International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8109
COMPUTATIONAL FLUID DYNAMIC ANALYSIS OF WAX MELTING
S.Rajkumar1, P.Venugopal2, P.Vinoth kumar3 , M.Tamilvanan4,R.Vishnukumar5.
1Assistant Professor, Department of Mechanical Engineering, KSR Institute for Engineering and Technology,
Tiruchengode.
2UG Scholar, Department of Mechanical Engineering, KSR Institute for Engineering and Technology,
Tiruchengode.
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - In the present numerical study and analysis a
three dimensional sphere with hallow section is considered as
test section. The grid independent test and time independent
test are performed and chosen the appropriate grid size for
numerical study. The diameterofhallowsectionofsphereis 84
mm. The aluminium wall thickness is 1 mm. The isothermal
boundary condition is taken for numerical simulation. The
three different PCMs (Paraffin wax, Sodium acetate tri-
hydrate and Lauric acid) are tested for energy storageandfor
performance analysis. TheenergystoredbyPCMsiscompared.
The melt fraction contour and temperature contour are also
analysed at different time of simulation.
Key Words: (Evacuate tube; Phase Change Material;
Paraffin Wax; Melting Process.)
1.INTRODUCTION
In the modern world with improved lifestyle the energy
demands of human beings have increased. We all know that
our conventional energy resources (fossil fuels) are limited
in quantity and are being used up at higher rate. The use of
fossil fuels such as coal, petroleum poses a large number of
problems due to their high cost, emission of greenhouse
gases (GHGs) and oil security. So it becomes important to
conserve these fossil fuels and to protect our environment
from the harmful effects of environmental pollution. We all
know that most of our fossil fuels are used in power plant
and transportation sector, which are not much efficient in
terms of energy use. There are huge amount of energylosses
in these systems. Most of these energy losses are in the form
of heat loss. If we take the example of an automobile about
30-40% of the energy produced by burning fuel is lost as
waste heat, which reduces the range of automobile. Also we
have HVAC systems in our automobile. A heating system of
about 5kW is used in i-MiEV of MITSUBISHI Motors. This
excess need of energy reduces the driving range of such
vehicles by about 10-65%. So it becomes importanttodothe
proper thermal management of such systems to increase
their efficiency which can help us in achieving our goal of
conserving fossil fuels and protecting the environment. The
use of thermal energy storage (TES) systems is an emerging
technology used nowadays for thermal management. These
systems are designed to store thermal energy. This can be
done with various modes such as by storing it as sensible
heat, latent heat and thermochemical process. The latent
heat storage (LHS) system makes the use of Phase Change
Materials (PCMs) for thermal energy storage.
1.2 Phase change material
PCMs are the materials which are used for storing latent
heat energy. These are the materials which changes its one
state to another when heat energy is supplied or extracted
away from them. They can change from solid to liquid state
by absorbing latent heat of fusion and vice versa or they can
change their state from liquid to gaseous byabsorbinglatent
heat to vaporization and vice versa or they can change their
state from solid to gaseous by absorbing latent heat of
sublimation and vice versa at constant temperature. The
solid to liquid phase change mode is most widely used for
LHS. The fig -1 shows the phenomenon of phase change for
solid to liquid phase change mode. The shaded regionshows
the total heat energy stored during phase change of a
material from solid to liquid. The total energy stored is the
sum of sensible heat in solid state, latent heat during phase
change at constant temperature and sensible heat in liquid
state.
Fig- 1: Heat storage during phase change of material
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8110
2.THERMO-PHYSICAL PROPERTIES OF PARAFFIN
WAX
Table 2.1:Thermo-physical properties of paraffin wax
Property Value
Density (kg/m3) 870 at T =300k
780 at T =340k
Specific heat (J/Kgk) 2900
Thermal conductivity
(W/mk)
0.24 at T =300k
0.22 at T =340k
Viscosity (Ns/m) 0.0057933
Latent heat (J/Kg) 190000
Solidus temperature (k) 331
Liquidus temperature (k) 3318
3.MATERIAL SELECTION
Paraffin waxes come directly from the vacuum distillationof
petroleum crude. Paraffin waxes can be refined, formulated,
modified with additives and are offered in packaged slabs,
powder, chips, etc. Petroleum crudeistherawmaterial used
to obtain paraffin waxes among other derivatives.
The other hydrocarbons can also be found within its
composition:
• Normal & Branched Paraffin’s
• Naphthenic
• Aromatic
Paraffin waxes are made up of a blend of saturated
hydrocarbons (alkenes) with a chainlengthfromC20toC60.
Depending on the structural shape of the chain, two
different types of paraffin exist
• Linear Paraffin Wax.
• Branched Paraffin Wax.
Table 3.1: Properties of Paraffin Wax
Levels of Refinement Oil Content (% of
weight)
Fully Refined <1
Semi Refined 1-3
Petrolatum  3
Macrocrystallin
e
Microcrystallin
e
Melt Point Medium(50-
70 )
High(70-90 )
MolecularWeig
ht
MediumC19-
C42
HighC25->C50
Crystals Large and
regular
Small &
Irregular
Flexibility Low High
Aspect Brilliat Opaque
3.1 LIST OF COMPONENTS
3.3.1 PARAFFIN WAX
Paraffin wax is a soft colourless solid, derived
from petroleum, coal or shale oil, that consists of a mixture
of hydrocarbon molecules containing between twenty and
forty carbon atoms. It is solid at room temperature
and begins to melt aboveapproximately37 °C(99 °F)and its
boiling point is >370 °C (698 °F).
THE GENERAL FORMULA
PARAFFIN WAX : CnH2n+2.
PROPERTIES
• It is mostly found as tasteless, odourless and waxy
solid.
• It ismelting point is 46 and 68o C (115 and 154oF).
• Paraffin wax is an excellent material for storing
heat, with a specific heat capacity of 2.14–
2.9 J g−1 K−1.
• And its heat of fusion is 200–220 J g−1.
3.1.2 ALUMINIUM
Aluminium or aluminiumisa chemical elementwith
symbol AI and atomic number 13. It is a silvery-white, soft,
nonmagnetic and ductile metal in the boron group.
aluminium makes up about 8% of the Earth's crust. The
chief ore of aluminium is bauxite. it is found combined in
over 270 different minerals.
PROPERTIES
• Density of aluminium is 2700 kg/m3.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8111
• Melting point of aluminium is 660oC.
• Thermal conductivity of aluminium is 204
W/mk.
• Specific heat capacity of aluminium is 940
J/kg oC.
3.3.3 EVACUATED TUBE
Evacuated Tubes are the heart of the Apricus AP
solar collector, responsible for absorbing sunlight and
converting it into usable heat. Tube Design. The tube is
essentially two glass tubes that are fused at the top and
bottom. The inner tube has a solar absorbing coating, and
the space between the two tubes is evacuated to form a
vacuum.
PROPERTIES
• They have normal reflective of 0.04.
• The maximum temperature upto 430oC.
• The outer and the inner emisivity of
evacuated tube is 0.9 and 0.35.
Sample paragraph Define abbreviations and acronyms the
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defined in the abstract. Abbreviations such as IEEE, SI, MKS,
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abbreviations in the title or heads unless they are
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4. 3D MODELING
CREATING 3D MODEL BY USING CREO SOFTWARE
By draw the hollow sphere for using some commends in
creo software
List below,
Circle, extrude and assemble
Fig 5.1 Isometric view
Fig 5.2 Front view
Fig 5.3 Side view
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8112
5.RESULT AND CALCULATION
5.1:Time interval 150 seconds
FIG:5.1 temperature distribution
FIG:5.2 mass fraction
FIG:5.3 net result
Thefigureshowsthetemperaturedistribution
over the entire length of the pipe that is obtained in a
time interval of 150 seconds. The variations in
temperature at various layers of the pipe were shown
above. It is seen that the temperature at outer wall is
maximum and the heat is gradually transfered to the
center fluid.
The volume of the phase change material is
0.84199585 m3 and it is the net volume of the material. And
the inlet and outlet temperature of the liquid is 300 k and
315.83737 k respectively. And the inlet and outlet
temperatureof the phasechangematerialis507.68057kand
509.10217 k respectively. . And net temperature during 250
second is 451.21429 k.
5.2:Time interval 200 seconds
FIG:5.4 mass fraction
FIG:5.5 temperature distribution
FIG:5.6 net result
Thefigureshowsthetemperaturedistribution
over the entire length of the pipe that is obtained in a
time interval of 200 seconds. The variations in
temperature at various layers of the pipe were shown
above. It is seen that the temperature at outer wall is
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8113
maximum and the heat is gradually transfered to the
center fluid.
The volume of the phase change material is
0.7608106 m3 and it is the net volume of the material. And
the inlet and outlet temperature of the liquid is 300 k and
315.13235 k respectively. And the inlet and outlet
temperature of the phase change material is 506.15582 k
and 507.64978 k respectively. . And net temperatureduring
200 second is 450.04974k.
5.3 Time interval 250 seconds
FIG:5.7 mass fraction
FIG:5.1 temperature distribution
FIG:5.9 net result
Thefigureshowsthetemperaturedistribution
over the entire length of the pipe that is obtained in a
time interval of 250 seconds. The variations in
temperature at various layers of the pipe were shown
above. It is seen that the temperature at outer wall is
maximum and the heat is gradually transfered to the
center fluid.
The volume of the phase change material is
0.68081147 m3 and it is the net volume of the material. And
the inlet and outlet temperature of the liquid is 300 k and
314.70621 k respectively. And the inlet and outlet
temperatureof the phasechangematerialis503.02301kand
506.36932 k respectively. And net temperature during 250
second is 448.41171 k.
5.4 CALCULATIONS
5.4.1 Heat transfer
diameter of inner aluminium plate d1=35mm ,
r1=17.5mm =0.0175m
diameter of outer aluminium plate d2=36mm,
r2=18mm =0.018m
diameter of inner evacuated tube d3=84mm,
r3=42mm =0.042m
diameter of outer evacuated tube d4=85mm,
r4=42.5mm=0.0425m
aluminium thermal conductivity k1=204w/mk
paraffin wax thermal conductivity k2=0.24w/mk
evacuated tube thermal conductivity k3=1w/mk
outer temperature Tb=393.1k
inner temperature Ta=509.4k
heat transfer
Q = Toverall/R
T= ta-tb
=509.4-393.1
T =116.3K
[refer hmt data book pg.no.43&45]
R=1/2 l[ln(r2/r1)/k1+ln(r3/r2)/k2+ln(r4/r3)/k3]
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8114
=1/2 (0.5)[ln(0.018/0.017)/204+ln(0.042/0.018)/0.24+
ln(0.043
/0.042)/1]
R= 1/2 l[0.00028+3.5+1.012]
For l=500mm, l=0.5m.
=1/2 (0.5)[4.51228]
=1.4363mk/W
Q=Ta-Tb/R
=(509.4-393.1)/1.4363
Q =80.97W/m
5.4.2 AREA
A=2 rl
Area of inner sphere (aluminium)
A=2 rl
=2 (17.5)(500)
=54.977x103mm
Area of outer sphere(aluminium)
A1=2 rl
=2 (18)(500)
=56.548x103mm
Area of inner sphere(evacuated tube)
A2=2 rl
=2 (42)(500)
=131.946x103mm
For the area of evacuated tube is
A3=A2-A1
=131.946x103-56.548x103
A3 =75.398x103mm
5.4.3VOLUME
/3
Volume of water
/3
V = 22.449x103mm3
For reducing aluminium thickness
V1 /3
= 24.429x103mm3
Volume of paraffin wax
V2= /3
= 310.339x103mm3
For get volume of paraffin wax
V=V2-V3
= (310.339X103)-(24.429X103)
V = 285.91X103mm3
6.CONCLUSION
In this numerical work, melting of paraffin wax to
achieve the vaporization of water in by low cost when
comparing another glycolic acid like Sodium acetate tri-
hydrate and Lauric acid.
Paraffin wax is phase change material to transfer
the heat. And the heat transfer rate is Q =80.97W/m.
It have thermal conductivity of 0.24 W/mk at the
temperature of 300K.
Temperature distribution curve is change in after
addition of 50s.
7. REFERANCE
[1] A. Hasan, Phase change material energy
storage system employing palmitic acid, Solar
Energy 1994, pp143–154.
[2] B. Gibbs and S. Hasnain, DSC study of
technical grade phase change heat storage
materials for solar heating applications. In:
Proceedings of the 1995 ASME/JSME/JSEJ
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8115
International Solar Energy Conference, Part 2,
1995.
[3] G. A Lane. Encapsulation of heat of fusion
storage materials. In: Proceedings of 2nd
Southeastern Conference on Application of Solar
Energy,p.442–50.1976.
[4] G. A. Lane. Low temperature heatstoragewith
phase change materials. Int J Ambient Energy;
1:155–68. 1980.
[5] Y. Hong, G. Xin-shi, Preparation of
polyethylene–paraffincompoundsasa form-stable
solid–liquid phase change material. Solar Energy
Mater Solar Sells 2000; 64:37–44.
[6] Z.Gu, H. Liu, Y. Li, Thermal energy recovery
heat recovery system calculation and phase
change material development. Applied Thermal
Engineering 24: (2004) 2511–2426.
[7] H. Hong, S. K. Kim, Y. S. Kim, Accuracy
improvement of t-history method for measuring
heat of fusion of various materials. International
Journal of Refrigeration 27: (2004) 360–366.
[8] J. P. Trelles, J. P. Duffy, Numerical simulation
of porous latent heat thermal energy storage for
thermoelectric cooling. Applied Thermal
Engineering 23: (2003) 1647–1664.
[9] M.Ravikumar,P.S.S.Srinivasan,Phasechange
material as a thermal energy storage material for
cooling of building, Journal of Theoretical and
Applied Information Technology (2005) 503-512.
[10] A. Felix Regin, S. C. Solanki, J. S. Saini, An
analysis ofa packed bedlatentheatthermal energy
storage system using PCM capsules: Numerical
investigation, Renewable Energy 34 (2009)1765–
1773.
[11] A. Mahmud, K. Sopian, M. Alghoul A. Mat
Sohif, Using a Paraffin wax- Aluminum compound
as a thermal storage material in a solar air heater,
ARPN Journal of Engineering andAppliedSciences,
vol. 4, no. 10, December2009.
[12] F. demirbas, Thermal Energy Storage and
Phase Change Materials: An Overview, Energy
Sources, Part B, 1:85–95, 2006.
[13] N. A. Mohd Amin, Martin Belusko, Frank
Bruno, Optimisation of A Phase Change Thermal
Storage System, World Academy of Science,
Engineering and Technology 56 (2009).
[14] S. A. Karaipekli, Thermal conductivity and
latent heat thermal energy storage characteristics
of paraffin/expanded graphite compositeasphase
change material, Applied Thermal Engineering,
Volume27,Issues8-9,June2007,Pages1271-1277.
[15] Z. Zhang, X. Fang, Study on
paraffin/expanded graphite composite phase
change thermal energy storage material , Energy
Conversion and Management, Volume 47, Issue 3,
February 12006, Pages 303-310.

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LOW POWER CLASS AB SI POWER AMPLIFIER FOR WIRELESS MEDICAL SENSOR NETWORK

IRJET- Computational Fluid Dynamic Analysis of Wax Melting

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8109 COMPUTATIONAL FLUID DYNAMIC ANALYSIS OF WAX MELTING S.Rajkumar1, P.Venugopal2, P.Vinoth kumar3 , M.Tamilvanan4,R.Vishnukumar5. 1Assistant Professor, Department of Mechanical Engineering, KSR Institute for Engineering and Technology, Tiruchengode. 2UG Scholar, Department of Mechanical Engineering, KSR Institute for Engineering and Technology, Tiruchengode. ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - In the present numerical study and analysis a three dimensional sphere with hallow section is considered as test section. The grid independent test and time independent test are performed and chosen the appropriate grid size for numerical study. The diameterofhallowsectionofsphereis 84 mm. The aluminium wall thickness is 1 mm. The isothermal boundary condition is taken for numerical simulation. The three different PCMs (Paraffin wax, Sodium acetate tri- hydrate and Lauric acid) are tested for energy storageandfor performance analysis. TheenergystoredbyPCMsiscompared. The melt fraction contour and temperature contour are also analysed at different time of simulation. Key Words: (Evacuate tube; Phase Change Material; Paraffin Wax; Melting Process.) 1.INTRODUCTION In the modern world with improved lifestyle the energy demands of human beings have increased. We all know that our conventional energy resources (fossil fuels) are limited in quantity and are being used up at higher rate. The use of fossil fuels such as coal, petroleum poses a large number of problems due to their high cost, emission of greenhouse gases (GHGs) and oil security. So it becomes important to conserve these fossil fuels and to protect our environment from the harmful effects of environmental pollution. We all know that most of our fossil fuels are used in power plant and transportation sector, which are not much efficient in terms of energy use. There are huge amount of energylosses in these systems. Most of these energy losses are in the form of heat loss. If we take the example of an automobile about 30-40% of the energy produced by burning fuel is lost as waste heat, which reduces the range of automobile. Also we have HVAC systems in our automobile. A heating system of about 5kW is used in i-MiEV of MITSUBISHI Motors. This excess need of energy reduces the driving range of such vehicles by about 10-65%. So it becomes importanttodothe proper thermal management of such systems to increase their efficiency which can help us in achieving our goal of conserving fossil fuels and protecting the environment. The use of thermal energy storage (TES) systems is an emerging technology used nowadays for thermal management. These systems are designed to store thermal energy. This can be done with various modes such as by storing it as sensible heat, latent heat and thermochemical process. The latent heat storage (LHS) system makes the use of Phase Change Materials (PCMs) for thermal energy storage. 1.2 Phase change material PCMs are the materials which are used for storing latent heat energy. These are the materials which changes its one state to another when heat energy is supplied or extracted away from them. They can change from solid to liquid state by absorbing latent heat of fusion and vice versa or they can change their state from liquid to gaseous byabsorbinglatent heat to vaporization and vice versa or they can change their state from solid to gaseous by absorbing latent heat of sublimation and vice versa at constant temperature. The solid to liquid phase change mode is most widely used for LHS. The fig -1 shows the phenomenon of phase change for solid to liquid phase change mode. The shaded regionshows the total heat energy stored during phase change of a material from solid to liquid. The total energy stored is the sum of sensible heat in solid state, latent heat during phase change at constant temperature and sensible heat in liquid state. Fig- 1: Heat storage during phase change of material
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8110 2.THERMO-PHYSICAL PROPERTIES OF PARAFFIN WAX Table 2.1:Thermo-physical properties of paraffin wax Property Value Density (kg/m3) 870 at T =300k 780 at T =340k Specific heat (J/Kgk) 2900 Thermal conductivity (W/mk) 0.24 at T =300k 0.22 at T =340k Viscosity (Ns/m) 0.0057933 Latent heat (J/Kg) 190000 Solidus temperature (k) 331 Liquidus temperature (k) 3318 3.MATERIAL SELECTION Paraffin waxes come directly from the vacuum distillationof petroleum crude. Paraffin waxes can be refined, formulated, modified with additives and are offered in packaged slabs, powder, chips, etc. Petroleum crudeistherawmaterial used to obtain paraffin waxes among other derivatives. The other hydrocarbons can also be found within its composition: • Normal & Branched Paraffin’s • Naphthenic • Aromatic Paraffin waxes are made up of a blend of saturated hydrocarbons (alkenes) with a chainlengthfromC20toC60. Depending on the structural shape of the chain, two different types of paraffin exist • Linear Paraffin Wax. • Branched Paraffin Wax. Table 3.1: Properties of Paraffin Wax Levels of Refinement Oil Content (% of weight) Fully Refined <1 Semi Refined 1-3 Petrolatum  3 Macrocrystallin e Microcrystallin e Melt Point Medium(50- 70 ) High(70-90 ) MolecularWeig ht MediumC19- C42 HighC25->C50 Crystals Large and regular Small & Irregular Flexibility Low High Aspect Brilliat Opaque 3.1 LIST OF COMPONENTS 3.3.1 PARAFFIN WAX Paraffin wax is a soft colourless solid, derived from petroleum, coal or shale oil, that consists of a mixture of hydrocarbon molecules containing between twenty and forty carbon atoms. It is solid at room temperature and begins to melt aboveapproximately37 °C(99 °F)and its boiling point is >370 °C (698 °F). THE GENERAL FORMULA PARAFFIN WAX : CnH2n+2. PROPERTIES • It is mostly found as tasteless, odourless and waxy solid. • It ismelting point is 46 and 68o C (115 and 154oF). • Paraffin wax is an excellent material for storing heat, with a specific heat capacity of 2.14– 2.9 J g−1 K−1. • And its heat of fusion is 200–220 J g−1. 3.1.2 ALUMINIUM Aluminium or aluminiumisa chemical elementwith symbol AI and atomic number 13. It is a silvery-white, soft, nonmagnetic and ductile metal in the boron group. aluminium makes up about 8% of the Earth's crust. The chief ore of aluminium is bauxite. it is found combined in over 270 different minerals. PROPERTIES • Density of aluminium is 2700 kg/m3.
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8111 • Melting point of aluminium is 660oC. • Thermal conductivity of aluminium is 204 W/mk. • Specific heat capacity of aluminium is 940 J/kg oC. 3.3.3 EVACUATED TUBE Evacuated Tubes are the heart of the Apricus AP solar collector, responsible for absorbing sunlight and converting it into usable heat. Tube Design. The tube is essentially two glass tubes that are fused at the top and bottom. The inner tube has a solar absorbing coating, and the space between the two tubes is evacuated to form a vacuum. PROPERTIES • They have normal reflective of 0.04. • The maximum temperature upto 430oC. • The outer and the inner emisivity of evacuated tube is 0.9 and 0.35. Sample paragraph Define abbreviations and acronyms the first time they are used in the text, even after they have been defined in the abstract. Abbreviations such as IEEE, SI, MKS, CGS, sc, dc, and rms do not have to be defined. Do not use abbreviations in the title or heads unless they are unavoidable. After the text edit has been completed, the paper is ready for the template. Duplicate the template file by using the SaveAs command, andusethenamingconventionprescribedbyyour conference for the name of your paper. In this newly created file, highlight all of the contents and import your prepared text file. You are now ready to style your paper. 4. 3D MODELING CREATING 3D MODEL BY USING CREO SOFTWARE By draw the hollow sphere for using some commends in creo software List below, Circle, extrude and assemble Fig 5.1 Isometric view Fig 5.2 Front view Fig 5.3 Side view
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8112 5.RESULT AND CALCULATION 5.1:Time interval 150 seconds FIG:5.1 temperature distribution FIG:5.2 mass fraction FIG:5.3 net result Thefigureshowsthetemperaturedistribution over the entire length of the pipe that is obtained in a time interval of 150 seconds. The variations in temperature at various layers of the pipe were shown above. It is seen that the temperature at outer wall is maximum and the heat is gradually transfered to the center fluid. The volume of the phase change material is 0.84199585 m3 and it is the net volume of the material. And the inlet and outlet temperature of the liquid is 300 k and 315.83737 k respectively. And the inlet and outlet temperatureof the phasechangematerialis507.68057kand 509.10217 k respectively. . And net temperature during 250 second is 451.21429 k. 5.2:Time interval 200 seconds FIG:5.4 mass fraction FIG:5.5 temperature distribution FIG:5.6 net result Thefigureshowsthetemperaturedistribution over the entire length of the pipe that is obtained in a time interval of 200 seconds. The variations in temperature at various layers of the pipe were shown above. It is seen that the temperature at outer wall is
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8113 maximum and the heat is gradually transfered to the center fluid. The volume of the phase change material is 0.7608106 m3 and it is the net volume of the material. And the inlet and outlet temperature of the liquid is 300 k and 315.13235 k respectively. And the inlet and outlet temperature of the phase change material is 506.15582 k and 507.64978 k respectively. . And net temperatureduring 200 second is 450.04974k. 5.3 Time interval 250 seconds FIG:5.7 mass fraction FIG:5.1 temperature distribution FIG:5.9 net result Thefigureshowsthetemperaturedistribution over the entire length of the pipe that is obtained in a time interval of 250 seconds. The variations in temperature at various layers of the pipe were shown above. It is seen that the temperature at outer wall is maximum and the heat is gradually transfered to the center fluid. The volume of the phase change material is 0.68081147 m3 and it is the net volume of the material. And the inlet and outlet temperature of the liquid is 300 k and 314.70621 k respectively. And the inlet and outlet temperatureof the phasechangematerialis503.02301kand 506.36932 k respectively. And net temperature during 250 second is 448.41171 k. 5.4 CALCULATIONS 5.4.1 Heat transfer diameter of inner aluminium plate d1=35mm , r1=17.5mm =0.0175m diameter of outer aluminium plate d2=36mm, r2=18mm =0.018m diameter of inner evacuated tube d3=84mm, r3=42mm =0.042m diameter of outer evacuated tube d4=85mm, r4=42.5mm=0.0425m aluminium thermal conductivity k1=204w/mk paraffin wax thermal conductivity k2=0.24w/mk evacuated tube thermal conductivity k3=1w/mk outer temperature Tb=393.1k inner temperature Ta=509.4k heat transfer Q = Toverall/R T= ta-tb =509.4-393.1 T =116.3K [refer hmt data book pg.no.43&45] R=1/2 l[ln(r2/r1)/k1+ln(r3/r2)/k2+ln(r4/r3)/k3]
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8114 =1/2 (0.5)[ln(0.018/0.017)/204+ln(0.042/0.018)/0.24+ ln(0.043 /0.042)/1] R= 1/2 l[0.00028+3.5+1.012] For l=500mm, l=0.5m. =1/2 (0.5)[4.51228] =1.4363mk/W Q=Ta-Tb/R =(509.4-393.1)/1.4363 Q =80.97W/m 5.4.2 AREA A=2 rl Area of inner sphere (aluminium) A=2 rl =2 (17.5)(500) =54.977x103mm Area of outer sphere(aluminium) A1=2 rl =2 (18)(500) =56.548x103mm Area of inner sphere(evacuated tube) A2=2 rl =2 (42)(500) =131.946x103mm For the area of evacuated tube is A3=A2-A1 =131.946x103-56.548x103 A3 =75.398x103mm 5.4.3VOLUME /3 Volume of water /3 V = 22.449x103mm3 For reducing aluminium thickness V1 /3 = 24.429x103mm3 Volume of paraffin wax V2= /3 = 310.339x103mm3 For get volume of paraffin wax V=V2-V3 = (310.339X103)-(24.429X103) V = 285.91X103mm3 6.CONCLUSION In this numerical work, melting of paraffin wax to achieve the vaporization of water in by low cost when comparing another glycolic acid like Sodium acetate tri- hydrate and Lauric acid. Paraffin wax is phase change material to transfer the heat. And the heat transfer rate is Q =80.97W/m. It have thermal conductivity of 0.24 W/mk at the temperature of 300K. Temperature distribution curve is change in after addition of 50s. 7. REFERANCE [1] A. Hasan, Phase change material energy storage system employing palmitic acid, Solar Energy 1994, pp143–154. [2] B. Gibbs and S. Hasnain, DSC study of technical grade phase change heat storage materials for solar heating applications. In: Proceedings of the 1995 ASME/JSME/JSEJ
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 8115 International Solar Energy Conference, Part 2, 1995. [3] G. A Lane. Encapsulation of heat of fusion storage materials. In: Proceedings of 2nd Southeastern Conference on Application of Solar Energy,p.442–50.1976. [4] G. A. Lane. Low temperature heatstoragewith phase change materials. Int J Ambient Energy; 1:155–68. 1980. [5] Y. Hong, G. Xin-shi, Preparation of polyethylene–paraffincompoundsasa form-stable solid–liquid phase change material. Solar Energy Mater Solar Sells 2000; 64:37–44. [6] Z.Gu, H. Liu, Y. Li, Thermal energy recovery heat recovery system calculation and phase change material development. Applied Thermal Engineering 24: (2004) 2511–2426. [7] H. Hong, S. K. Kim, Y. S. Kim, Accuracy improvement of t-history method for measuring heat of fusion of various materials. International Journal of Refrigeration 27: (2004) 360–366. [8] J. P. Trelles, J. P. Duffy, Numerical simulation of porous latent heat thermal energy storage for thermoelectric cooling. Applied Thermal Engineering 23: (2003) 1647–1664. [9] M.Ravikumar,P.S.S.Srinivasan,Phasechange material as a thermal energy storage material for cooling of building, Journal of Theoretical and Applied Information Technology (2005) 503-512. [10] A. Felix Regin, S. C. Solanki, J. S. Saini, An analysis ofa packed bedlatentheatthermal energy storage system using PCM capsules: Numerical investigation, Renewable Energy 34 (2009)1765– 1773. [11] A. Mahmud, K. Sopian, M. Alghoul A. Mat Sohif, Using a Paraffin wax- Aluminum compound as a thermal storage material in a solar air heater, ARPN Journal of Engineering andAppliedSciences, vol. 4, no. 10, December2009. [12] F. demirbas, Thermal Energy Storage and Phase Change Materials: An Overview, Energy Sources, Part B, 1:85–95, 2006. [13] N. A. Mohd Amin, Martin Belusko, Frank Bruno, Optimisation of A Phase Change Thermal Storage System, World Academy of Science, Engineering and Technology 56 (2009). [14] S. A. Karaipekli, Thermal conductivity and latent heat thermal energy storage characteristics of paraffin/expanded graphite compositeasphase change material, Applied Thermal Engineering, Volume27,Issues8-9,June2007,Pages1271-1277. [15] Z. Zhang, X. Fang, Study on paraffin/expanded graphite composite phase change thermal energy storage material , Energy Conversion and Management, Volume 47, Issue 3, February 12006, Pages 303-310.