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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7015
Numerical Investigation of Heat Performance Enhancement for a
Double-Pipe Heat Exchanger at Annulus with Continuous Helical
Baffles using Al2O3 as Nanofluid
Amit Kumar Singh1, H.C.Thakur2
1,2Department of Mechanical Engineering, Gautam Buddha University, Greater Noida,, India
---------------------------------------------------------------------***----------------------------------------------------------------------
Abstract - Main goal of our project is to maximize the heat transfer rate and minimizing the pressure drop as much as possibleto
increase the performance enhancementfactorforheatexchanger. Asweknowthatby increasingReynoldsnumberNusseltnumber
increases thus increasing the heat transfer rate but in doing so pressure drop is also increased that is not beneficial for the
operating of heat exchanger so we used passive technique that is the use of nanofluid in place of water as cold fluid in the annulus
side to increase heat transfer rate. In this project we keep the mass flow at 0.1, 0.15, 0.2, 0.25, 0.3 Kg/s. AL2O3 is used as nanofluid
with volumetric concentration of 1%, 2%, 3%, 4% respectively and found that heat transfer rate is increased while there is a
decrement in pressure drop. And we have also plotted the graph for heat transfer, pressure drop and performance enhancement
factor
Key Words: Continuous helical baffles, Water to water heat exchanger, Heat transfer enhancement, Double pipe, Friction,
Numerical
1. INTRODUCTION
Double-pipe exchanger is made of two pairs of pipes that are concentrictoeachother.Therecanbesameortwodifferentfluids
that are transferring heat from inner to outer pipes or vice versa. The fluids usually flow in counter clockwise directions.They
are mostly used in applications involving relatively low flow rates and high temperatures or pressures. Other advantages
include low installation cost, ease of maintenance, and flexibility.
One of the starting studies performed on double pipe heat exchangers was done by Mozley [1] who numerically and
experimentally developed a case to study various dynamic characteristics of a special DPHEs.Those werederivedfromsimple
mathematical models. From this researchfrequencyresponseswasstudieditmatchedexperimental results.Researchhasbeen
done to increase the heat transfer rate of heat exchangers which helps in saving energy, money and time. It also helps in
increasing thermal rating and extending the overall workinglifeofthedevice. Thisisdone byusingvariouspassivegeometrical
features to increase the heat transfer capacity. These innovations reduces the thermal resistance but increasing the pressure
drop , as reported by Jian et al. [2] Bhadouriya et al. [3].
In this study, Rennie and Raghavan [4] studied DPHE. The study was conducted using both parallel and counter flow
arrangements. During research it was concluded that performance evaluation criterion was identical for both configurations,
also there was a huge difference in the heat transfer to the counter flow configuration due toitshightemperaturedifferenceas
compared to its counterpart Wilson plots were used to determine the heat transfer rates of inner tube and the annulus.
In this research Bhadouriya et al. [5] studied DPHE both experimentally and numerically. The objective was to researchon
the heat transfer and pressure drop. Boundary condition of annuluswall wastakenasuniformtemperature wall forouterflow.
The important point of the study was to research the effect of twist ratio of the inner tube on the flow characteristics. Air and
water were taken as the working fluid in the outer and inner tube of the heat exchanger, respectively.
Following the pervious researches, in another experimental investigation, Yadav [6] investigated the effects of half-length
twisted tapes on heat transfer and pressure drop of a double pipe U-bend heat exchanger. The twisted tapes were in the inner
tube of a DPHE which caused a 40-percent increase in heat transfer in comparison with smooth tube
Prasad et al. [7] studied the effect of trapezoidal-cut twisted tapes in a DPHE. The nanofluid used in this investigation was
water-based Al2O3 which was in turbulent flow regime. The results showed that the heat transfer rate increase in the annulus
was higher than that of the inner tube which this was mainly due tothesecondaryflowsintheannulus.Theyalsoobservedthat
the increase in nanofluid concentration and also the twist ratio leads to a higher heat transferandpressuredrop.Heattransfer
performance of a double pipe heat exchanger at annulus side with continuous helical baffles was studied by Maakoul et al.[8]
numerically The research was conducted for different mass flow rate (0.1 -0.3 kg/s) and baffle spacing (0.025–0.1 m). The
results showed an increase in heat transfer and pressure drop as compared to
the simple double-pipe exchanger.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7016
Nomenclature
Latin symbols u average velocity, m/s
Across cross-flow area at the annulus side, m2 x; y; z Cartesian coordinate
B baffle spacing, mm
cp specific heat capacity, J/(kg K) Greek symbols
ci coefficients in k e model Γ generalized diffusion coefficient
Ds internal annulus diameter, m ε turbulent kinetic energy dissipation rate, m2/s3
Do external tube diameter, m k thermal conductivity, W/(m K)
Dh hydraulic diameter, m μ dynamic viscosity, kg/(m s)
h average heat transfer coefficient, W/(m2 K) ν kinematic viscosity, m2/s
k turbulent fluctuation kinetic energy, m2/s2 q density, kg/m3
L tube total effective length, m σk Prandtl number for k
f friction factor σε Prandtl number for ε
m mass flow rate, kg/s ϕ nanoparticle volume fraction
Pr Prandtl number
Subscripts
∆p pressure drop, Pa
in inlet
Q heat transfer rate, W
out outlet
Re Reynolds number
a annulus side
Nu Nusselt number
t tube side
Tin hot water inlet temperature, oC
turb turbulent
tin cold water inlet temperature, oC
2. NUMERICAL MODEL
The main goal of this paper is to study heat transfer performance for double-pipe heat exchanger at annulus side with
continuous baffle of different spacing. This leads to change in the heat transfer, pressure drop, velocity in the annulus flow
domain and thus the net heat transfer rate and pressure drop varies from initial values. This structure is made of steel to
facilitate better heat transfer and resistance to corrosion. The D structure is shown in fig 1the baffle spacing is varied between
100mm to 0.25 mm and the heat performance of the structureis analyzed using water and nanofluid. Even thoughitseemsthat
the structure is simple but when analyzing the fluid flow it becomes complex due to introduction of baffles on annulus side.
In this paper first the base paper [8] result is validated for double pipe heat exchanger when water is taken as fluid on
annulus side and inner tube side. The flow in both tubes is taken as counter flow. The best part of the research is that due to
introduction of baffle the overall length of the exchanger remains the same but the flow path of the fluid is increased. The only
variation in the geometry is that the baffle spacing varies from 100mm to 25mm. More geometry details are listed in Table 1.
Also during further research water in the annulus side is replaced with Al2O3 nanofluid.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7017
Figure 1 geometry (3D & 2D)
Table 1 Structural parameters
Material: Stainless steel
Inner tube internal diameter 10 mm
Inner tube thickness 1 mm
Outer tube external diameter 16 mm
Outer tube thickness 1 mm
Annulus side baffles spacing 100–25 mm
Heat exchanger length 100 mm
2.1 Governing Equations
Continuity equation:
(1)
Momentum equation
(2)
Energy equation
(3)
To solve the problem that arises by turbulent flow which was caused by the introduction of baffle spacing on annulus side
Realizable k e turbulence model was selected in energy. The equations for realizable k e model are given below:
Turbulent kinetic energy k equation:
(4)
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7018
Turbulent energy dissipation equation
(5)
where C represents the generation of turbulence kinetic energy k due to the mean velocity gradients The wall is set to
scalable wall function
2.2 Domains definitions, mesh sensitivity and boundary conditions
At geometry creation we have to make a straight doublepipeheat exchanger withcontinuousbaffleonannulusside. Firstwe
have to draw a circle of Dia 10mm and then another concentric circle of Dia 12mm at the center the select both the sketch and
click generate surface. Similarly from the center point draw another sketch of two circle of Dia 16mm and 17mm. again select
the second sketch and click on generate surface. After this draw a new sketch that are two straight line between inner tube
outer circumference and outer tube inner circumference also the distance of both straightlinefromaxisis0.5mmonbothside.
Again select this sketch and click on generate surface. Now select the first two sketches and select extrude. In this select
direction as both forward and backward with extrude length of 50mm. Now separately select the third sketch and select
revolve in the pitch section select the pitch according to the bafflespacing.Thenselect directionasforwardand backward.Also
select the axis that is passing through the center of the circle around which the helical baffle will be rotated.
Meshing is done in the mesh window. In this portion a mix of unstructured tetrahedral and wedge (Prism) grid is used.
Inflation option is used near the wall of tubes
Table 2 Mesh quality
The no slip condition for all the solid walls
The software FLUENT is used to calculate the fluid flow and heat transfer in the computational domains. The governing
equations are iteratively solved bythefinite-volumeformulationwiththeSIMPLEalgorithm.Thesecond-orderupwindscheme
is adopted for the momentum, energy, turbulence and its dissipation rate. The pressure term is treated with the standard
scheme.
Outer wall is considered as insulated wall. In this condition heat is transferred from hot fluid to cold fluid through a solid
steel wall that is the inner wall of heat exchanger and cold fluid gets warmer and hot fluid gets colder. For inlet of hot fluidwas
set as velocity inlet. Here the velocity of inlet is kept constant at 0.1kg/smassflowratethroughoutthe entireanalysis. Theinlet
temperature of the hot fluid was taken as 312K. Similarly for inlet of cold fluidwasset asvelocityinlet.Herethevelocityofinlet
was varied by changing the mass flow rate. The mass flow rate of the working fluid was varied between 0.1, 0.15, 0.2, 0.25, 0.3
kg/s. The inlet temperature of cold fluid was taken as 288K. For the outlet of cold fluid and hot fluid was takes as Pressure
outlet boundary condition.
Nodes Elements Average skewness Average orthogonal quality
286288 392755 0.270605 0.844705
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7019
At the outlet the gauge pressure was taken as zero atmospheric pressure. Thewall oftheoutertubeistakenasinsultedwall
condition, this done because there is no heat exchange taking place through that wall The fluidpropertyof waterwasassumed
to be continuous throughout the analysis with respect to temperature.
3. DATA REDUCTION
3.1 Annulus side velocity
ua= ma/(ρaAcross) (6)
3.2 Characteristics cross section area for helically baffle annulus side
Across= 0.5B(Ds - Do) (7)
With the mean velocity value, the Reynolds number for the annulus side is determined by:
Re= (ρauaDo)/μ (8)
3.3 Heat transfer rate:
Heat transfer rate of the annulus side fluid (cool water):
Qa= maCpa(Tout a-Tin a) (9)
Heat transfer for hot fluid tube
Qt=mtCpt(Tin t-Tout t) (10)
3.4 Nusselt number
Nu = (haDh)/k (11)
When using nanofluid in place of water
3.5 Thermal conductivity:
For calculating thermal conductivity of water based Nanofluid Maxwell [9] formula is used. Also Brownian effect is
neglected. The effective thermal conductivity of nanofluid is given by:
(12)
3.6 Specific heat and density:
Calculation of specific heat and density is straight forward. They can be based on the physical guideline of the blend
administer these outcomes are in great understanding with experiment information. The specific heat is formula [9]:
(Cp)nf = (1-ϕ)(Cp)f + ϕ(Cp)np (13)
3.7 Density is calculated by using formula given by[9]
ρnf = (1-ϕ)ρf + ϕρnp (14)
3.9 Viscosity
μnf = μf(1+2.5ϕ) (15)
4. RESULTS AND DISCUSSION
The research work was done in two parts. First water was taken as fluid in both the inner and outer pipe and the results
obtained from it are compared with results from the base paper. Second the fluid in the annulus side is replaced with Al2O3.
Also nanofluid concentration is varied from 1% to 4% and the results obtained are shown below. In order to verify the results
graph with various parameters like heat transfer coefficient, pressure drop, thermal enhancement factorwith respecttomass
flow rate is plotted and is compared to the graph obtained from the base paper. This showed satisfactory result
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7020
4.1 Fluid flow characteristics
In Fig. 3 velocity streamline simulation has been shown. It can be seen that the max velocity is at the inlet of the fluid. It can
also be seen that due to introduction of continuous helical baffle on annulus side,helical flowisinitiated.Duetohelical paththe
same length of double pipe exchanger provides a greater flow path for the fluid hence increasing the heat transfer effect. This
leads more compact exchanger design. Also due to helical path the turbulence of the fluid is increased which is beneficial in
energy transfer. From analyzing the fig 3 it can be seen that the velocity is directly proportional to massflowratebutinversely
proportional to the baffle spacing. The total flow path length can be determined by following formulae
(16)
Figure 3 Annulus side velocity streamlines at m= 0:3 kg/s for different baffle spacing when using water as fluid
The velocity is at max at the inlet of the annulus this can be explained by the fact that there is a sudden decreaseinthecross
section area. Hence the velocity can only be increased to maintain the same massflow rateattheannulusside.This canbeused
to explain the sudden rise in velocity when increasing the mass flow rate at the annulus side.
4.2 Heat transfer performance
From Fig. 4(A) results for the base paper validation is shown. From graph it can be seen that results almost matches the
graph drawn in the base paper [8]. In this the heat transfer coefficient at the annulus side is shown foe different baffle spacing
as well as for simple double pipe heat exchanger. Results obtained showed the benefits of having continuous baffle spacingon
annulus side as compared to simple double pipe heat exchanger. The average increment of the overall heattransfercoefficient
on annulus side for 100, 50, 33.33, 25mm is 5%, 17%, 30% and 45% respectively. The results obtained approximately have
same as in the base paper.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7021
Figure 4(A)
Figure 4(B)
Figure 4(C)
Figure 4(D)
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7022
Figure 4(E)
Figure 4(A)(B)(C)(D)(E). Annulus side heat transfer coefficient (*104) w.r.t. mass flow rate for different baffle spacing
Fig.4 (B), (C), (D), (E) demonstrate the heat transfer coefficient results for the annulus side with same condition of baffle
spacing and mass flow rate as used in base paper [8]. But the difference is that in this case Al2O3 nanofluid of concentration
from 1% to 4% respectively is used. The results from the graph showsthatthereisanaverageincreasein2.88%,5.90%,9.83%
and 12.21% for volumetric concentration of 1%, 2%, 3% and 4% of nanoparticle respectively.Theincreaseinheat transfercan
be explained by the fact that with the addition of nanoparticle increases the overall thermal conductivity of base fluid and
enhancing the heat transfer results. Also from the graph it can be interpreted that the heat transfer coefficient rate is directly
proportional to mass flow rate and inversely proportional to baffle spacingassmallerthebafflespacinggreateristheflowpath
and hence greater is the heat transfer.
4.3 Nusselt number
From Fig. 5(A) results for the base paper [8] validation is shown. From graph it can be seen that results almost matchesthe
graph drawn in the base paper. In this the Nusselt number in the form of NuPr-1/3 at the annulus side is shown foe different
baffle spacing as well as for simple double pipe heat exchanger. Results obtained showed the benefits of having continuous
baffle spacing on annulus side as compared to simple double pipe heat exchanger.
Figure 5(A)
Figure 5(B)
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7023
Figure 5(C)
Figure 5(D)
Figure 5(E)
Figure 5(A)(B)(C)(D)(E). Annulus side Nusselt number w.r.t. Reynolds number (*104) for different baffle spacing
From this it can be seen that with increasing mass flow rate and decreasing baffle spacing heat transfer of the heat
exchanger increases.
NuPr-1/3 = 0.04572Re0.6098(1+B)7.565 (17)
From equation 17 it can be seen that the value of NuPr-1/3 is inversely proportional to dynamic viscosity which increases
with increasing the nanoparticle concentration hence with increasing nanofluid concentration the value forNuPr-1/3 beginsto
decrease. The results from the fig 5(B), (C), (D), (E) shows that there is an average decreaseof1.49%,3.22%,4.31%and5.64%
for volumetric concentration of 1%, 2%, 3% and 4% of nanoparticle respectively.
4.4 Pressure drop
The pumping power that is supplied to the heat exchanger is an important factorindeterminingthenetoverall efficiencyof
that particular heat exchanger. Since simple double pipe heat exchangerscanonlybe usedinthefieldwithlowpumpingpower
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7024
hence it is most important to reduce the net pressure drop for the heat exchanger so that it can be most efficient. When the
continuous baffle was provided at the annulus side the pressure drop was increased due to following reasons
 Fluid flow path was increased
 Due to sudden reduction in cross sectional area to maintain the mass flow rate, fluid velocity has to increase.
Figure 6(A)
Figure 6(B)
Figure 6(C)
Figure 6(D)
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7025
Figure 6(E)
Figure 6(A)(B)(C)(D)(E). Annulus side pressure drop w.r.t. mass flow rate for different baffle spacing
In fig 6(A) results from base paper [8] is validated. It can be seen from the graph that pressure dropdirectlydependsonthe
mass flow rate. Also as baffle spacing is decreased the flow path length increase to maintain the overall fluid flow till the end,
pressure has to be increased. Hence pressure drop is inversely proportional to the baffle spacing.
(18)
Fig 6 (B), (C), (D), (E) demonstrates the pressure drop in the outer tube flow region. In these cases Al2O3 nanofluid of
concentration from 1% to 4% respectively is used. The results from the graph shows that there is an average decrease of
2.29%, 4.58%, 6.69% and 8.60% for volumetric concentration of 1%, 2%, 3% and 4% of nanoparticle respectively. The
decrease in pressure drop can be explained by the fact that it is directly proportional to friction factor and inversely
proportional to density of fluid. With the addition of nanoparticle both friction factor and density increase but the increase of
density is greater as compared to friction factor. Hence the values of pressure drop on annulus side decreases with increment
in the nanoparticle concentration.
4.5 Thermal performance enhancement factor
In earlier times researchers mainly focusedonincreasing heattransferirrespectiveof pumpingpowerloss.Thisapproachis
good when the size and pumping power requirement of heat exchanger are considered secondary when comparing it to heat
transfer.
Figure 7(A)
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7026
Figure 7(B)
Figure 7(C)
Figure 7(D)
Figure 7(E)
Figure 7(A)(B)(C)(D)(E). Thermal performance enhancement factor w.r.t. mass flow rate for various baffle spacing
But in this paper research is done on those types of heat exchangers that are used in small machinery with low pumping
power. Hence we cannot rely on only increasing heat transfer and neglecting pressure drop. So after analyzing the problem a
new term was introduced which was called as thermal performance enhancement factor, represented by symbol η. It is the
comparison between Nusselt number and pressuredropofannulussidewith bafflesto Nusseltnumberofordinary doublepipe
heat exchanger without any modifications. This quantity is given by:
(19)
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
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In Fig. 7(A) results from base paper [8] is validated. It can be seen from the graph that thermal performance enhancement
factor is directly proportional to baffle spacing. Also it decreases with the increasing mass flow rate.
This result can be explained by the fact that when the baffle spacing is decreased the pressure drop is tremendously
increased as compared to increment in Nusselt number this leads to decrement in the thermal performance enhancement
factor, this result is similar to base paper.
From fig 7 (B), (C), (D), (E) When the nanofluid is used the average percentageofchangeinthermal performanceenhancement
factor are 0.97%, 0.96%, 0.94% and 0.93% for volumetric concentration of 1%, 2%, 3% and 4% of nanoparticle respectively.
5 CONCLUSIONS
A numerical study has been carried out for tube and tube heat exchanger with continuous helical baffle on annulus side
subjected to different boundary conditions. Heat transfer coefficient,productofNusseltnumberandPrandtl number,pressure
drop, thermal enhancement factor with respect to mass flow rate for different bafflespacingisplotted. Followingobservations
has been noticed-
 Increasing the mass flow rate increases the heat transfer coefficient on annulus side.
 With decreasing the baffle spacing heat transfer coefficient is increased.
 Increasing the mass flow rate increases the pressure drop on annulus side.
 With decreasing the baffle spacing pressure drop is exponentially increased
 The product of Nusselt number and Prandtl numberincreaseswithdecreasing bafflespacingandincreasing massflow
rate.
 Overall the thermal enhancement factor for the mass flow rate of 0.3 kg/s and baffle spacing of 33.33mm is the most
balanced of all the results.
When Al2O3 nanofluid is used on annulus side with different boundary conditions following observations has been noticed-
 As the concentration of nanofluid is increased the thermal conductivity of the nanofluid is enhanced hence the heat
transfer coefficient is also increased. The effect of mass flow rateandbafflespacingremainsthesameas whenwateris
used in annulus tube.
 Pressure drop is directly proportional to friction factor but inversely proportional todensityofnanofluidhencewhen
comparing at the same mass flow rate as used in the base paper [8] the pressure drop decreases with increasing
volumetric concentration of the nanofluid because the increase of density is greater as compared to friction factor.
REFERENCES
[1] J. Mozley, Predicting dynamics of concentric pipe heat exchangers, Ind. Eng. Chem. 48 (1956) 1035–1041.
[2] Jian W, Huizhu Y, Wang S, Xu S, Yulan X, Tuo H. Numerical investigation on baffle configuration improvement of the heat
exchanger with helical baffles. Energy Conversion and Management (2015); 89: 438–48..
[3] Bhadouriya R, Agrawal A, Prabhu SV. Experimental and numerical study of fluid flow and heat transfer in an annulus of
inner twisted square duct and outer circular pipe. International Journal of Thermal Sciences (2015); 94:96–109.
[4] T.J. Rennie, V.G. Raghavan, Experimental studies of a double-pipe helical heat exchanger,Exp.Thermal FluidSci.29(2005)
919–924.
[5] R. Bhadouriya, A. Agrawal, S. Prabhu, Experimental and numerical study of fluid flow and heat transfer in an annulus of
inner twisted square duct and outer circular pipe, Int. J. Therm. Sci. 94 (2015) 96–109.
[6] A.S. Yadav, Effect of half length twisted-tape turbulators on heat transfer andpressure dropcharacteristicsinsidea double
pipe u-bend heat exchanger, JJMIE 3 (2009).
[7] P.D. Prasad, A. Gupta, K. Deepak, Investigation oftrapezoidal-cuttwistedtapeinsertina doublepipeU-tubeheatexchanger
using Al2O3/water nanofluid, Procedia Mater. Sci. 10 (2015) 50–63.
[8] Anas El Maakoul, Azzeddine Laknizi, Said Saadeddine, Abdellatif Ben Abdellah, Mohamed eziane, Mustapha El Metoui,
Numerical design and investigation of heat transfer enhancement and performancefor anannuluswithcontinuous helical
baffles in a double-pipe heat exchanger, Energy Conversion and Management (2016), 76-86.
[9] B. Ghasemi, S.M. Aminossadati, Brownian motion of nanoparticles in a triangular enclosure with natural convection,
International Journal of Thermal Sciences 49 (6) (2010) 931–940.

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Numerical Investigation of Heat Performance Enhancement for a Double-Pipe Heat Exchanger at Annulus with Continuous Helical Baffles using Al2O3 as Nanofluid

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7015 Numerical Investigation of Heat Performance Enhancement for a Double-Pipe Heat Exchanger at Annulus with Continuous Helical Baffles using Al2O3 as Nanofluid Amit Kumar Singh1, H.C.Thakur2 1,2Department of Mechanical Engineering, Gautam Buddha University, Greater Noida,, India ---------------------------------------------------------------------***---------------------------------------------------------------------- Abstract - Main goal of our project is to maximize the heat transfer rate and minimizing the pressure drop as much as possibleto increase the performance enhancementfactorforheatexchanger. Asweknowthatby increasingReynoldsnumberNusseltnumber increases thus increasing the heat transfer rate but in doing so pressure drop is also increased that is not beneficial for the operating of heat exchanger so we used passive technique that is the use of nanofluid in place of water as cold fluid in the annulus side to increase heat transfer rate. In this project we keep the mass flow at 0.1, 0.15, 0.2, 0.25, 0.3 Kg/s. AL2O3 is used as nanofluid with volumetric concentration of 1%, 2%, 3%, 4% respectively and found that heat transfer rate is increased while there is a decrement in pressure drop. And we have also plotted the graph for heat transfer, pressure drop and performance enhancement factor Key Words: Continuous helical baffles, Water to water heat exchanger, Heat transfer enhancement, Double pipe, Friction, Numerical 1. INTRODUCTION Double-pipe exchanger is made of two pairs of pipes that are concentrictoeachother.Therecanbesameortwodifferentfluids that are transferring heat from inner to outer pipes or vice versa. The fluids usually flow in counter clockwise directions.They are mostly used in applications involving relatively low flow rates and high temperatures or pressures. Other advantages include low installation cost, ease of maintenance, and flexibility. One of the starting studies performed on double pipe heat exchangers was done by Mozley [1] who numerically and experimentally developed a case to study various dynamic characteristics of a special DPHEs.Those werederivedfromsimple mathematical models. From this researchfrequencyresponseswasstudieditmatchedexperimental results.Researchhasbeen done to increase the heat transfer rate of heat exchangers which helps in saving energy, money and time. It also helps in increasing thermal rating and extending the overall workinglifeofthedevice. Thisisdone byusingvariouspassivegeometrical features to increase the heat transfer capacity. These innovations reduces the thermal resistance but increasing the pressure drop , as reported by Jian et al. [2] Bhadouriya et al. [3]. In this study, Rennie and Raghavan [4] studied DPHE. The study was conducted using both parallel and counter flow arrangements. During research it was concluded that performance evaluation criterion was identical for both configurations, also there was a huge difference in the heat transfer to the counter flow configuration due toitshightemperaturedifferenceas compared to its counterpart Wilson plots were used to determine the heat transfer rates of inner tube and the annulus. In this research Bhadouriya et al. [5] studied DPHE both experimentally and numerically. The objective was to researchon the heat transfer and pressure drop. Boundary condition of annuluswall wastakenasuniformtemperature wall forouterflow. The important point of the study was to research the effect of twist ratio of the inner tube on the flow characteristics. Air and water were taken as the working fluid in the outer and inner tube of the heat exchanger, respectively. Following the pervious researches, in another experimental investigation, Yadav [6] investigated the effects of half-length twisted tapes on heat transfer and pressure drop of a double pipe U-bend heat exchanger. The twisted tapes were in the inner tube of a DPHE which caused a 40-percent increase in heat transfer in comparison with smooth tube Prasad et al. [7] studied the effect of trapezoidal-cut twisted tapes in a DPHE. The nanofluid used in this investigation was water-based Al2O3 which was in turbulent flow regime. The results showed that the heat transfer rate increase in the annulus was higher than that of the inner tube which this was mainly due tothesecondaryflowsintheannulus.Theyalsoobservedthat the increase in nanofluid concentration and also the twist ratio leads to a higher heat transferandpressuredrop.Heattransfer performance of a double pipe heat exchanger at annulus side with continuous helical baffles was studied by Maakoul et al.[8] numerically The research was conducted for different mass flow rate (0.1 -0.3 kg/s) and baffle spacing (0.025–0.1 m). The results showed an increase in heat transfer and pressure drop as compared to the simple double-pipe exchanger.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7016 Nomenclature Latin symbols u average velocity, m/s Across cross-flow area at the annulus side, m2 x; y; z Cartesian coordinate B baffle spacing, mm cp specific heat capacity, J/(kg K) Greek symbols ci coefficients in k e model Γ generalized diffusion coefficient Ds internal annulus diameter, m ε turbulent kinetic energy dissipation rate, m2/s3 Do external tube diameter, m k thermal conductivity, W/(m K) Dh hydraulic diameter, m μ dynamic viscosity, kg/(m s) h average heat transfer coefficient, W/(m2 K) ν kinematic viscosity, m2/s k turbulent fluctuation kinetic energy, m2/s2 q density, kg/m3 L tube total effective length, m σk Prandtl number for k f friction factor σε Prandtl number for ε m mass flow rate, kg/s ϕ nanoparticle volume fraction Pr Prandtl number Subscripts ∆p pressure drop, Pa in inlet Q heat transfer rate, W out outlet Re Reynolds number a annulus side Nu Nusselt number t tube side Tin hot water inlet temperature, oC turb turbulent tin cold water inlet temperature, oC 2. NUMERICAL MODEL The main goal of this paper is to study heat transfer performance for double-pipe heat exchanger at annulus side with continuous baffle of different spacing. This leads to change in the heat transfer, pressure drop, velocity in the annulus flow domain and thus the net heat transfer rate and pressure drop varies from initial values. This structure is made of steel to facilitate better heat transfer and resistance to corrosion. The D structure is shown in fig 1the baffle spacing is varied between 100mm to 0.25 mm and the heat performance of the structureis analyzed using water and nanofluid. Even thoughitseemsthat the structure is simple but when analyzing the fluid flow it becomes complex due to introduction of baffles on annulus side. In this paper first the base paper [8] result is validated for double pipe heat exchanger when water is taken as fluid on annulus side and inner tube side. The flow in both tubes is taken as counter flow. The best part of the research is that due to introduction of baffle the overall length of the exchanger remains the same but the flow path of the fluid is increased. The only variation in the geometry is that the baffle spacing varies from 100mm to 25mm. More geometry details are listed in Table 1. Also during further research water in the annulus side is replaced with Al2O3 nanofluid.
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7017 Figure 1 geometry (3D & 2D) Table 1 Structural parameters Material: Stainless steel Inner tube internal diameter 10 mm Inner tube thickness 1 mm Outer tube external diameter 16 mm Outer tube thickness 1 mm Annulus side baffles spacing 100–25 mm Heat exchanger length 100 mm 2.1 Governing Equations Continuity equation: (1) Momentum equation (2) Energy equation (3) To solve the problem that arises by turbulent flow which was caused by the introduction of baffle spacing on annulus side Realizable k e turbulence model was selected in energy. The equations for realizable k e model are given below: Turbulent kinetic energy k equation: (4)
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7018 Turbulent energy dissipation equation (5) where C represents the generation of turbulence kinetic energy k due to the mean velocity gradients The wall is set to scalable wall function 2.2 Domains definitions, mesh sensitivity and boundary conditions At geometry creation we have to make a straight doublepipeheat exchanger withcontinuousbaffleonannulusside. Firstwe have to draw a circle of Dia 10mm and then another concentric circle of Dia 12mm at the center the select both the sketch and click generate surface. Similarly from the center point draw another sketch of two circle of Dia 16mm and 17mm. again select the second sketch and click on generate surface. After this draw a new sketch that are two straight line between inner tube outer circumference and outer tube inner circumference also the distance of both straightlinefromaxisis0.5mmonbothside. Again select this sketch and click on generate surface. Now select the first two sketches and select extrude. In this select direction as both forward and backward with extrude length of 50mm. Now separately select the third sketch and select revolve in the pitch section select the pitch according to the bafflespacing.Thenselect directionasforwardand backward.Also select the axis that is passing through the center of the circle around which the helical baffle will be rotated. Meshing is done in the mesh window. In this portion a mix of unstructured tetrahedral and wedge (Prism) grid is used. Inflation option is used near the wall of tubes Table 2 Mesh quality The no slip condition for all the solid walls The software FLUENT is used to calculate the fluid flow and heat transfer in the computational domains. The governing equations are iteratively solved bythefinite-volumeformulationwiththeSIMPLEalgorithm.Thesecond-orderupwindscheme is adopted for the momentum, energy, turbulence and its dissipation rate. The pressure term is treated with the standard scheme. Outer wall is considered as insulated wall. In this condition heat is transferred from hot fluid to cold fluid through a solid steel wall that is the inner wall of heat exchanger and cold fluid gets warmer and hot fluid gets colder. For inlet of hot fluidwas set as velocity inlet. Here the velocity of inlet is kept constant at 0.1kg/smassflowratethroughoutthe entireanalysis. Theinlet temperature of the hot fluid was taken as 312K. Similarly for inlet of cold fluidwasset asvelocityinlet.Herethevelocityofinlet was varied by changing the mass flow rate. The mass flow rate of the working fluid was varied between 0.1, 0.15, 0.2, 0.25, 0.3 kg/s. The inlet temperature of cold fluid was taken as 288K. For the outlet of cold fluid and hot fluid was takes as Pressure outlet boundary condition. Nodes Elements Average skewness Average orthogonal quality 286288 392755 0.270605 0.844705
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7019 At the outlet the gauge pressure was taken as zero atmospheric pressure. Thewall oftheoutertubeistakenasinsultedwall condition, this done because there is no heat exchange taking place through that wall The fluidpropertyof waterwasassumed to be continuous throughout the analysis with respect to temperature. 3. DATA REDUCTION 3.1 Annulus side velocity ua= ma/(ρaAcross) (6) 3.2 Characteristics cross section area for helically baffle annulus side Across= 0.5B(Ds - Do) (7) With the mean velocity value, the Reynolds number for the annulus side is determined by: Re= (ρauaDo)/μ (8) 3.3 Heat transfer rate: Heat transfer rate of the annulus side fluid (cool water): Qa= maCpa(Tout a-Tin a) (9) Heat transfer for hot fluid tube Qt=mtCpt(Tin t-Tout t) (10) 3.4 Nusselt number Nu = (haDh)/k (11) When using nanofluid in place of water 3.5 Thermal conductivity: For calculating thermal conductivity of water based Nanofluid Maxwell [9] formula is used. Also Brownian effect is neglected. The effective thermal conductivity of nanofluid is given by: (12) 3.6 Specific heat and density: Calculation of specific heat and density is straight forward. They can be based on the physical guideline of the blend administer these outcomes are in great understanding with experiment information. The specific heat is formula [9]: (Cp)nf = (1-ϕ)(Cp)f + ϕ(Cp)np (13) 3.7 Density is calculated by using formula given by[9] ρnf = (1-ϕ)ρf + ϕρnp (14) 3.9 Viscosity μnf = μf(1+2.5ϕ) (15) 4. RESULTS AND DISCUSSION The research work was done in two parts. First water was taken as fluid in both the inner and outer pipe and the results obtained from it are compared with results from the base paper. Second the fluid in the annulus side is replaced with Al2O3. Also nanofluid concentration is varied from 1% to 4% and the results obtained are shown below. In order to verify the results graph with various parameters like heat transfer coefficient, pressure drop, thermal enhancement factorwith respecttomass flow rate is plotted and is compared to the graph obtained from the base paper. This showed satisfactory result
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7020 4.1 Fluid flow characteristics In Fig. 3 velocity streamline simulation has been shown. It can be seen that the max velocity is at the inlet of the fluid. It can also be seen that due to introduction of continuous helical baffle on annulus side,helical flowisinitiated.Duetohelical paththe same length of double pipe exchanger provides a greater flow path for the fluid hence increasing the heat transfer effect. This leads more compact exchanger design. Also due to helical path the turbulence of the fluid is increased which is beneficial in energy transfer. From analyzing the fig 3 it can be seen that the velocity is directly proportional to massflowratebutinversely proportional to the baffle spacing. The total flow path length can be determined by following formulae (16) Figure 3 Annulus side velocity streamlines at m= 0:3 kg/s for different baffle spacing when using water as fluid The velocity is at max at the inlet of the annulus this can be explained by the fact that there is a sudden decreaseinthecross section area. Hence the velocity can only be increased to maintain the same massflow rateattheannulusside.This canbeused to explain the sudden rise in velocity when increasing the mass flow rate at the annulus side. 4.2 Heat transfer performance From Fig. 4(A) results for the base paper validation is shown. From graph it can be seen that results almost matches the graph drawn in the base paper [8]. In this the heat transfer coefficient at the annulus side is shown foe different baffle spacing as well as for simple double pipe heat exchanger. Results obtained showed the benefits of having continuous baffle spacingon annulus side as compared to simple double pipe heat exchanger. The average increment of the overall heattransfercoefficient on annulus side for 100, 50, 33.33, 25mm is 5%, 17%, 30% and 45% respectively. The results obtained approximately have same as in the base paper.
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7021 Figure 4(A) Figure 4(B) Figure 4(C) Figure 4(D)
  • 8. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7022 Figure 4(E) Figure 4(A)(B)(C)(D)(E). Annulus side heat transfer coefficient (*104) w.r.t. mass flow rate for different baffle spacing Fig.4 (B), (C), (D), (E) demonstrate the heat transfer coefficient results for the annulus side with same condition of baffle spacing and mass flow rate as used in base paper [8]. But the difference is that in this case Al2O3 nanofluid of concentration from 1% to 4% respectively is used. The results from the graph showsthatthereisanaverageincreasein2.88%,5.90%,9.83% and 12.21% for volumetric concentration of 1%, 2%, 3% and 4% of nanoparticle respectively.Theincreaseinheat transfercan be explained by the fact that with the addition of nanoparticle increases the overall thermal conductivity of base fluid and enhancing the heat transfer results. Also from the graph it can be interpreted that the heat transfer coefficient rate is directly proportional to mass flow rate and inversely proportional to baffle spacingassmallerthebafflespacinggreateristheflowpath and hence greater is the heat transfer. 4.3 Nusselt number From Fig. 5(A) results for the base paper [8] validation is shown. From graph it can be seen that results almost matchesthe graph drawn in the base paper. In this the Nusselt number in the form of NuPr-1/3 at the annulus side is shown foe different baffle spacing as well as for simple double pipe heat exchanger. Results obtained showed the benefits of having continuous baffle spacing on annulus side as compared to simple double pipe heat exchanger. Figure 5(A) Figure 5(B)
  • 9. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7023 Figure 5(C) Figure 5(D) Figure 5(E) Figure 5(A)(B)(C)(D)(E). Annulus side Nusselt number w.r.t. Reynolds number (*104) for different baffle spacing From this it can be seen that with increasing mass flow rate and decreasing baffle spacing heat transfer of the heat exchanger increases. NuPr-1/3 = 0.04572Re0.6098(1+B)7.565 (17) From equation 17 it can be seen that the value of NuPr-1/3 is inversely proportional to dynamic viscosity which increases with increasing the nanoparticle concentration hence with increasing nanofluid concentration the value forNuPr-1/3 beginsto decrease. The results from the fig 5(B), (C), (D), (E) shows that there is an average decreaseof1.49%,3.22%,4.31%and5.64% for volumetric concentration of 1%, 2%, 3% and 4% of nanoparticle respectively. 4.4 Pressure drop The pumping power that is supplied to the heat exchanger is an important factorindeterminingthenetoverall efficiencyof that particular heat exchanger. Since simple double pipe heat exchangerscanonlybe usedinthefieldwithlowpumpingpower
  • 10. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7024 hence it is most important to reduce the net pressure drop for the heat exchanger so that it can be most efficient. When the continuous baffle was provided at the annulus side the pressure drop was increased due to following reasons  Fluid flow path was increased  Due to sudden reduction in cross sectional area to maintain the mass flow rate, fluid velocity has to increase. Figure 6(A) Figure 6(B) Figure 6(C) Figure 6(D)
  • 11. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7025 Figure 6(E) Figure 6(A)(B)(C)(D)(E). Annulus side pressure drop w.r.t. mass flow rate for different baffle spacing In fig 6(A) results from base paper [8] is validated. It can be seen from the graph that pressure dropdirectlydependsonthe mass flow rate. Also as baffle spacing is decreased the flow path length increase to maintain the overall fluid flow till the end, pressure has to be increased. Hence pressure drop is inversely proportional to the baffle spacing. (18) Fig 6 (B), (C), (D), (E) demonstrates the pressure drop in the outer tube flow region. In these cases Al2O3 nanofluid of concentration from 1% to 4% respectively is used. The results from the graph shows that there is an average decrease of 2.29%, 4.58%, 6.69% and 8.60% for volumetric concentration of 1%, 2%, 3% and 4% of nanoparticle respectively. The decrease in pressure drop can be explained by the fact that it is directly proportional to friction factor and inversely proportional to density of fluid. With the addition of nanoparticle both friction factor and density increase but the increase of density is greater as compared to friction factor. Hence the values of pressure drop on annulus side decreases with increment in the nanoparticle concentration. 4.5 Thermal performance enhancement factor In earlier times researchers mainly focusedonincreasing heattransferirrespectiveof pumpingpowerloss.Thisapproachis good when the size and pumping power requirement of heat exchanger are considered secondary when comparing it to heat transfer. Figure 7(A)
  • 12. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7026 Figure 7(B) Figure 7(C) Figure 7(D) Figure 7(E) Figure 7(A)(B)(C)(D)(E). Thermal performance enhancement factor w.r.t. mass flow rate for various baffle spacing But in this paper research is done on those types of heat exchangers that are used in small machinery with low pumping power. Hence we cannot rely on only increasing heat transfer and neglecting pressure drop. So after analyzing the problem a new term was introduced which was called as thermal performance enhancement factor, represented by symbol η. It is the comparison between Nusselt number and pressuredropofannulussidewith bafflesto Nusseltnumberofordinary doublepipe heat exchanger without any modifications. This quantity is given by: (19)
  • 13. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 7027 In Fig. 7(A) results from base paper [8] is validated. It can be seen from the graph that thermal performance enhancement factor is directly proportional to baffle spacing. Also it decreases with the increasing mass flow rate. This result can be explained by the fact that when the baffle spacing is decreased the pressure drop is tremendously increased as compared to increment in Nusselt number this leads to decrement in the thermal performance enhancement factor, this result is similar to base paper. From fig 7 (B), (C), (D), (E) When the nanofluid is used the average percentageofchangeinthermal performanceenhancement factor are 0.97%, 0.96%, 0.94% and 0.93% for volumetric concentration of 1%, 2%, 3% and 4% of nanoparticle respectively. 5 CONCLUSIONS A numerical study has been carried out for tube and tube heat exchanger with continuous helical baffle on annulus side subjected to different boundary conditions. Heat transfer coefficient,productofNusseltnumberandPrandtl number,pressure drop, thermal enhancement factor with respect to mass flow rate for different bafflespacingisplotted. Followingobservations has been noticed-  Increasing the mass flow rate increases the heat transfer coefficient on annulus side.  With decreasing the baffle spacing heat transfer coefficient is increased.  Increasing the mass flow rate increases the pressure drop on annulus side.  With decreasing the baffle spacing pressure drop is exponentially increased  The product of Nusselt number and Prandtl numberincreaseswithdecreasing bafflespacingandincreasing massflow rate.  Overall the thermal enhancement factor for the mass flow rate of 0.3 kg/s and baffle spacing of 33.33mm is the most balanced of all the results. When Al2O3 nanofluid is used on annulus side with different boundary conditions following observations has been noticed-  As the concentration of nanofluid is increased the thermal conductivity of the nanofluid is enhanced hence the heat transfer coefficient is also increased. The effect of mass flow rateandbafflespacingremainsthesameas whenwateris used in annulus tube.  Pressure drop is directly proportional to friction factor but inversely proportional todensityofnanofluidhencewhen comparing at the same mass flow rate as used in the base paper [8] the pressure drop decreases with increasing volumetric concentration of the nanofluid because the increase of density is greater as compared to friction factor. REFERENCES [1] J. Mozley, Predicting dynamics of concentric pipe heat exchangers, Ind. Eng. Chem. 48 (1956) 1035–1041. [2] Jian W, Huizhu Y, Wang S, Xu S, Yulan X, Tuo H. Numerical investigation on baffle configuration improvement of the heat exchanger with helical baffles. Energy Conversion and Management (2015); 89: 438–48.. [3] Bhadouriya R, Agrawal A, Prabhu SV. Experimental and numerical study of fluid flow and heat transfer in an annulus of inner twisted square duct and outer circular pipe. International Journal of Thermal Sciences (2015); 94:96–109. [4] T.J. Rennie, V.G. Raghavan, Experimental studies of a double-pipe helical heat exchanger,Exp.Thermal FluidSci.29(2005) 919–924. [5] R. Bhadouriya, A. Agrawal, S. Prabhu, Experimental and numerical study of fluid flow and heat transfer in an annulus of inner twisted square duct and outer circular pipe, Int. J. Therm. Sci. 94 (2015) 96–109. [6] A.S. Yadav, Effect of half length twisted-tape turbulators on heat transfer andpressure dropcharacteristicsinsidea double pipe u-bend heat exchanger, JJMIE 3 (2009). [7] P.D. Prasad, A. Gupta, K. Deepak, Investigation oftrapezoidal-cuttwistedtapeinsertina doublepipeU-tubeheatexchanger using Al2O3/water nanofluid, Procedia Mater. Sci. 10 (2015) 50–63. [8] Anas El Maakoul, Azzeddine Laknizi, Said Saadeddine, Abdellatif Ben Abdellah, Mohamed eziane, Mustapha El Metoui, Numerical design and investigation of heat transfer enhancement and performancefor anannuluswithcontinuous helical baffles in a double-pipe heat exchanger, Energy Conversion and Management (2016), 76-86. [9] B. Ghasemi, S.M. Aminossadati, Brownian motion of nanoparticles in a triangular enclosure with natural convection, International Journal of Thermal Sciences 49 (6) (2010) 931–940.