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Performance evaluation of a shell and tube heat exchanger with recovery

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Journal of the Taiwan Institute of Chemical Engineers
journal homepage: www.elsevier.com/locate/jtice
Performance evaluation of a shell and tube heat exchanger with recovery
of mass flow rate
Babak Masoumpour, Mohammad Ataeizadeh, Hassan Hajabdollahi,
Mohammad Shafiey Dehaj*
Department of Mechanical Engineering, Faculty of Engineering, Vali-e-Asr University of Rafsanjan, Rafsanjan, Iran
A R T I C L E
I N F O
Article History:
Received 8 February 2021
Revised 29 April 2021
Accepted 16 May 2021
Available online xxx
Keywords:
Shell and tube heat exchanger
Mass flow rate recovery
Reflux ratio
Multi objective optimization
A B S T R A C T
In this paper, a new heat exchanger configuration considering return of stream from outlet to mixed with inlet
stream is investigated. For this purpose, the effect of mass flow rate recovery (MFRR) using reflux direction on
thermo-economic optimizing the shell and tube heat exchanger (STHE) is investigated numerically and compared to the case without recovery. Effectiveness and total annual cost (TAC) are considered as objective functions and nine design parameters related to the STHE parameters as well as reflux ratio and recovery tube
diameter are considered. The optimum results are presented as Pareto front and reveal the significant improvement in the both TAC and effectiveness by considering MFRR compared with conventional heat exchanger (without stream recovery). For example, 5.8% improvement in the effectiveness is observed in the case of MFRR
compared with the conventional heat exchanger for the fixed value of TAC=4943 $/year. Furthermore, the TAC
decreased by 24% in the cases of MFRR compared with conventional heat exchanger with a fixed effectiveness
(e = 0.54) . For extending the results, the effect of MFRR at different mass flow rates of the tube side (cold side)
_ c ¼ 5 kg=s.
are studied. The obtained results show that, the best results are obtained at the mass flow rate of m
Finally, using the definition of reflux ratio, its effect on optimum objective functions are derived and discussed.
© 2021 Taiwan Institute of Chemical Engineers. Published by Elsevier B.V. All rights reserved.
1. Introduction
Heat exchangers are devices that provide heat transfer flow
between two or more fluids at different temperatures. Shell and tube
heat exchangers, among others heat exchanger, have the most variety of shapes and applications in the industry (40% - 50%) [1].
Recently, energy problems are noticed in many countries. An increase
in energy consumption, energy cost, energy safety, competitive market of energy among countries, increase in greenhouse gases emission, and environmental problems are now serious issues for all
countries. Energy-saving and storage are the main economic goal of
the world. Using various theories for enhancing the technical and
economical function of industrial equipment including heat exchangers has been noticed by many researchers worldwide. Recovery
effects can play a very important role in the thermal design of industrial equipment and heat and mass transfer processes. These studies
are categorized in three kind including, experimental, numerical and
both of experimental and numerical analysis. For example, Pandiyarajan et al. experimentally investigated the heat recovery from diesel
engine exhaust adopting thermal storage system and finned STHE
* Corresponding author. Mohammad Shafiey Dehaj, Department of Mechanical Engineering, Vali-e-Asr University of Rafsanjan, TelFax: +98-34-31312499
E-mail address: m.shafiey@vru.ac.ir (M. Shafiey Dehaj).
[2]. Their experimental results revealed that approximately 10%-15%
of heat is recovered with storage system. Recovery of the waste heat
from a diesel engine using two STHEs available in the market is
examined by Bari and Hossain [3]. They used water as the working
fluid. Their results showed that excess power increases from 16 to
23.7 after the optimization process. Lu et al. was performed experimental inquiry on thermoelectric generator for waste heat recovery
(WHR) [4]. Their experimental results showed the net power
strengthened remarkably by employ of winglet vortex generators.
WHR processes can be classified according to their temperature
range including high temperature, low temperature, and mean temperature. For a precise and proper analysis of every industry and process, temperature classification is a very useful method in selecting
various technologies including the WHR. For example, Bernardo et al.
experimentally studied the organic Rankine cycle for low grade WHR
in a ceramic industry [5]. Their results presented that maximal cycle
performance gained are a gross electrical effectiveness of 12.47 % and
a net electrical effectiveness of 10.94 %. Hongting et al. experimentally studied on heat pipe reinforced heat exchanger handled for
industrial waste heat recovery [6]. The results showed that the thermal effectiveness parameters of the HPHE reduced with running time
of the system.
In the case of numerical analysis, Lin et al. analytically investigated the influence of the recycle effect on heat transfer to the
https://doi.org/10.1016/j.jtice.2021.05.022
1876-1070/© 2021 Taiwan Institute of Chemical Engineers. Published by Elsevier B.V. All rights reserved.
Please cite this article as: B. Masoumpour et al., Performance evaluation of a shell and tube heat exchanger with recovery of mass flow rate,
Journal of the Taiwan Institute of Chemical Engineers (2021), https://doi.org/10.1016/j.jtice.2021.05.022
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Nomenclature
Ao
af
cp
C*
Cmin
Cmax
di
do
f
ir
h
K
j
L
np
Nt
Nu
NTU
pt
Pr
R
Re
Rf
T
U
zop
zinv
Tube side flow cross section area(m2)
Annualized factor (–)
Specific heat (J/kg. K)
Heat capacity rate ratio
Minimum of Ch and Cc (W/K)
Maximum of Ch and Cc (W/K)
Tube inside diameter (m)
Tube outside diameter (m)
Fanning friction factor (-)
Interest rate (−)
Heat transfer coefficient (W/ m2 K)
Thermal conductivity (Wm−1K−1)
Colburn factor (−)
Tube length (m)
Number of tube pass (−)
Tube number in cross section (−)
Nusselt number (-)
Number of transfer units (-)
Tube pitch (m)
Prandtl number (-)
Reflux ratio (-)
Reynolds number (-)
Fouling resistance (K .m2/W)
Temperature (K)
Overall heat transfer coefficient (W/ m2 K)
Operational cost ($/year)
Investment cost ($)
Greek abbreviation
m
Viscosity (kgm−1s−1)
ΔP
Pressure drop (kpa)
hp
Pump efficiency (-)
r
Density (kg/ m3)
e
Effectiveness (-)
t
Hours of operation per year (hour)
s
Ratio between Aflow and Afront
fel
Unit price of electricity ($/kWh)
studied to reveal the effects of external recycles on HEs with different configurations [11-13]. On the other, several researchers performed the influence of external recycles on different boundary
conditions [14-16].
As it is mentioned, in some research, both experimental and
numerical analysis were carried out. For instance, Kandilli and Koclu
evaluated the optimum operation conditions of PHE for WHR in textile industry and employed first and second-law analysis [17]. Their
results showed that enhancing the waste water mass flow rates
flow rates at constant cold water mass flow rate can increase the
ration of heat transfer. Ma et al. investigated the characteristics of a
HPHE employed for recovering the waste heat in a slag cooling process in steel industry using both experimental and numerical methods [18]. Their experimental and numerical results revealed that the
heat transfer effectiveness considerably improved after using the
on-line cleaning device. Jouhara et al. described the design, construction and examining of an innovative heat recovery system
based on a Flat Heat Pipe HE [19]. Their results concluded that the
FHP is an innovative maximum performance technology for WHR.
Gu et al. studied the organic Rankine cycle (ORC) for a WHRS by
both theoretical and experimental [20]. It was demonstrated that
the maximal cycle performance of the Appling system is 5.2 %, and
the testing result as well as affirms that cycle performance is insentient to heat source temperature, but sentient to evaporating pressure. Tryfon et al. investigated the effectiveness of a custom made
subcooler was experimentally and CFD analytically [21]. The experimental results proved that the new obtained formula predicts an
acceptable functionality for the system with an average relative
error of 0.2% and maximum relative error of 1.8%. In addition, a
numerical simulation was performed for the same heat exchanger.
Yang et al. applied a novel full-open absorption heat pump to
recover heat from a flue gas using both experimental and theoretical
investigation [22]. It was indicated that theoretical investigation
approbates well with the experimental results. Brough et al. investigated heat pipe heat exchanger to recover surface heat base on
numerical simulation (TRNSYS software) and experiment [23]. In
some more new research, numerical analysis also optimization is
carried out. For instance, Sanaye and Hajabdollahi investigate the
multi-objective optimization of STHE for improving the effectiveness
[24]. Their results indicated the level of contrast between
Subscripts
i
Inside or tube side
c
Cold side
h
Hot side
o
Outside or shell side
s
Shell
t
Tube
power-law fluids from a double-pass parallel plate heat exchanger
with uniform wall temperature [7]. Analytical results indicated that
the recycle effect can effectively increase the effectiveness compared
with that in a single-pass. Evaluating the effectiveness of a baffled
solar air heater with external recycle was investigated by Mohammadi and Sabzpooshani [8]. Their results were performed for various
mass flow rates. HO and Chen theoretically external recycle (ER) in
the double-pass sheet-and-tube solar water heater to enhance the
collector effectiveness [9]. Their results revealed that collector effectiveness improved in the case of recycle effect in comparison to single-pass device for the same flow rate. Heat transfer improvement
for the power-law fluids through a parallel-plate double-pass HEs
with recycle effect was solved analytically by Lin et al [10]. The
numerical results showed that the recycle ratio and impermeable
sheet play remarkable effects on the performance of the heat transfer as compared to that in a single pass. Some other research was
Fig. 1. Schematic of shell and tube heat exchanger with E type of shell. a) Without
recovery or conventional heat exchanger, b) With recovery or reflux.
Please cite this article as: B. Masoumpour et al., Performance evaluation of a shell and tube heat exchanger with recovery of mass flow rate,
Journal of the Taiwan Institute of Chemical Engineers (2021), https://doi.org/10.1016/j.jtice.2021.05.022
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effectiveness and total annual cost. Some another authors have been
done that showed the application of waste heat recovery in different
types of heat exchangers, such as cross-flow heat exchanger [25]
and Compact heat exchangers [26]. Some other works, numerically
analysis have studied the effects of waste heat recovery in the heat
exchanger from the thermoelectric [27] and thermo-economic [28]
optimization viewpoint.
There are three aims in the present paper: first, to extend the
numerical simulation for a shell and tube heat exchanger with mass
flow rate recovery(MFRR) and study the recovery effects on the
thermo-economic optimization; second, effectiveness and total
annual cost (TAC) are considered as objective functions and nine
design parameters are selected; third, to investigate variations of
objective functions versus some important parameters such as temperature distribution, reflux ratio, cost, and the results are obtained
and discussed.
2. Thermal modeling
There are some various kinds of shells such as E, F and kinds
used in various applications. In this paper, E kind of shell (which is
the most common type of shell) in TEMA standard (Tubular
exchanger manufacturing association), as shown in Fig. 1a, is
selected. As it is mentioned, the main contribution of this paper is
studying the mass flow rate recovery as shown in Fig. 1b. For this
purpose, an additional line is provided to reflux some part of fluid
from outlet to the inlet. Because of pressure loss in the heat
exchanger, an additional pump is required which work in the steady
state condition. Effectiveness in terms of number of transfer units
(NTU) and heat capacity ratio (C*) for this kind of shell and tube
heat exchanger was estimated from [1]:
e¼
2
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
r
r
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
ffi
ffi 2
ð1 þ C Þ þ
1þC
Coth 0:5 NTU
1 þ C2
ð1Þ
resistances, tube inside diameter, tube wall conductivity and tube
inside fouling resistances, respectively. In addition, hi and ho are tube
and shell side convection heat transfer coefficients which are presented in the following sub-sections
2.1. Heat transfer coefficient and friction factor in tube side (cold side)
R¼
_R
m
_ i;primary
m
ð10Þ
For thermal analysis of the MFRR from the cooling fluid and reflux
direction from the outlet to the inlet, a parameter called reflux ratio
(R) is used, which is defined as follows:
Outlet pressure and flow stability are two important parameters
which may be affected by refluxing. The mentioned parameters are
more important in the case of gas stream with high rate of refluxing.
To avoid the mentioned negative effects, the liquid based heat
exchanger with the reasonable reflux ratio are selected.
Formulation of tube side inlet mass flow rate of STHE are obtained
as:
_ i;t ¼ ð1 þ RÞm
_ i;primary
m
ð11Þ
_ R ،m
_ i;t and m
_ i;primary are reflux direction mass flow rate, total
where m
inlet mass flow rate and primary inlet mass flow rate, respectively.
Convection heat transfer coefficient in the tube side is obtained as
following equations [30]:
2300 < Re104
ð12Þ
0
1
f ðRe 1000ÞPr C k
B
qffiffi
h¼@ 2
A
1 þ 12:7 2f ðPr0:67 1Þ di
Re > 104
ð13Þ
0
in which C*and NTU are defined as:
C
C ¼ min
Cmax
ð2Þ
_ p Þc ; ðmc
_ p Þh ÞandC max ¼ maxððmc
_ p Þc ; mc
_ p Þh Þ
Cmin ¼ minððmc
ð3Þ
3
B
h¼@
1
1:07 þ
900
Re
Re Pr 2f
C k
qffiffi
A
f
0:67
1Þ di
ð0:63=ð1 þ 10 PrÞÞ þ 12:7 2ðPr
f is friction factor which is estimated from formula (12 and 13).
2
f ¼ ð1:58 logðReÞ 3:28Þ
Uo A O
NTU ¼
Cmin
ð4Þ
e ¼ Q=Q max
ð5Þ
_ and cp are the mass flow rate and the specific heat capacity,
where m
the subscripts h and c indicates hot-side and cold-side, respectively.
The effectiveness can be determined using the following definition
[1]: in which Q is rate of heat transfer and obtained as follows using
the first law of thermodynamic:
_ p c Tc;out Tc;in ¼ mc
_ p h Th;in Th;out
Q ¼ DHc ¼ DHh ¼ mc
ð6Þ
Q max ¼ Cmin DTmax ¼ Cmin Th;in Tc;in
ð7Þ
where Qmax is maximum rate of heat transfer and calculated with the
following formula: where AO is the total tube outside heat transfer
surface area and Uo is the overall heat transfer coefficient which are
computed from [1]:
Ao ¼ At ¼ pLdo Nt
Uo ¼
ð8Þ
1
1
ho
þ Ro;f þ
do lnðdo =di Þ
2kw
þ ddoi Ri;f þ ddoi h1i
ð9Þ
where L ، do, Nt ، Ro,f, di ، kw and Ri,f are tube length in each pass, tube
outside diameter, tube number in cross section, tube outside fouling
2300 < Re104
ð14Þ
f ¼ 0:00128 þ 0:1143 ðReÞ0:311 Re > 104
ð15Þ
Where Pr, f, k are Prantel number, friction factor and fluid conductivity, respectively.
In addition, Re is Reynolds number and in the with and without
MFRR are defined as:
Ret ¼
_ i;primary
4np ð1 þ RÞm
Nt pdi mt
ð16Þ
Ret ¼
_ i;primary
4np m
Nt pdi mt
ð17Þ
In the above equations, npand m are number of tube pass and viscosity in the tube side.
!
np
4fl 2
2
DPt ¼ m_
þ
1
s
þ
K
s
K
DPrecovery
1
c
e
di
2rt Ao 2
ð18Þ
In addition, pressure drop in the tube side is obtained as follows [1]
here r, Kc, Ke and s are the tube side density, tube inlet and outlet
Please cite this article as: B. Masoumpour et al., Performance evaluation of a shell and tube heat exchanger with recovery of mass flow rate,
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pressure drop coefficients as well as ratio of minimum free flow area
to the frontal area, respectively. Furthermore, Ao is tube side flow
cross section area in each pass defined as [1]:
pdi 2 Nt
Ao ¼
ð19Þ
4
np
2.2. Heat transfer coefficient and pressure drop in shell side
In this research, Bell-Delaware technique is applied to obtain the
coefficient of heat transfer and pressure drop in the shell side [29]. In
this technique, an ideal heat transfer coefficient for cross flow stream
in the tube bundle is estimated and improved with some correction
factors. Ideal heat transfer coefficient in the shell side is obtained
as [29]:
0:67 _
ks
ms 0:14
m
hid ¼ js Cp
ð20Þ
As
C p ms
msw
here As, ks and ms are cross flow area at near the shell centerline, fluid
conductivity and viscosity in the shell side, respectively. Moreover,
msw is shell side viscosity at wall temperature and js is ideal Colburn
factor in the shell side estimated as [29]:
1:33 a
ðRes Þa2
ð21Þ
js ¼ a1
Pt =do
a¼
a3
1 þ 0:14ðRes Þa4
Res ¼
As ¼
_
do m
A s ms
Ds
ðPt do ÞBS
Pt
2.3. Economic Analysis
In this research, two objective functions including the effectiveness of the STHE or effectiveness and TAC are considered for the optimization problem. The TAC of the system is included of the
operational cost and investment cost. Effectiveness is obtained in
Eq. 1 and TAC is described in the below form [24]:
TACð=yearÞ ¼ af Zi þ Zop
Zi ¼ 8500 þ 409 At 0:85
af ¼
ð30Þ
ð31Þ
ir
n
1 ð1 þ irÞ
ð32Þ
where af, Zi, ir and n are annualized factor, investment cost, interest
rate and depreciation time, respectively. In addition, the total operating cost related to pumping power to overcome friction losses of
both hot and cold streams was computed from [24]:
Zop ð=yearÞ ¼ ðDPt þ DPs þ DPrecovery Þ ’el t
P¼
_
m
rhp
ð33Þ
DP
ð34Þ
ð22Þ
where subscripts t and s indicate the tube and shell side. Moreover,
hp, feland t are isentropic effectiveness of pump, unit price of electricity and hours of system operation in a year, respectively.
ð23Þ
3. Fitness functions, design parameters and constraints
ð24Þ
here Pt, Res and BS are tube pitch, shell side Reynolds and baffle spacing, respectively. In addition, a1-a4 are constants and depend on the
Reynolds number and tube arrangement and are obtained by BellDelaware team [29]. Furthermore, where Ds is considered as shell
diameter and obtained as follow [29]
rffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
4 Nt CL
Ds ¼ Pt
ð25Þ
p CTP
where CL and CTP are tube layout and tube count constants, respectively which depend on the tube arrangement and pass. Shell side
heat transfer coefficient is modified by having ideal heat transfer
coefficient and some correction factors as follows [29]
ho ¼ hs ¼ hid ðJc JI Jb Js Jr Þ
pressure drop, Colburn factor, friction factors and constants in relations 21-22 and 27-28, are referred to references [1, 29]
ð26Þ
where Jc, JI, Jb, Js and Jr are correction factors related to the baffle configuration, baffle leakage, bundle/pass partition bypass streams, inlet/
outlet baffle spacing and adverse temperature gradient, respectively.
Friction factor is also evaluated as follows [29]:
!b
1:33
f s b1
ðRes Þb2
ð27Þ
pt
Using the flow reflux direction for the cold fluid has two opposite
effects. Increasing the mass flow rate of the clod fluid, and the Reynolds number, which in turn increases the overall heat transfer coefficient, have a very favorable effect on the thermal performance of
the system. On the other hand, the increase in mass flow rate because
of the increase in operational cost, due to the increase in pump power
consumption, has a conflicting effect on the heat exchanger. To evaluate the conflicting effects of thermo-economic, effectiveness and total
annual cost (TAC) are selected as two objective functions. In this
work, tube arrangement, tube diameter, tube pitch ratio (ratio
between tube pitch and tube outside diameter), tube length, tube
Table. 1
Variation range of design parameters
Design parameter
Lower bound
Upper bound
Tube arrangement (degree)
Tube inside diameter (mm)
Tube pitch ratio (pt/do)
Tube length in each pass (m)
Tube number (-)
Baffle spacing ratio (BS/Ds)
Baffle cut ratio (BC/Ds)
Reflux ratio (-)
Recovery direction diameter (mm)
10.3
1.25
3
100
0.2
0.19
0
10.3
30°-45° -90°
17.3
2
8
800
1.4
0.32
1
17.3
do
b¼
b3
b4
1 þ 0:14ðRes Þ
ð28Þ
here b1-b4are constants and depend on the Reynolds number and
tube arrangement. Finally, the total pressure drop in the shell side is
estimated as follows:
Dps ¼ Dpcr þ Dpi=o þ Dpw
ð29Þ
where Dpcr, Dpi/o and Dpware pressure drop in cross-flow, inlet/outlet and window part, respectively. The details for computation of
Table. 2
Input data for modeling and optimization [24].
Parameter
Value
Water fouling resistance (m2. W/K)
Oil fouling resistance (m2. W/K)
Interest rate (–)
System life time (year)
Hours of operation in year (h)
Price of electrical energy ($/kW h)
Pump effectiveness (–)
0.000074
0.00015
0.10
10
5000
0.02
0.6
Please cite this article as: B. Masoumpour et al., Performance evaluation of a shell and tube heat exchanger with recovery of mass flow rate,
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number, baffle spacing ratio (ratio between baffle spacing and shell
inside diameter), baffle cut ratio (ratio between baffle cut and shell
inside diameter), as well as reflux ratio and recovery direction diameter are considered as nine design parameters and listed in Table. 1 are
selected. The standard size of the tube’s internal and external diameters is presented in the appendix.
The constraint is also considered as follows:
3<
L
< 12
DS
5
Table. 3
Constants considered in the Eq. (36)
ð35Þ
In addition, input parameters listed in Table 2 are considered for
numerical simulation.
Parameter
With recovery
Without recovery
α1
α2
α3
α4
α5
β1
β2
β3
β4
-595.1
-284.9
273.2
-193.9
312.9
71.61
-150
-170.3
167
774.9
-2406
1785
-1197
529.2
359.2
-35.74
-534.4
260.1
4. Case study
In this study, a verified code which was previously developed by
the author is used for modelling [24]. In fact, the details of verification are referred into the reference [24]. In this study, the fast and
elitism Non-Dominated Genetic Algorithm (NSGA-II) was applied to
find the effects of mass flow rate recovery (MFRR) to the tube side
in a shell and tube heat exchanger. The Oil with a mass flow rate of
10 kg/s and inlet temperature of 80⸰C is considered as shell side
(hot fluid), while water with a mass flow rate of 6 kg/s and inlet
temperature of 20⸰C is selected as tube side (cold fluid). Thermophysical properties of both side are considered as a function of temperature and concluded at the input and output average
temperature. Lastly, to extend the results, the optimization is also
carried out for various tube side (cold side) mass flow rates including 4, 5, 8 and 10 kg/s.
5. Discussion and results
In this research, the effect of fluid inlet parameters, including
mass flow rate and inlet temperature, on the optimal results of the
shell and tube heat exchanger has been investigated using the mass
flow rate recovery(MFRR) technique (reflux direction). It is worth
noting that the thermo-economic optimal results are presented after
3 repetitions and re-ranking. Utilizing this method leads to an
increase in the inlet temperature of the fluid, somehow of preheating,
which improves the thermal performance of STHE. Besides, establishing a reflux direction increases the inlet mass flow rate, and pump
power, and consequently, the operational cost is increased. Therefore,
to achieve the conflicting effect of MFRR on effectiveness and TAC, the
use of multi-objective algorithm becomes necessary. For this purpose, the geometry of the considered STHE is simulated, and the final
optimal results are obtained next. The NSGAII is applied for 1000
generations, using a search population size of 150 individuals, gene
mutation probability of 0.035, crossover probability of 0.9 and controlled elitism value of 0.5 and the results for the Pareto optimal front
are showed in Fig. 2. Also, to better understand the effect of MFRR on
optimal results, the results of cases with MFRR and without it are
compared.
The final optimal results (pareto front) for both cases of with and
without MFRR are shown in Figure 2 for hot and cold side mass
flow rate of 10 and 6 kg/s, respectively. The present results confirm
the enhancing effect of recovery on the thermo-economic characteristics of the shell and tube heat exchanger, which is indicated by the
dominance of the final optimal results in the case with recovery
over the optimal results in the case without it. Simply put, Figure 2
illustrates that by installing a reflux direction to return cold fluid
from the outlet to the inlet of the STHE, effectiveness and the TAC of
the STHE increase and decrease, respectively, which are desired, and
shows that the constructive effect of the recovery has been
achieved.
MFRR, on the one hand, increases the inlet mass flow rate of the
heat exchanger and consequently increases the Re number, overall
heat transfer coefficient, and on the other hand, is associated with
favorable changes in C*(Reduce C*). These are two important factors
that enhance thermal effectiveness. Formula 36 is calculated in
order to find the relationship between effectiveness and TAC in the
optimal position for the points presented in Figure 2 for the two
cases of the conventional heat exchanger and recovered one, respectively with the constants listed in Table 3. Equation 36 is valid for an
effectiveness value of 0.1168 e 0.6483 and a TAC of 2088.1 TAC 8808.9 for the MFRR. The above equation can also be used for
the effectiveness value of 0.1190 e 0.6128 and the TAC of
2082.6 TAC 10227 for the conventional exchangers. The above
equation calculates the minimum values of the TAC (optimal TAC)
for a given effectiveness. Also, the validation of the extracted relationship with the optimal results presented in Figure 2 has been
performed for the state without and with recovery in Figure 3 a and
3b, respectively.
TAC ¼
Fig. 2. Pareto optimal fronts for both studied cases
a1e4 þ a2e3 þ a3e2 þ a4e1 þ a5e0
1000
b1e3 þ b2e2 þ b3e1 þ b4e0
ð36Þ
Variation of objective functions in terms of mass flow rate recovery (MFRR)
The optimal values of the design parameters and objective functions for the five sample points of a-e presented in Figure 2 for the
conventional heat exchanger and the recovered one are listed in
Tables 4 and 5, respectively. As it can be seen in these tables,
because of mass reflux in the case of recovery, generally higher tube
number are selected in this case as compared with conventional
case. In fact, the net tube side mass flow rate in the case of reflux
Please cite this article as: B. Masoumpour et al., Performance evaluation of a shell and tube heat exchanger with recovery of mass flow rate,
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Fig. 3. . Comparison of TAC between the result in results in figure 2 and equation 36. (a) Without recovery (b) with recovery
Table. 4
Design parameters and objective functions for five optimum points a-e in Fig. 2 in the case of with recovery
Design parameter
(a)
(b)
(c)
(d)
(e)
Tube arrangement (°)
Tube number (–)
Tube pitch ratio (pt/do)
Tube inside and outside diameter (m)
Tube length in each pass (m)
Baffle spacing ratio (BS/Ds)
Baffle cut ratio (BC/Ds
Reflux ratio (-)
Recovery direction diameter (mm)
Effectiveness (-)
TAC ($/year)
Tube side Reynolds number (-)
45
576
1.2610
0.0052-0.0063
7.1961
0.2283
0.2206
0.1945
0.0196-0.0220
0.6445
8757.4
4304.2
45
473
1.3043
0.0052-0.0063
5.4362
0.3606
0.2655
0.2028
0.0203-0.0220
0.5959
5775.8
5061.1
45
414
1.2654
0.0052-0.0063
4.9613
0.4929
0.3139
0.1975
0.0203-0.0220
0.5641
4943.9
5528.3
45
271
1.2500
0.0052-0.0063
3.8961
0.9370
0.3195
0.1896
0.0203-0.0220
0.4433
3386.5
7426.8
45
186
1.2725
0.0052-0.0063
3.0354
1.3717
0.2604
0.1222
0.0196-0.0220
0.3119
2608.6
9353.5
Table. 5
Design parameters and objective functions for five optimum points a-e in Fig. 2 in the case of without recovery
Design parameter
(a)
(b)
(c)
(d)
(e)
Tube arrangement (°)
Tube number (–)
Tube pitch ratio (pt/do)
Tube inside and outside diameter (m)
Tube length in each pass (m)
Baffle spacing ratio (BS/Ds)
Baffle cut ratio (BC/Ds
Reflux ratio (-)
Recovery direction diameter (mm)
Effectiveness (-)
TAC ($/year)
Tube side Reynolds number (-)
45
544
1.2823
0.0052-0.0063
7.1729
0.200
0.3103
0.6068
8657.6
4034.8
45
377
1.2852
0.0052-0.0063
6.0698
0.3470
0.2614
0.5650
5800
5036.6
45
364
1.2566
0.0052-0.0063
5.1496
0.4740
0.2680
0.5332
4943
5089.0
45
269
1.2933
0.0052-0.0063
3.8461
0.7858
0.3038
0.4229
3354.0
5917.2
45
188
1.2727
0.0052-0.0063
3.1282
1.3150
0.2680
0.3175
2655.0
7992.0
increases and optimization algorithm adjusted the tube number
higher to moderate the Reynolds number and pressure drop. Considering the values of tube side Reynolds number in these tables, verified
this point. Figure 4 shows the changes in effectiveness and TAC with
the reflux ratio for the five sample points of a-e. It can be seen from
Figure 4 that the trend of changes in both objective functions is incremental, but this trend is linear for the effectiveness while following
the nonlinear trend for the TAC. Reflux ratio is directly related to C*
and Re number. On the one hand, according to Equation 12 and 13,
the increase in the reflux ratio has increased the heat transfer coefficient of the tube side, and with the increase of this important thermal
parameter, overall heat transfer coefficient and NTU increase according
to Equations 9 and 4, respectively. On the other hand, according to
Equation 2, C* has also decreased, Therefore both factors have helped
to increase the thermal effectiveness and ultimately have increased
the shell and tube heat exchanger performance.
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Fig. 4. Objective functions variations respect to reflux ratio for typical five optimal points a-e in Fig. 2.
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Fig. 5. Percentage improvement in objective function versus reflux ration ratio for typical five optimal points a-e in case of recovery. (A) Percent variation of effectiveness versus
reflex ratio. (B) Percent variation of TAC versus reflux ratio.
It is noteworthy that the reflux ratio due to the increase in
pump power consumption is directly related to the TAC, such that
with its increase, this economic parameter, especially at high values of reflux ratio, is associated with a significant increase, which
is unfavorable. According to Eqs. 14 and 15, although the ft is
decreased, the pressure drop in the tube side of the heat
exchanger is increased with increasing the reflux ratio. On the
other hand, the pressure drop of the reflux direction, as an effective parameter, also contributes to the increase in pump power
consumption and unfavorably leads to an increase in the operational cost due to the fixed initial cost, it increases the total annual
cost. To better understand the presented figures in Fig.4, the percentage of objective functions changes with the reflux ratio is
shown in Fig. 5A and Fig. 5B for five sample points of a-e. The variation trend of effectiveness is almost the same for all five points.
However, point A has the highest slope and then B, C, D and E.
Besides, the slope of the TAC curve is adversely the highest for
point E and then is D, C, B and A, respectively.
In fact, Fig. 5 indicates that for a constant reflux ratio, a heat
exchanger with higher effectiveness experiences more difference in
the effectiveness and a lower increase in TAC. For example, when the
reflux ratio is increased to R = 1, the effectiveness and the TAC of
point A, are increased %22 and %76, respectively, while for the same
reflux ratio, the values are %9 and %122 for point E. According to the
presented results, the application of MFRR is not recommended for
low-effectiveness STHE.
In the continue, the recovery effect of the mass flow rate was
presented and compared on the thermo-economic and hydraulic
specification such as Zop,AO, Zi and ft of the heat exchanger with
and without recovery under the optimal condition (fig 6a- fig6d).
The direct relation between the reflux direction with the tube side
Reynolds number can alter the thermo-economic and hydraulic
parameters of the STHE. An increase in the Reynolds number of
the tube side will enhance the overall heat transfer coefficient and
number of transfer units (NTU); thus maintaining a constant effectiveness requires lower total heat transfer surface area heat
exchanger and hence lower volumes. Moreover, according to
Eq 31, the initial cost of the heat exchanger will also decline due
to the decrement in the total heat transfer surface area. On the
other hand, at the recovery state, although the ft decreased due to
the increase in Reynolds number, the pump power was enhanced
due to the establishment of the reflux direction which will increment the operating cost. In fact, the increase in the power consumption of the pump can be regarded as a negative effect of flow
recovery.
Output temperature is one of the important parameters in the
design of an optimal heat exchanger. Having the effectiveness of the
heat exchanger and input parameters of the fluid, the output temperature of the exchanger can be determined by Eq 5, These parameters are presented for the optimal points. They are also depicted in
Fig 7 for the cases with and without recovery, respectively (fig 7a
and fig 7b). The variation of the effectiveness with the output temperature was linear for both cases. The highest temperature difference of the fluid occurred at the maximum effectiveness giving rise
to the highest output temperature of the cold fluid and the lowest
output temperature of the hot fluid. Moreover, the proportionality
of the effectiveness with the output temperature concludes the
presence of an optimal temperature for each effectiveness. As mentioned before, the application of a recovery system can enhance the
thermal performance, giving rise to higher effectiveness and hence
higher temperature of the clod fluid and lower temperature of the
hot one.
To generalize the results, the optimization was carried out at various cold side mass flow rate (varying the input rate ending up to the
_ c ¼ 4 kg
_
_
_
recovery) including m
s ; mc ¼ 5 kg=s, mc ¼ 8 kg=s and mc ¼
10 kg=s. Fig. 8 shows the optimal final effectiveness vs. the TAC. Generally, the results indicate an improvement in the final optimal points
(pareto front) of the case with recovery as compared to the without
recovery. According to Fig. 8, at high and low mass flow rate of the
cold side, the recovery of the mass flow rate did not significantly
affect the objective function (effectiveness and TAC). Moreover, the
_ c ¼ 5 kg=s with recovery case dominated
final optimal points at m
those of the without recovery case which can be inferred as a
thermo-economic improvement.
For further investigation of the differences at various cold side
mass flow rates, the variations in the effectiveness/TAC were calculated at constant TAC/effectiveness as depicted in Fig. 9. It
must be noted that due to the same pareto front at mass flow
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Fig. 6. Distribution of some important parameters vs objective function for the optimum results in Fig. 2. (a) Heat transfer area vs effectiveness. (b) Investment cost vs effectiveness.
(c) Friction factor vs effectiveness. (d)Operational cost vs TAC.
Fig. 7. Distribution of outlet temperature versus effectiveness on each side for the Pareto optimal front in fig2. (a) with recovery. (b) without recovery.
Please cite this article as: B. Masoumpour et al., Performance evaluation of a shell and tube heat exchanger with recovery of mass flow rate,
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Fig. 8. Optimal Pareto fronts in the case of recovery and without recovery for different rates of cooling fluid.
(a). 4 kg/s, (b). 5 kg/s, (c). 8 kg/s, (d) 10kg/s
Fig. 9. Percent of variation in objective functions for the case of recovery and for various mass flow rate. (a) Percent variation of TAC versus effectiveness. (b) Percent variation of
effectiveness versus TAC
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Fig 10. variation in objective functions for the case of recovery and for various reflux ratio(R). (a) variation of effectiveness versus hot fluid inlet temperature. (b) variation of TAC
versus hot fluid inlet temperature. (c) variation of effectiveness versus cold fluid inlet temperature. (d) variation of TAC versus cold fluid inlet temperature. (e) variation of effectiveness versus hot mass flow rates. (f) variation of TAC versus hot mass flow rates. (g) variation of effectiveness versus hot mass flow rate in R=0.6.
Please cite this article as: B. Masoumpour et al., Performance evaluation of a shell and tube heat exchanger with recovery of mass flow rate,
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_ c ¼ 4 kg=s and m
_ c ¼ 10 kg=s, their results were ignored
rates of m
to avoid irregularity in the figure. Generally, the improvement in
the TAC was more significant at high efficiencies (a considerable
increase in the slope at high efficiencies). Moreover, the desirable
_ c ¼ 5 kg=s followed by
economic properties were observed at m
_ c ¼ 6 kg=s and m
_ c ¼ 8 kg=s. For example, the
mass flow rates of m
_ c ¼ 5 kg=s in constant effecTAC experienced a 24% decrease at m
tiveness (e = 0.54) while the percentage in the improvement of the
TAC was 11% and 8%, respectively. The same trend can be observed
for the thermal effectiveness as the best results were observed at
_ c ¼ 5 kg=s.
m
Fig. 10 shows the sensitivity analysis of the objective functions for
similar input conditions (mass flow rate and inlet temperature) and
various reflux ratio include R = 0, R = 0.3, R = 0.6 and R = 1. By an
increment in the hot fluid temperature, its viscosity changed, which
enhanced the Re number of the shell side; hence increasing the heat
transfer coefficient of that side. By installing a reflux direction to
recover and increase the reflux ratio, the Re number of the tube side
also enhanced giving rise to an increment in the heat transfer coefficient of the tube side. Regarding the rise in the heat transfer coefficient at both sides, the highest difference in the effectiveness occurs
at high reflux ratio and hot side temperatures. Also, the changes in
the input temperature of the hot and cold fluid had no significant
influence on the TAC. An increase in the reflux ratio, however, is
accompanied by a rise in the pressure drop due to the increase in the
mass flow rate of the cold side which will increment the operating
cost and hence enhance the TAC. It must be noted that the increase in
the mass flow rate of the hot side (shell side) will increase the pressure drop in that side. An increase in the reflux ratio also caused the
same trend in the cold side (tube side), giving rise to an increment in
the TAC.
The variation trend of the effectiveness with the mass flow rate of
the hot fluid showed an inflection point at all reflux ratio. For the
points before the inflection point, an increase in the mass flow rate of
the hot side increased the C* due to the increased Cmin at constant
Cmax (Eq2), This will decline the effectiveness. After the inflection
point, an increase in the mass flow rate of the hot side at constant
Cmin, increased the Cmax parameter which decreased the C* parameter and hence increased the effectiveness. Therefore, any changes in
the mass flow rates of the hot or cold sides can negatively affect the
thermal performance if accompanied by an increase in the C* parameter and vice versa. Regarding the input conditions of both fluids, as
the recovery of the mass flow rate will further increase the difference
between Cs and Ct (Cs<Ct), it will shift the inflection point at higher
mass flow rates of the hot fluid. the higher the reflux ratio, the inflection point will occur at higher mass flow rates of the hot fluid. For a
better understanding of the mentioned points, the variations in the
effectiveness are plotted versus the mass flow rate(R = 1) of the hot
side in Fig. 10g.
6. Conclusion
In this research, the effect of mass flow rate recovery(MFRR) using
reflux direction on thermo-economic optimizing the shell and tube
heat exchanger(STHE) is investigated and compared to the case without recovery. For this purpose, effectiveness and TAC were selected
as two objective functions and nine design parameters were considered in this study.
The most significant findings of this study are presented in the
following:
Thermo-economically, the best optimal thermal effectiveness and
_ c ¼ 5 kg=s followed by m
_ c ¼ 6 kg=s and
TAC were observed at m
_ c ¼ 8 kg=s:
m
Almost the same final optimal points (pareto front) at high and
_ c ¼ 4 and m
_ c ¼ 10 kg=sÞ indicate the
low mass flow rates (m
ineffectiveness of the studied solutions at the mentioned mass
flow rates.
The objective functions (effectiveness and TAC) followed an
ascending trend with the recovery of mass flow rate. This trend
was linear for the effectiveness while showed a nonlinear behavior in terms of TAC.
The sensitivity analysis of the thermo-economic properties with
the reflux ratio indicated a higher difference in the effectiveness
and a lower increase in the TAC in a constant reflux ratio for heat
exchanger with higher effectiveness. Therefore, the use of recovery is not recommended for heat exchanger with low effectiveness.
The growth in the input mass flow rate as a result of the reflux
direction installation caused an increase in the Reynold number of
the tube side with enhanced the heat transfer coefficient. Therefore, at constant effectiveness and NTU, it required lower heat
transfer and initial cost.
In the case of recovery, although the friction factor declined due to
the increase in Reynold number, the power consumption of the
pump also incremented due to the installation of a new reflux
direction (negative effect of the MFRR) which will adversely influence the operating cost.
An increase in the mass flow rate of the tube and shell side
increased the pump power consumption due to the pressure
drop. The increment in the reflux ratio the mentioned factor
which considerably enhanced the operating cost and TAC of the
heat exchanger at high input mass flow rates of both fluids and
higher recovery rates.
The variations in effectiveness vs. cold or hot fluid mass flows had
an inflection point. The application of the MFRR dependent on the
C* parameter changed the inflection point. Therefore, any alterations in the input mass flow rates can negatively influence the
thermal performance if increments the C*parameter and vice
versa.
Declaration of Competing Interest
None.
Appendix
Table 6
Table. 6
Thirty-eight standard diameter considered in inch dimension [1]
(0.194, 1/4)
(0.331, 3/8)
(0.435, 5/8)
(0.555, 5/8)
(0.606, 3/4)
(0.635, 7/8)
(0.805, 7/8)
(0.206, 1/4)
(0.370, 1/2)
(0.481, 5/8)
(0.482, 3/4)
(0.620, 3/4)
(0.657, 7/8)
(0.214, 1/4)
(0.402, 1/2)
(0.495, 5/8)
(0.510, 3/4)
(0.643, 3/4)
(0.685, 7/8)
(0.277, 3/8)
(0.430, 1/2)
(0.509, 5/8)
(0.532, 3/4)
(0.352, 3/4)
(0.709, 7/8)
(0.67, 1)
(0.305, 3/8)
(0.444, 1/2)
(0.527, 5/8)
(0.560, 3/4)
(0.680, 3/4)
(0.745, 7/8)
(0.319, 3/8)
(0.407, 5/8)
(0.541, 5/8)
(0.584, 3/4)
(0.607, 7/8)
(0.777, 7/8)
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