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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1882
THERMAL ANALYSIS OF HEAT TRANSFER THROUGH COMPOSITE WALL
BY USING F.E.A. METHOD
Bhangale Bhushan Suresh1, Dr.M.K.Chopra2
1PG Student, Department of Mechanical Engineering, RKDF IST, Bhopal, MP, India
2Vice Principal & HOD Department of Mechanical Engineering, RKDF IST, Bhopal, MP, India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - It is very difficult to calculate and analyze with
precision the thermal behavior of the walls of different
materials attached to each other. The study of composite
materials thermal behavior is useful for the determination of
heat flux, temperature distribution, heatflowrateandthermal
conductivity.
These composite materials which can be implemented to
many applications such as thermal ventilations, Insulators,
metallic multiwall thermal protection systems, etc. In this
study we are going to analyze the thermal behavior of four
composites. For finding heat flux, temperature distribution,
heat flow rate and thermal conductivity the finite element
program method ANSYS is used. The experimental test is
carried out for heat flux, temperature distribution, heat flow
rate and thermal conductivity of composite materials.
Experimental Results are compared with thefiniteelement
ANSYS results and the validation is done.
KeyWords:Thermal Conductivity,Composite Materials,
Heat Flux, Conduction, Heat Flow Rate
1. INTRODUCTION:-
The Study of composites is a philosophy of material design
that allows for the optimum material compositionalongwith
structural design and optimization in one concurrent and
interactive process.
The scope of composite materials research and technology
consists of Investigation of basic characteristics of the
constituent and composite materials, Material optimization
for given service conditions, Development of effective and
efficient fabrication procedures and understanding of their
effect on material properties.
1.1 Heat Transfer:-
The amount of heat transferred per unit time is called heat
transfer rate and is denoted by Q. The heat transfer rate has
unit J/s which is equivalent to Watt. When the rate of heat
transfer Q is available, then total amount of heat energy
transferred ∆U during a time interval ∆ t can be obtained
form,
(Joule)
The rate of heat transfer per unit area normal to the
direction of heat flow is called heat flux and is expressed as,
q=Q/A.
2. OBJECTIVE OF WORK:-
The main objective of the presentresearchwork istodevelop
composite structure and to find the thermal behavior of that
composite using Finite Element method, analytical method
and Experimental method
Analytical method has been performed to obtain the
relative values of temperature, heat flow rate and heat flux.
After Analytical method, Experimental method has been
performed to obtain the relative values of temperature, heat
flux, heat flow rate and thermal conductivity.
After analytical and experimental method, Finite Element
Analysis has been performed to obtain the relative values of
temperature, heat flow rate, heat flux and thermal
conductivity.
Finally a comparative study has been made between Finite
Element Method and Experimental method.
3. METHODOLOGY:-
The experimental set up consists of three disks of equal
diameters but variable thickness arranged to form a slab of
same diameter and the heater ware placed at one side of
composite wall. Three types of slabs are provided on heater
which forms a composite structure.
Composition of materials:
1. MS-Hylum-wood
2. MS-Concrete-Fiber
3. MS-Fiber Glass-Brick
4. MS-Wood-Fiber Glass
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1883
Specifications:
Plate Dimensions:
Materials Diameter (mm)
Thickness
(mm)
MS 300 25
Fiber glass 300 20
Hylum 300 20
Wood 300 15
Brick 300 15
Concrete 300 15
4. MATHEMATICAL MODELING:-
The mathematical modelling is the idealization of the
physical problems until defined set of (mathematical)
constraints, representing the main features is established.
Mathematical modeling is required not only in analytical
work but also in actual heat- transfer practice, where a large
commercial computer package is used.
Table 4.1:-MS-Hylum-Wood
T1 T2 T3 T4 Q (W)
q
(W/m2)
100 99.97 38.05 22.86 3.7202 52.6311
150 149.96 48.34 23.42 6.1050 86.3690
200 199.95 58.64 23.99 8.4898 120.106
Table 4.2:- MS-Concrete-Fiber Glass
T1 T2 T3 T4 Q (W)
q
(W/m2)
100 99.95 96.86 36.27 7.8519 111.08
150 149.92 144.85 45.42 12.885 182.28
200 199.89 192.84 54.57 17.918 253.49
Table 4.3:- MS-Fiber Glass-Brick
T1 T2 T3 T4 Q (W)
q
(W/m2)
100 99.95 28.49 27.11 6.945 98.2562
150 149.93 32.66 30.39 11.397 161.24
200 199.90 36.82 33.67 15.849 224.225
Table 4.4:- MS-Wood-Fiber Glass
T1 T2 T3 T4 Q (W)
q
(W/m2)
100 99.96 71.63 31.45 5.206 73.653
150 149.95 103.46 37.53 8.5435 120.86
200 199.93 135.28 43.60 11.88 168.08
5. EXPERIMENTATION:-
A composite slab consists of slab of three different materials
which are MS, Hylum, & wood for one composite. There are
such four composites of different materials. Slabs & heating
element are circular in cross section. The instrument
consists of three disks of equal diameters but variable
thickness arranged to form a slab. The set up consists of a
heater placed at one side of composite wall.
Experimental Result Table for Temperature
Distribution:-
Table 5.1:-MS-Hylum-Wood
Sr.
No.
Temperature Q (W)
q
(W/m2)
K
(W/m0c)
1 100 5 70.82 0.0544
2 150 7.5 106.23 0.0497
3 200 9.0 127.47 0.0429
Table 5.2:- MS-Concrete-Fiber Glass
Sr.
No.
Temperature Q (W) q (W/m2)
K
(W/m0c)
1 100 8 113.31 0.0871
2 150 14 198.30 0.0929
3 200 18.6 263.45 0.0888
Table 5.3:- MS-Fiber Glass-Brick
Sr.
No.
TemperatureQ (W)
q
(W/m2)
K
(W/m0c)
1 100 7.3 103.39 0.0795
2 150 12.6 178.47 0.0836
3 200 16.8 237.96 0.0802
Table 3.1:- Plate Dimensions
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1884
Table 5.4:- MS-Wood-Fiber Glass
Sr.
No.
Temperature Q(w)
q
(W/m2)
K (W/m0c)
1 100 7.5 106.23 0.0817
2 150 9.5 134.56 0.0630
3 200 14 198.30 0.0668
Experimental Result Table for Directional
Heat Flux:-
Table 5.5 Directional Heat Flux
Temperature
(0C)
MS-F-GB
MS-H-
W
MS-C-FG
MS-W-
FG
100 103.39 70.8 113.31 106.23
150 178.47 106.23 198.3 134.56
200 237.96 127.47 263.45 198.3
Experimental Result Table for Heat Flow Rate:-
Table 5.6 Heat Flow Rate
Temperature
(0C)
MS-F-GB MS-H-W MS-C-FG
MS-W-
FG
100 7.3 5 8 7.5
150 12.6 7.5 14 9.5
200 16.8 9 18.6 14
Experimental Result Table for Thermal
Conductivity:-
Table5.7 Thermal Conductivity
Temperature
(0C)
MS-F-GB MS-H-W MS-C-FG
MS-W-
FG
100 0.0795 0.0544 0.0871 0.0817
150 0.0836 0.0497 0.0929 0.063
200 0.0802 0.0429 0.0888 0.0668
6. FINITE ELEMENT ANALYSIS:-
The finite element method is a numerical analysis technique
for obtaining approximate solutions to a wide variety of
engineering problems. Because of its diversity and flexibility
as an analysis tool, it is receiving much attention in
engineering schools and in industries. In more and more
engineering situations today, we find that it is necessary to
obtain approximate numerical solutions to problems rather
than exact closed form solution.
ANSYS Result table for Temperature Distribution:-
Table 6.1 Temperature Distribution at 1000c
Materials T1 T2 T3 T4
MS-F-GB 100 99.95 28.49 27.12
MS-H-W 100 99.97 38.05 22.88
MS-C-FG 100 99.95 96.86 36.25
MS-W-FG 100 99.96 71.63 31.6
Table 6.2 Temperature Distribution at 1500c
Materials T1 T2 T3 T4
MS-F-GB 150 149.93 32.66 30.39
MS-H-W 150 149.96 48.34 23.45
MS-C-FG 150 149.92 144.85 45.42
MS-W-FG 150 149.95 103.46 37.82
Table 6.3 Temperature Distribution at 2000c
Materials T1 T2 T3 T4
MS-F-GB 200 199.9 36.82 33.67
MS-H-W 200 199.95 58.64 24.01
MS-C-FG 200 199.89 192.84 54.54
MS-W-FG 200 199.93 135.28 44.01
ANSYS Result table for Directional Heat Flux:-
Table 6.4 Directional Heat Flux
Temperature
(0C)
MS-F-
GB
MS-H-W MS-C-FG
MS-W-
FG
100 98.25 52.63 111.08 73.65
150 161.24 86.36 182.28 120.86
200 224.225 120.106 253.49 168.08
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1885
ANSYS Result table for Heat Flow Rate:-
Table 6.5 Heat Flow Rate
Temperature
(0C)
MS-F-GB MS-H-W MS-C-FG
MS-W-
FG
100 6.945 3.7602 7.8519 5.3114
150 11.397 6.1706 12.885 8.7162
200 15.85 8.5802 17.919 12.121
7. Graphical Results:-
Graphical Experimental Results of Materials Vs
Heat Flux for all Composite Materials:-
0
50
100
150
200
250
300
MS-F-GB MS-H-W MS-C-FG MS-W-FG
HEATFLUX
MATERIAL
MATERIAL Vs HEAT FLUX
100
150
200
Graph 7.1 Materials Vs Heat Flux
Graphical Experimental Results of Materials Vs
Heat Flow Rate for all Composite Materials:-
Graph 7.2 Materials Vs Heat Flow Rate
Graphical Experimental Result of Materials Vs
Thermal Conductivity for all Composite
Materials:-
0
0.02
0.04
0.06
0.08
0.1
MS-F-GB MS-H-W MS-C-FG MS-W-FG
ThermalConductivity
Material
Material VsThermal Conductivity
100
150
200
Graph 7.3 Materials Vs Thermal conductivity
Graphical ANSYS Results of Materials Vs Heat
Flux for all Composite Materials:-
Graph 7.4 Materials Vs Heat Flux
Graphical ANSYS Results of Materials Vs Heat
Flow rate for all Composite Materials:-
Graph 6.5 Materials Vs Heat Flow Rate
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1886
8. CONCLUSIONS
Based on the analytical, finite element and experimental
investigation on the thermal behavior of different
composites, it can be concluded that:
1) The results obtained from the proposed analytical
method are in close approximation with the values
obtained by FEM simulation using ANSYS.
2) The values obtained from the proposed analytical
method are in close approximation with the values
obtained from experimental values.
3) The study shows that the thermal conductivity of the
composite material MS-Concrete-Fiber Glass is
0.0871MS-Fiber Glass-Brick is 0.0795 MS-Wood-Fiber
Glass is 0.0817 &MS-Hylum-Wood is 0.0544
4) The study shows that the heat flow rate MS-Hylum-
Wood is 5 MS-Concrete-Fiber Glass is 8MS-Fiber Glass-
Brick is 7.3&MS-Wood-Fiber Glass is 7.5
5) The study shows that Heat flux of composite material
MS-Hylum-Wood is 70.08 MS-Concrete-Fiber Glass is
113.31 MS-Fiber Glass-Brick is 103.39&MS-Wood-Fiber
Glass is 106.23
6) The temperature distribution of MS-Hylum-Wood is
23.05 MS-Concrete-Fiber Glass is 370.2MS-Fiber Glass-
Brick is 29.49&MS-Wood-Fiber Glass is 32.05
7) It is seen that the Finite element method (FEM) can be
gainfully employed for determination of thermal
behavior like heat flux, heat flow rate and temperature
distribution of all composite walls.
8) Then it can be concluded that the composite MS-Hylum-
Wood shows lower heat flux, temperature distribution,
heat flow rate and thermal conductivity values than that
of the other compositeslikeMS-Concrete-FiberGlass,MS-
Fiber Glass-Brick &MS-Wood-Fiber Glass respectively.
9. ACKNOWLEDGEMENT:-
Author is thankful to the Department of Mechanical
Engineering of RKDF IST Bhopal for his invaluable guidance
and support
10. REFERENCES:-
[1] AbdulazizAlmujahid, ZakariyaKaneesamkandi,
“Construction Of A TestRoom For Evaluating Thermal
Performance Of Building Wall Systems Under Real
Conditions’’ IJIRSET Vol. 2, Issue 6, June
2013,pg.no.2000-2007.
[2] NavidEkrami, Anais Garat, Alan S. Fung, “Thermal
Analysis of Insulated Concrete Form (ICF) Walls”
Science Direct, Energy Procedia 75 ( 2015)pg.no.2150 –
2156.
[3] Sawankumar E. Patil,N. N. Shinde, “Theoretical
Analysis of Composite Roof with Respect to Comfort in
Building Envelope” Current Trends in Technology and
Science ISSN: 2279-0535. Volume: 3, Issue: 3 (Apr-May.
2014), pg.no.168-172.
[4]Dr.R.Uday Kumar, “Evaluation And Effect Of
Convective Resistance And Convective Heat Transfer
Coefficient On Heat Transfer Rate In Composite
Structure” IJAREST,Volume 3, Issue 10, October – 2016
pg no.81-85.
[5]Adel A. Abdouand Ismail M.Budaiwi,“Measurements
of Building Insulation Materials under Various
Operating Temperatures”, Journal of BUILDING
PHYSICS, 29(2), p.171, 2005.
[6] Amjed, A. Maghrabi, “Comparative Study of Thermal
Insulation Alternatives for Building Walls and Roofs in
Makkah, Saudi Arabia”, Journal of Sci. Med. Eng., 17(2),
pp.273 -287, 2005.
[7] Bjorn PetterJelle, “Traditional, state-of-the-art and
future thermal building insulation materials and
solutions-Properties, requirements and possibilities”,
Energy and Buildings, 43,pp. 2549–2563, 2011.
[8] Cabeza, L.F., Castell, A., Medrano, M., Martorell, I.,
Perez, G.and Fernandez I, “Experimental study on the
performance of insulation materials in Mediterranean
construction”, Energy and Buildings, 42, pp.630–636,
2010. [5] Eoghan Frawley andDavidKennedy,“Thermal
Testing of Building Insulation Materials”, Engineers
Journal, I (61) 9, 2007.

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IRJET- Thermal Analysis of Heat Transfer through Composite Wall by using F.E.A. Method

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1882 THERMAL ANALYSIS OF HEAT TRANSFER THROUGH COMPOSITE WALL BY USING F.E.A. METHOD Bhangale Bhushan Suresh1, Dr.M.K.Chopra2 1PG Student, Department of Mechanical Engineering, RKDF IST, Bhopal, MP, India 2Vice Principal & HOD Department of Mechanical Engineering, RKDF IST, Bhopal, MP, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - It is very difficult to calculate and analyze with precision the thermal behavior of the walls of different materials attached to each other. The study of composite materials thermal behavior is useful for the determination of heat flux, temperature distribution, heatflowrateandthermal conductivity. These composite materials which can be implemented to many applications such as thermal ventilations, Insulators, metallic multiwall thermal protection systems, etc. In this study we are going to analyze the thermal behavior of four composites. For finding heat flux, temperature distribution, heat flow rate and thermal conductivity the finite element program method ANSYS is used. The experimental test is carried out for heat flux, temperature distribution, heat flow rate and thermal conductivity of composite materials. Experimental Results are compared with thefiniteelement ANSYS results and the validation is done. KeyWords:Thermal Conductivity,Composite Materials, Heat Flux, Conduction, Heat Flow Rate 1. INTRODUCTION:- The Study of composites is a philosophy of material design that allows for the optimum material compositionalongwith structural design and optimization in one concurrent and interactive process. The scope of composite materials research and technology consists of Investigation of basic characteristics of the constituent and composite materials, Material optimization for given service conditions, Development of effective and efficient fabrication procedures and understanding of their effect on material properties. 1.1 Heat Transfer:- The amount of heat transferred per unit time is called heat transfer rate and is denoted by Q. The heat transfer rate has unit J/s which is equivalent to Watt. When the rate of heat transfer Q is available, then total amount of heat energy transferred ∆U during a time interval ∆ t can be obtained form, (Joule) The rate of heat transfer per unit area normal to the direction of heat flow is called heat flux and is expressed as, q=Q/A. 2. OBJECTIVE OF WORK:- The main objective of the presentresearchwork istodevelop composite structure and to find the thermal behavior of that composite using Finite Element method, analytical method and Experimental method Analytical method has been performed to obtain the relative values of temperature, heat flow rate and heat flux. After Analytical method, Experimental method has been performed to obtain the relative values of temperature, heat flux, heat flow rate and thermal conductivity. After analytical and experimental method, Finite Element Analysis has been performed to obtain the relative values of temperature, heat flow rate, heat flux and thermal conductivity. Finally a comparative study has been made between Finite Element Method and Experimental method. 3. METHODOLOGY:- The experimental set up consists of three disks of equal diameters but variable thickness arranged to form a slab of same diameter and the heater ware placed at one side of composite wall. Three types of slabs are provided on heater which forms a composite structure. Composition of materials: 1. MS-Hylum-wood 2. MS-Concrete-Fiber 3. MS-Fiber Glass-Brick 4. MS-Wood-Fiber Glass
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1883 Specifications: Plate Dimensions: Materials Diameter (mm) Thickness (mm) MS 300 25 Fiber glass 300 20 Hylum 300 20 Wood 300 15 Brick 300 15 Concrete 300 15 4. MATHEMATICAL MODELING:- The mathematical modelling is the idealization of the physical problems until defined set of (mathematical) constraints, representing the main features is established. Mathematical modeling is required not only in analytical work but also in actual heat- transfer practice, where a large commercial computer package is used. Table 4.1:-MS-Hylum-Wood T1 T2 T3 T4 Q (W) q (W/m2) 100 99.97 38.05 22.86 3.7202 52.6311 150 149.96 48.34 23.42 6.1050 86.3690 200 199.95 58.64 23.99 8.4898 120.106 Table 4.2:- MS-Concrete-Fiber Glass T1 T2 T3 T4 Q (W) q (W/m2) 100 99.95 96.86 36.27 7.8519 111.08 150 149.92 144.85 45.42 12.885 182.28 200 199.89 192.84 54.57 17.918 253.49 Table 4.3:- MS-Fiber Glass-Brick T1 T2 T3 T4 Q (W) q (W/m2) 100 99.95 28.49 27.11 6.945 98.2562 150 149.93 32.66 30.39 11.397 161.24 200 199.90 36.82 33.67 15.849 224.225 Table 4.4:- MS-Wood-Fiber Glass T1 T2 T3 T4 Q (W) q (W/m2) 100 99.96 71.63 31.45 5.206 73.653 150 149.95 103.46 37.53 8.5435 120.86 200 199.93 135.28 43.60 11.88 168.08 5. EXPERIMENTATION:- A composite slab consists of slab of three different materials which are MS, Hylum, & wood for one composite. There are such four composites of different materials. Slabs & heating element are circular in cross section. The instrument consists of three disks of equal diameters but variable thickness arranged to form a slab. The set up consists of a heater placed at one side of composite wall. Experimental Result Table for Temperature Distribution:- Table 5.1:-MS-Hylum-Wood Sr. No. Temperature Q (W) q (W/m2) K (W/m0c) 1 100 5 70.82 0.0544 2 150 7.5 106.23 0.0497 3 200 9.0 127.47 0.0429 Table 5.2:- MS-Concrete-Fiber Glass Sr. No. Temperature Q (W) q (W/m2) K (W/m0c) 1 100 8 113.31 0.0871 2 150 14 198.30 0.0929 3 200 18.6 263.45 0.0888 Table 5.3:- MS-Fiber Glass-Brick Sr. No. TemperatureQ (W) q (W/m2) K (W/m0c) 1 100 7.3 103.39 0.0795 2 150 12.6 178.47 0.0836 3 200 16.8 237.96 0.0802 Table 3.1:- Plate Dimensions
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1884 Table 5.4:- MS-Wood-Fiber Glass Sr. No. Temperature Q(w) q (W/m2) K (W/m0c) 1 100 7.5 106.23 0.0817 2 150 9.5 134.56 0.0630 3 200 14 198.30 0.0668 Experimental Result Table for Directional Heat Flux:- Table 5.5 Directional Heat Flux Temperature (0C) MS-F-GB MS-H- W MS-C-FG MS-W- FG 100 103.39 70.8 113.31 106.23 150 178.47 106.23 198.3 134.56 200 237.96 127.47 263.45 198.3 Experimental Result Table for Heat Flow Rate:- Table 5.6 Heat Flow Rate Temperature (0C) MS-F-GB MS-H-W MS-C-FG MS-W- FG 100 7.3 5 8 7.5 150 12.6 7.5 14 9.5 200 16.8 9 18.6 14 Experimental Result Table for Thermal Conductivity:- Table5.7 Thermal Conductivity Temperature (0C) MS-F-GB MS-H-W MS-C-FG MS-W- FG 100 0.0795 0.0544 0.0871 0.0817 150 0.0836 0.0497 0.0929 0.063 200 0.0802 0.0429 0.0888 0.0668 6. FINITE ELEMENT ANALYSIS:- The finite element method is a numerical analysis technique for obtaining approximate solutions to a wide variety of engineering problems. Because of its diversity and flexibility as an analysis tool, it is receiving much attention in engineering schools and in industries. In more and more engineering situations today, we find that it is necessary to obtain approximate numerical solutions to problems rather than exact closed form solution. ANSYS Result table for Temperature Distribution:- Table 6.1 Temperature Distribution at 1000c Materials T1 T2 T3 T4 MS-F-GB 100 99.95 28.49 27.12 MS-H-W 100 99.97 38.05 22.88 MS-C-FG 100 99.95 96.86 36.25 MS-W-FG 100 99.96 71.63 31.6 Table 6.2 Temperature Distribution at 1500c Materials T1 T2 T3 T4 MS-F-GB 150 149.93 32.66 30.39 MS-H-W 150 149.96 48.34 23.45 MS-C-FG 150 149.92 144.85 45.42 MS-W-FG 150 149.95 103.46 37.82 Table 6.3 Temperature Distribution at 2000c Materials T1 T2 T3 T4 MS-F-GB 200 199.9 36.82 33.67 MS-H-W 200 199.95 58.64 24.01 MS-C-FG 200 199.89 192.84 54.54 MS-W-FG 200 199.93 135.28 44.01 ANSYS Result table for Directional Heat Flux:- Table 6.4 Directional Heat Flux Temperature (0C) MS-F- GB MS-H-W MS-C-FG MS-W- FG 100 98.25 52.63 111.08 73.65 150 161.24 86.36 182.28 120.86 200 224.225 120.106 253.49 168.08
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1885 ANSYS Result table for Heat Flow Rate:- Table 6.5 Heat Flow Rate Temperature (0C) MS-F-GB MS-H-W MS-C-FG MS-W- FG 100 6.945 3.7602 7.8519 5.3114 150 11.397 6.1706 12.885 8.7162 200 15.85 8.5802 17.919 12.121 7. Graphical Results:- Graphical Experimental Results of Materials Vs Heat Flux for all Composite Materials:- 0 50 100 150 200 250 300 MS-F-GB MS-H-W MS-C-FG MS-W-FG HEATFLUX MATERIAL MATERIAL Vs HEAT FLUX 100 150 200 Graph 7.1 Materials Vs Heat Flux Graphical Experimental Results of Materials Vs Heat Flow Rate for all Composite Materials:- Graph 7.2 Materials Vs Heat Flow Rate Graphical Experimental Result of Materials Vs Thermal Conductivity for all Composite Materials:- 0 0.02 0.04 0.06 0.08 0.1 MS-F-GB MS-H-W MS-C-FG MS-W-FG ThermalConductivity Material Material VsThermal Conductivity 100 150 200 Graph 7.3 Materials Vs Thermal conductivity Graphical ANSYS Results of Materials Vs Heat Flux for all Composite Materials:- Graph 7.4 Materials Vs Heat Flux Graphical ANSYS Results of Materials Vs Heat Flow rate for all Composite Materials:- Graph 6.5 Materials Vs Heat Flow Rate
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1886 8. CONCLUSIONS Based on the analytical, finite element and experimental investigation on the thermal behavior of different composites, it can be concluded that: 1) The results obtained from the proposed analytical method are in close approximation with the values obtained by FEM simulation using ANSYS. 2) The values obtained from the proposed analytical method are in close approximation with the values obtained from experimental values. 3) The study shows that the thermal conductivity of the composite material MS-Concrete-Fiber Glass is 0.0871MS-Fiber Glass-Brick is 0.0795 MS-Wood-Fiber Glass is 0.0817 &MS-Hylum-Wood is 0.0544 4) The study shows that the heat flow rate MS-Hylum- Wood is 5 MS-Concrete-Fiber Glass is 8MS-Fiber Glass- Brick is 7.3&MS-Wood-Fiber Glass is 7.5 5) The study shows that Heat flux of composite material MS-Hylum-Wood is 70.08 MS-Concrete-Fiber Glass is 113.31 MS-Fiber Glass-Brick is 103.39&MS-Wood-Fiber Glass is 106.23 6) The temperature distribution of MS-Hylum-Wood is 23.05 MS-Concrete-Fiber Glass is 370.2MS-Fiber Glass- Brick is 29.49&MS-Wood-Fiber Glass is 32.05 7) It is seen that the Finite element method (FEM) can be gainfully employed for determination of thermal behavior like heat flux, heat flow rate and temperature distribution of all composite walls. 8) Then it can be concluded that the composite MS-Hylum- Wood shows lower heat flux, temperature distribution, heat flow rate and thermal conductivity values than that of the other compositeslikeMS-Concrete-FiberGlass,MS- Fiber Glass-Brick &MS-Wood-Fiber Glass respectively. 9. ACKNOWLEDGEMENT:- Author is thankful to the Department of Mechanical Engineering of RKDF IST Bhopal for his invaluable guidance and support 10. REFERENCES:- [1] AbdulazizAlmujahid, ZakariyaKaneesamkandi, “Construction Of A TestRoom For Evaluating Thermal Performance Of Building Wall Systems Under Real Conditions’’ IJIRSET Vol. 2, Issue 6, June 2013,pg.no.2000-2007. [2] NavidEkrami, Anais Garat, Alan S. Fung, “Thermal Analysis of Insulated Concrete Form (ICF) Walls” Science Direct, Energy Procedia 75 ( 2015)pg.no.2150 – 2156. [3] Sawankumar E. Patil,N. N. Shinde, “Theoretical Analysis of Composite Roof with Respect to Comfort in Building Envelope” Current Trends in Technology and Science ISSN: 2279-0535. Volume: 3, Issue: 3 (Apr-May. 2014), pg.no.168-172. [4]Dr.R.Uday Kumar, “Evaluation And Effect Of Convective Resistance And Convective Heat Transfer Coefficient On Heat Transfer Rate In Composite Structure” IJAREST,Volume 3, Issue 10, October – 2016 pg no.81-85. [5]Adel A. Abdouand Ismail M.Budaiwi,“Measurements of Building Insulation Materials under Various Operating Temperatures”, Journal of BUILDING PHYSICS, 29(2), p.171, 2005. [6] Amjed, A. Maghrabi, “Comparative Study of Thermal Insulation Alternatives for Building Walls and Roofs in Makkah, Saudi Arabia”, Journal of Sci. Med. Eng., 17(2), pp.273 -287, 2005. [7] Bjorn PetterJelle, “Traditional, state-of-the-art and future thermal building insulation materials and solutions-Properties, requirements and possibilities”, Energy and Buildings, 43,pp. 2549–2563, 2011. [8] Cabeza, L.F., Castell, A., Medrano, M., Martorell, I., Perez, G.and Fernandez I, “Experimental study on the performance of insulation materials in Mediterranean construction”, Energy and Buildings, 42, pp.630–636, 2010. [5] Eoghan Frawley andDavidKennedy,“Thermal Testing of Building Insulation Materials”, Engineers Journal, I (61) 9, 2007.