T O U T L E T → Shell side I N L E T O U T L E T
  • 19. RESULT  Comparison of simulated and experimental data Variables Experimental Simulated Diff: Tube side Temp: Difference 3.4 3.15 7.35% Shell side Temp: difference 7.5 6.92 7.7% Overall HT coeff: (W/m2.K) 1765 1623 8.05% NTU 0.248 0.228 8.06% Effectiveness 0.208 0.196 5.76%
  • 20.  Effect of mass flow rate on Heat Transfer  Variation in hot mass flow rate  At 𝒎 𝒉𝒐𝒕 = 0.038 Kg/sec , U = 1184 W/m2.K , Effect: = 0.143  With increasing mass flow rate – effectiveness increased RESULT 37% 42.00% 43.00% 37% 44.00% 46.00% 0% 5% 10% 15% 20% 25% 30% 35% 40% 45% 50% 100% 200% 300% Increment Mass Flow Increment U (W/m2.K) Effectiveness
  • 21. CONCLUSION  Effect of Mass Flow rate  Effectiveness is increased with increase in hot fluid flow  Increment of effectiveness in counter flow is almost 90% more than of that in parallel flow for same mass flow increment  Effect of Flow Configuration  Effectiveness in counter flow is almost 20% to 25% more than of that in Parallel Flow for same mass flow  CFD Analysis  Good agreement with experimental data and theoretical concepts
  • 22. [1] M. Thirumarimurugan, T.Kannadasan and E.Ramasamy, Performance Analysis of Shell and Tube Heat Exchanger Using Miscible System, American Journal of Applied Sciences 5 (5): 548-552, 2008 [2] Žarko Stevanović , Gradimir Ilić, Nenad Radojković, Mića Vukić, Velimir Stefanović, Goran Vučković, Design of shell-and-tube heat exchangers by using CFD technique – part one: thermo-hydraulic calculation, FACTA UNIVERSITATIS Series: Mechanical Engineering Vol.1, No 8, 2001, pp. 1091 – 1105 [3] Ender Ozden, Ilker Tari, Shell Side CFD Analysis of a Small Shell And Tube Heat Exchanger, Energy Conversion and Management, 2010: 51;1004-1014 REFERENCE