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Purpose

The aim of this study is to evaluate the thermal performance of a triple-tube heat exchanger equipped with staggered fins for food processing. Challenges arise due to the high viscosity of non-Newtonian fluids treated in the food industry, which lead to laminar flow and limited thermal penetration. This research focuses on enhancing heat transfer efficiency and improving fluid thermal mixing using passive heat transfer enhancement methods in a triple-tube heat exchanger.

Design/methodology/approach

Numerical simulations, implemented within an ANSYS© Fluent environment, are used to solve the equations governing the thermofluid dynamics of a triple-tube heat exchanger with staggered fins in the internal annulus. The rheological behavior of tomato concentrate is modeled by means of a power-law model, coupled with the Arrhenius law to introduce temperature dependency of the consistency index. Experimental validation is adopted to verify simulations accuracy.

Findings

The finned configuration enhances heat transfer and improves thermalization by induced swirling flows and consequent boundary layers disruption. The geometrical configuration presenting eight-finned modules achieves a maximum performance index of 1.23 in the entrance region, while mitigating frictional effects. Moreover, such fins arrangement guarantees good thermal mixing.

Originality/value

This study represents one of the first attempts of enhancing heat transfer performance of a triple-tube heat exchanger for thermal processing of food products. The exceptionally low generalized Reynolds number and high generalized Prandtl number characterizing the treated fluid result in severe heat transfer limitations, tackled by a practical design strategy able to improve energy and thermal treatment efficiency.

A

= Constant (Pa sn);

Atot

= Total heat transfer area (m2);

Brg

= Generalized Brinkman number;

cp

= Specific heat (J/kg K);

d

= Distance between finned modules (m);

Dh

= Hydraulic diameter (m);

Di

= Inner diameter (m);

Do

= Outer diameter (m);

Ea

= activation energy (J/mol);

f

= Friction factor;

h

= Convective heat transfer coefficient (W/m2K);

K

= Consistency index (Pa sn);

k

= Thermal conductivity (W/mK);

L

= Length of the triple-tube passage (m);

l

= Length of the finned module (m);

Lc

= Curvilinear length of the sterilizer curve (m);

ṁ

= Mass flow rate (kg/s);

n^

= Unity vector (m);

n

= Flow behavior index;

Nu

= Nusselt number;

PD

= Percentage deviation (%);

Prg

= Generalized Reynolds number;

Q

= Heat transfer rate (W);

R

= Universal gas constant (J/mol K);

Reg

= Generalized Reynolds number;

T

= Temperature (K);

u

= Velocity vector (m/s);

W

= Average velocity (m/s);

x

= Axial coordinate (m);

α

= Thermal diffusivity (m2/s);

γ̇

= Rate-of-strain tensor (1/s);

ΔTml

= Logarithmic mean temperature difference (K);

δ

= Uncertainty;

η

= Performance index;

ηa

= Apparent viscosity (Pa s);

θ

= Dimensionless temperature;

ρ

= Density (kg/m3);

τ

= Shear stress tensor (Pa);

σ

= Temperature standard deviation (K); and

ψ

= Mixing parameter.

*

= Dimensionless;

b

= Bulk;

c

= Cold;

f

= Fluid;

h

= Hot;

in

= Section inlet;

out

= Section outlet;

s

= Solid;

wall

= Wall properties; and

0

= Reference conditions.

Innovation in the food machinery sector is currently driven by the demand for novel food processing techniques – both thermal and nonthermal – that ensure microbiological and chemical safety while preserving nutritional content and sensory qualities. At the same time, these processes must minimize energy consumption, thereby reducing the environmental impact of the entire food chain (Chakka et al., 2021).

A key element in food thermal processing is the Heat Exchanger (HE). This equipment must comply with strict safety standards to effectively inactivate microbes while maintaining the food’s nutritional and sensory properties. The design and optimization of HEs are critical: achieving uniform heat distribution, preventing contamination and minimizing thermal degradation are all essential goals (Tonyali Karsli and Cekmecelioglu, 2023).

These problems, which refer to forced convection heat transfer within internal flow configurations, imply the selection of a suitable passive enhancement strategy, a choice that is highly dependent on the established flow regime, primarily influenced by the fluid’s rheological properties and the geometrical features. When the laminar flow regime limiting boundaries cannot be overcome, the only possibility to passively enhance the heat transfer phenomenon is associated with solutions that force the fluid mixing, such as flow inserts (Bozzoli et al., 2021; Pagliarini et al., 2024a), twisted tapes (Zimparov et al., 2024) or other solutions aimed at promoting swirl flow components (Rainieri and Pagliarini, 2002). These additional geometrical solutions improve fluid thermalization without requiring external power (Bozzoli et al., 2020), but not all the listed methods are suitable for the food sector because fouling phenomena must be prevented or at least minimized (Schnöing et al., 2020). Another challenge arises from the complex rheological behavior exhibited by many food products, which is often associated with the laminar flow regime due to the high consistency index of food products (Myhan et al., 2012).

Heat transfer capability optimization relies on accurate modeling of the complex thermal fluid dynamics within the HE system. Advanced Computational Fluid Dynamics (CFD) simulations and predictive algorithms allow for detailed analysis of flow patterns and temperature distributions. By systematically adjusting geometric parameters, it becomes possible to quantify and implement improvements in heat transfer performance, comparing enhanced configurations to a baseline design [see, for instance, Vocale et al. (2019)]. The combination of experimental and numerical pieces of information becomes thus necessary for approaching the best strategy for topological and morphological optimization of the heat transfer sections with the aim of increasing the overall energy efficiency of industrial equipment (Bhattacharyya et al., 2022). Recent works dealing with the numerical analysis of heat transfer augmentation solutions in HEs via commercial software can be found, for instance, in Abbasian Arani and Moradi (2021) and Aytaç et al. (2023).

The above consideration holds for both double-pipe and triple-tube HEs (TTHEs). In particular, the latter systems stand as highly advantageous heat transfer systems, especially when the treated fluid presents high viscosity and complex rheological behavior, such as in the food thermal processing (García-Valladares, 2004; Malavasi et al., 2021). TTHEs present an additional annular passage, which consequently increases the heat transfer area. Large temperature gradients in the fluid are mitigated by such a geometrical configuration, thanks to its intrinsic capability of controlling the temperature difference between the process and the service fluids. Hence, enhancing heat transfer in TTHEs by means of passive methods is crucial to obtain even more efficient and cost-effective solutions for food processing.

While passive heat transfer enhancement methods for double-pipe HEs have been widely studied, only recently scholars have extended their application to the internal annulus of TTHEs by also relying on numerical approaches, given the practical unfeasibility of experimentally monitoring all the thermofluidic features of the treated flows.

Gomaa et al. (2017) were among the firsts to experimentally and numerically study the effect of rib inserts on the performance of a TTHE for hot water cooling. Different geometrical parameters were considered, including varying heights and pitches of ribs. Simulations were carried out to shed light on the thermofluid dynamics characterizing the system. The Nusselt number was assessed to undergo an increase of 21.48% with respect to the nonfinned geometry. The heat transfer per unit pumping power exhibited an increase of 32.49% for the counter flow. Higher ribs height and low pitch resulted in a slight increase in the internal annulus heat transfer coefficient, when compared to the resulting increased pressure drops. Bahiraei et al. (2021a) proposed novel crimped-spiral ribs in the internal annulus of a TTHE and nanofluids for heat transfer improvement. The flow was characterized by a Reynolds number greater than 2,000. Numerical solutions were obtained through the two-phase mixture method. Turbulent flow was modeled by the Reynolds Stress Model. Different heights and pitches of the ribs were explored. Numerical data were validated against the data by Gomaa et al. (2017). The employment of higher height and pitch led to a significant increase in the heat transfer capability of the system (enhancement in heat transfer coefficient higher than 35.65%), contrarily to what reported in Gomaa et al. (2017). In addition, increment in nanofluid volume fraction of 0.02 resulted in an increment of overall heat transfer coefficient of 44.91%. The heat transfer augmentation achieved through geometrical characteristics of ribs and nanoparticle concentration agreed with that reported by Bahiraei et al. (2019) in turbulent flow condition. The heat transfer rate of a ribbed TTHE operating with nanofluids was therefore predicted with good accuracy by Bahiraei et al. (2021b) through an artificial neural network approach, coupled with the ant lion optimizer, by performing numerical simulations. Tiwari et al. (2021) analyzed, through experiments and CFD, the effects of a turbulent WO3/water nanofluid flow and different inserts on the thermal performance of a TTHE. The investigated geometries were rib inserts, twisted tape inserts and porous plate inserts. The numerical results highlighted increments of 12.38%, 11.83% and 8.61% in overall heat transfer coefficient were achieved using rib, porous plate and twisted tape inserts, respectively, with respect to the nonfinned geometry. The authors additionally underlined the urgent need for size optimization of the HE by using various novel inserts.

In the light of the provided literature, research effort has been focusing on heat transfer augmentation of TTHEs, despite the number of studies and research groups involved is still extremely limited. Moreover, to the authors’ best knowledge, solutions for the food processing field in TTHEs are not yet proposed and analyzed because investigations mainly deal with turbulent flows of water or nanofluids. Such a lack of outcomes on TTHEs and their optimization has also been pointed out by the recent review works by Mukesh Kumar and Hariprasath (2020) and Akgul et al. (2023). Established performance enhancement techniques for TTHEs are thus still far from being achieved, undermining proper design and application. From the applicative point of view, such a limited offer of heat transfer augmentation solutions in the field of food thermal treatment via TTHEs leads to the usual employment of high safety factors, eventually undermining plants efficiency at the expense of poorer product quality and higher environmental impact (higher energy and water consumption) (Kubo et al., 2023).

The aim of the present work is to fill this literature gap by studying a novel geometry for heat transfer enhancement in TTHEs for food processing, capable of ensuring both enhanced heat transfer and good fluid thermalization in laminar flows. The internal annulus of the investigated TTHE is equipped with modules of staggered, interrupted helical fins to induce swirling flow and boundary layer disruption. The novel design for heat transfer augmentation in TTHEs comes from the idea of revisiting classical geometries, extensively studied in the field of double-pipe HEs for higher heat transfer efficiency and fluid mixing. In particular, the beneficial effects of classical helical fins, i.e. lower pressure drops with resulting lower heat transfer coefficients (Mozafarie and Javaherdeh, 2019), are here integrated with those of interrupted fins configurations, i.e. higher heat transfer coefficients with resulting higher pressure drops due to higher flow disturbances (El Maakoul et al., 2020). The present hybrid geometry is thus believed to promote better fluid mixing and overall heat transfer performance during the operation of TTHEs, while mitigating the resulting pressure drops. A numerical approach is used to provide an in-depth and robust insight into the complex thermal fluid dynamic phenomena occurring within the system. The CFD model, implemented within an ANSYS© Fluent environment, is experimentally validated by means of the data collected on an industrial plant for tomato concentrate sterilization. A similar model on the staggered helical fins geometry was previously validated against analytical solution available for the nonfinned annulus for non-Newtonian flows (Pagliarini et al., 2024b). The effect of varying number of finned modules along the length of the HE is investigated at same nominal mass flow rate at the inlet. The results, including heat transfer enhancement, pressure drop augmentation and fluid thermal mixing for different displacements of finned modules, are discussed in relation to the effects induced by the staggered fins through the hydrodynamic and thermal entrance regions of the TTHE. The outcome of the present research provides a useful approach in the design of TTHEs for non-Newtonian fluids processed in the food industry, by fostering optimization strategies able to enhance the overall efficiency of the plant. Hence, the newly proposed augmented geometry may stand as a possible and valuable solution for thermal treatment applications involving highly viscous fluids and, more specifically, food products.

In the present section, the industrial plant is first described in its parts. The mathematical formulation adopted to model tomato processing through the considered sterilizer is therefore presented, and the numerical approach is finally described.

The experimental analysis, performed to validate the numerical approach adopted in the present work, is carried out on a sterilizer of an industrial plant for tomato processing. In particular, the system under investigation is a TTHE in a counterflow arrangement, having the hot service fluid flowing through the external annulus and internal tube, whereas the cold process fluid flows through the internal annulus. A section view of the system is shown in Figure 1. For the present application, the process fluid is tomato concentrate (°Bx = 28), while the service fluid is saturated vapor.

Figure 1.
Cross-sectional schematic of a multilayer annular channel, showing two channels with red-colored service fluid flowing leftward and a central blue-colored channel with process fluid flowing rightward. Arrows indicate the opposing flow directions within the system.The illustration depicts a cross-sectional view with three distinct layers: two outer layers represent service fluid in pink, while the central layer illustrates process fluid in blue. The service fluid layers are oriented vertically, with red arrows indicating flow direction upwards and downwards, while the process fluid flows horizontally from left to right, marked by a blue arrow. The layout features a linear arrangement of the fluid layers, with the HE axis labeled at the bottom, indicating a specific reference point, and internal flow details represented through curved lines within the process fluid layer.

Section view of the system, with reference to the service and process fluids flow direction

Source: Authors’ own work

Figure 1.
Cross-sectional schematic of a multilayer annular channel, showing two channels with red-colored service fluid flowing leftward and a central blue-colored channel with process fluid flowing rightward. Arrows indicate the opposing flow directions within the system.The illustration depicts a cross-sectional view with three distinct layers: two outer layers represent service fluid in pink, while the central layer illustrates process fluid in blue. The service fluid layers are oriented vertically, with red arrows indicating flow direction upwards and downwards, while the process fluid flows horizontally from left to right, marked by a blue arrow. The layout features a linear arrangement of the fluid layers, with the HE axis labeled at the bottom, indicating a specific reference point, and internal flow details represented through curved lines within the process fluid layer.

Section view of the system, with reference to the service and process fluids flow direction

Source: Authors’ own work

Close modal

The novel feature of the analyzed HE is represented by the presence of stationary finned modules in the internal annulus, whose geometrical features are outlined in Figure 2. They are constituted by six twisted fins made of stainless steel, arranged to enhance heat transfer by promoting fluid mixing and boundary layer disruption. The fins in each module are interrupted at the midpoint of the section, and they therefore proceed in a staggered configuration. The ratio between inner and outer diameters is equal to Di/Do = 0.6, while the length of the finned module is l = 2.5Di.

Figure 2.
Schematic of the finned module positioned in the internal annulus of a cylindrical sterilizer, showing labeled dimensions including internal and external diameters and axial length.The image depicts a fluid flow diagram featuring a sinusoidal path between an inner diameter, labeled as "D sub i," and an outer diameter, labeled as "D sub o." The length of the flow path is denoted by "l," indicated by horizontal arrows at both ends. The flow path twists in a wave-like manner, creating two distinct flow channels. The annotations are clear and legible, highlighting how the dimensions relate to the fluid's movement.

Finned module in the internal annulus of the sterilizer

Source: Authors’ own work

Figure 2.
Schematic of the finned module positioned in the internal annulus of a cylindrical sterilizer, showing labeled dimensions including internal and external diameters and axial length.The image depicts a fluid flow diagram featuring a sinusoidal path between an inner diameter, labeled as "D sub i," and an outer diameter, labeled as "D sub o." The length of the flow path is denoted by "l," indicated by horizontal arrows at both ends. The flow path twists in a wave-like manner, creating two distinct flow channels. The annotations are clear and legible, highlighting how the dimensions relate to the fluid's movement.

Finned module in the internal annulus of the sterilizer

Source: Authors’ own work

Close modal

The sterilizer is made of six straight triple-tube passages of length L =24l, connected by curves having curvilinear length equal to Lc = 2 l. The first passage presents four-finned modules, spaced d1 = 6 l apart, while the others present eight-finned modules each, spaced d2 = 2 l apart. A drawing of the HE is shown in Figure 3. The inlet and outlet are represented by a blue and a red arrow, respectively. A section view of the first curve is additionally included in the bottom left of Figure 3.

Figure 3.
Schematic diagram of the sterilizer system, showing the fluid flow path with labeled temperature (T1–T3) and pressure (P1–P2) measurement points. Arrows indicate inlet (blue) and outlet (red) flow directions, with components positioned along a vertical layout.The image is a diagram depicting a network with labels for various points designated as T1, T2, T3, P1, and P2. Lines connecting these points indicate relationships and distances, denoted as d1 and d2. The layout features horizontal lines with loops or knots along them, emphasizing the network's structure. Red and blue arrows indicate specific directions or points of interest at T3 and T1, respectively. The entire arrangement flows from left to right, showing the connections and distances between the labeled nodes clearly.

Schematic layout of the sterilizer under investigation

Source: Authors’ own work

Figure 3.
Schematic diagram of the sterilizer system, showing the fluid flow path with labeled temperature (T1–T3) and pressure (P1–P2) measurement points. Arrows indicate inlet (blue) and outlet (red) flow directions, with components positioned along a vertical layout.The image is a diagram depicting a network with labels for various points designated as T1, T2, T3, P1, and P2. Lines connecting these points indicate relationships and distances, denoted as d1 and d2. The layout features horizontal lines with loops or knots along them, emphasizing the network's structure. Red and blue arrows indicate specific directions or points of interest at T3 and T1, respectively. The entire arrangement flows from left to right, showing the connections and distances between the labeled nodes clearly.

Schematic layout of the sterilizer under investigation

Source: Authors’ own work

Close modal

The process fluid temperature and pressure were monitored by means of 2 pressure transducers (Endress Hauser© Cerabar PMP71, full scale = 200, precision 0.05% of full scale, sampling frequency = 1 Hz) and 12 Pt100 (Endress Hauser iTHERM CableLine TST310, tolerance = 0.3°C, sampling frequency = 0.1 Hz), located at three curves as shown in Figure 3. In Figure 4(a), a picture of the instrumented curves is shown. In particular, four Pt100 sensors were placed, at each curved section, at varying penetration lengths into the fluid stream and different circumferential positions. The Pt100 sensors location is depicted in Figure 4(b); the subscripts S, M and L stand for “Short,” “Medium” and “Long” penetration length, respectively.

Figure 4.
Composite image showing (a) the external view of the sterilizer’s finned module with multiple sensors and electrical connections mounted on metallic piping, and (b) a front view of a flanged pipe section with four labeled Pt100 temperature sensors (S, M1, M2, L) placed symmetrically around the internal perimeter.Several temperature sensors are visible, identifiable by their yellow casings and connected orange wires. These sensors are placed among pipe bends and junctions, indicating they are part of a system designed to monitor temperature within the piping network. The second image focuses on a metallic flange with an open circular centre. Four temperature probes are installed around the inner edge of the flange and are labelled as P t one hundred underscore L, P t one hundred underscore M one, P t one hundred underscore M two, and P t one hundred underscore S. Each probe is enclosed in a red box for emphasis. The flange includes multiple bolt holes evenly spaced around its circumference, suggesting it is intended for secure mounting within a larger industrial system.

Finned module in the internal annulus of the sterilizer

Source: Authors’ own work

Figure 4.
Composite image showing (a) the external view of the sterilizer’s finned module with multiple sensors and electrical connections mounted on metallic piping, and (b) a front view of a flanged pipe section with four labeled Pt100 temperature sensors (S, M1, M2, L) placed symmetrically around the internal perimeter.Several temperature sensors are visible, identifiable by their yellow casings and connected orange wires. These sensors are placed among pipe bends and junctions, indicating they are part of a system designed to monitor temperature within the piping network. The second image focuses on a metallic flange with an open circular centre. Four temperature probes are installed around the inner edge of the flange and are labelled as P t one hundred underscore L, P t one hundred underscore M one, P t one hundred underscore M two, and P t one hundred underscore S. Each probe is enclosed in a red box for emphasis. The flange includes multiple bolt holes evenly spaced around its circumference, suggesting it is intended for secure mounting within a larger industrial system.

Finned module in the internal annulus of the sterilizer

Source: Authors’ own work

Close modal

The sensors continuatively acquired signals during plant functioning. In nominal operation, the mass flow rate m˙ of processed tomato concentrate was equal to 1.3 kg/s.

The tomato concentrate flow through the industrial sterilizer under study was modeled by considering the assumptions of incompressible, steady-state, laminar forced flow, with negligible viscous dissipations, constant thermal properties and negligible axial conduction in the fluid. The continuity, momentum and energy equations governing the non-Newtonian, annular flow under investigation are listed below, respectively, in their general formulation for purely viscous fluids (Schlichting and Gersten, 2017):

(1)
(2)
(3)

where u is the velocity vector, P is the fluid pressure, τ is the stress tensor, T is temperature, ρ is the density and α is the thermal diffusivity. To note, equations (1)–(3) can describe the thermofluid dynamics of either Newtonian or non-Newtonian fluids, depending on the used definition of stress tensor in the momentum equation. Further considerations on how the non-Newtonian stresses are handled in the present work are discussed in the following subsection 2.3. The governing equations are completed, for the present case study, by the following boundary conditions representing uniform axial flow and temperature at the inlet section:

(4)
(5)
(6)

where x and r are the axial and radial coordinates, respectively. Hydrodynamic and thermal entrance was accounted for by imposing, at the inlet, uniform velocity and temperature equal to uinlet = m˙ρπ(Do2Di2)/4 and Tinlet = 348.15 K, respectively. Specifically, the inlet temperature reflected the one resulted by nominal operation of the plant upstream the sterilizer. The wall temperature at the inner and outer surfaces of the internal annulus, i.e. at the separation walls between process and service fluid (Figure 1), was kept constant during the process, Twall = 388.15 K. The curves wall was considered as adiabatic.

Conjugate heat transfer at the fluid–solid (fins-to-fluid) interface was considered, ensuring continuity of temperature and heat flux at the boundaries. The interfacial conditions read as:

(7)
(8)

where the subscripts s and f stand for “solid” and “fluid,” respectively, Γ is the solid–fluid interface, k is the thermal conductivity and n^ is the unity vector normal to the interfaces.

In the numerical analysis, the density, specific heat and thermal conductivity of tomato concentrate were considered equal to ρ = 1,150 kg/m3, cp = 3,600 J/kgK and k = 0.5 W/mK, respectively, according to the previous findings by Choi and Okos (1983). The rheological behavior of tomato concentrate was modeled by a power-law model of the form:

(9)

where η is the apparent viscosity, K is the consistency index, |γ˙| is the magnitude of the rate-of-strain tensor and n is the flow behavior index. The latter was considered as constant and equal to 0.15 (Dak et al., 2008). On the contrary, the consistency index was considered to vary with temperature in accordance with the Arrhenius’ law:

(10)

where A is a constant, Ea is the activation energy, R is the universal gas constant (8.314 J/molK) and T is the absolute temperature. For the present tomato concentrate, A and Ea were considered equal to 1.93 Pa·sn and 13,500 J/mol, respectively, according to the previous literature (Dak et al., 2008). Hence, in equation (2), the non-Newtonian stresses are related with the velocity gradients by the generalized Newtonian model τ=ηaγ˙ (Missirlis et al., 2001).

In the light of the considered properties, the tomato concentrate under investigation can be characterized by means of the generalized Reynolds number by Metzner and Reed (1955) and the generalized Prandtl number (Farajzadeh and Tohidi, 2019), respectively, defined as follows:

(11)
(12)

where W is the average velocity and Dh = DoDi is the hydraulic diameter.

Reg and Prg are shown for the nominal temperature range of the studied sterilizer, such as Tinlet ≤ T ≤ Twall, in Figure 5(a) and (b), respectively.

Figure 5.
Side-by-side plots showing (a) the generalized Reynolds number increasing with temperature, and (b) the generalized Prandtl number decreasing over the same temperature range, both referring to the nominal operating conditions of the sterilizer.The image contains two graphs labeled (a) and (b). The first graph (a) illustrates the relationship between temperature (T) in Kelvin on the horizontal axis and Re,g on the vertical axis, which ranges from zero point three to zero point five five. This graph shows a positive trend. The second graph (b) depicts the relationship between T in Kelvin and Pr,g, which spans from three point five times ten to the power of five to six times ten to the power of five on the vertical axis. This graph shows a negative trend. Both graphs include a linear scale on the axes.

(a) Generalized Reynolds number and (b) Prandtl number in the nominal temperature range of the studied sterilizer

Source: Authors’ own work

Figure 5.
Side-by-side plots showing (a) the generalized Reynolds number increasing with temperature, and (b) the generalized Prandtl number decreasing over the same temperature range, both referring to the nominal operating conditions of the sterilizer.The image contains two graphs labeled (a) and (b). The first graph (a) illustrates the relationship between temperature (T) in Kelvin on the horizontal axis and Re,g on the vertical axis, which ranges from zero point three to zero point five five. This graph shows a positive trend. The second graph (b) depicts the relationship between T in Kelvin and Pr,g, which spans from three point five times ten to the power of five to six times ten to the power of five on the vertical axis. This graph shows a negative trend. Both graphs include a linear scale on the axes.

(a) Generalized Reynolds number and (b) Prandtl number in the nominal temperature range of the studied sterilizer

Source: Authors’ own work

Close modal

The reported data well reflect the extreme working conditions encountered during food processing, and they also suggest an extreme penalization in the heat transfer capabilities. In fact, the high apparent viscosity results in a flow regime regarded as deep laminar, further characterized by a significantly high generalized Prandtl number which hampers thermal penetration into the fluid core. This confirms the extreme need for passive heat transfer enhancement techniques for the present application. It has to be stressed that the low values of generalized Reynolds number reached during the operating conditions under investigation are in line with those considered by the previous literature on thermal treatment of tomato concentrates (Rios-Iribe et al., 2015), where the generalized Reynolds number can often drop below unity.

The finite-volume method was applied to discretize and solve the equations for continuity, momentum and energy of subsection 2.2 within an ANSYS© Fluent 2023 R1 environment. To note, the deep laminar nature of the investigated flow prevented the adoption of any transformation or closure equation in the resolution of the governing equations. The computational framework was specifically designed to capture the laminar flow features and heat transfer phenomena within the complex geometry, accounting for the boundary conditions and the non-Newtonian behavior of tomato concentrate. The solid and fluid domains constituting the internal annulus of the HE were meshed using polyhedral elements through the ANSYS© Fluent Mesher 2023 R1, ensuring an accurate representation of the sharp gradients expected at the walls. Seventeen inflation layers were applied at the walls, including the fin surfaces, with a growth rate of 1.1, allowing smooth cell size transition. The adopted grid is shown in Figure 6. It has to be stressed that a high-quality and high-density computational mesh is here required in the light of the low flow behavior index considered in the present investigation, which may hamper proper convergence of the governing equations solution due to the their high nonlinearity (Khandelwal et al., 2015). The SIMPLE (Semi-Implicit Method for Pressure-Linked Equations) algorithm was used for pressure–velocity coupling, as it offers both stability and efficiency in laminar flow simulations. Discretization of the continuity equation is handled by means of the approach proposed by Rhie and Chow (1983) to prevent unphysical pressure fluctuations. Least squares cell-based gradient evaluation is used. For spatial discretization, a second-order upwind scheme was used for the governing equations to enhance solution accuracy. Default underrelaxation factors are adopted. Before calculations, hybrid initialization algorithm is performed. The absolute convergence criterion for all the residuals was set to 1E-6.

Figure 6.
Mesh visualization of the computational domain: the left image shows a 3D helical structure with fine hexagonal mesh elements along the surface of twisted fins inside a cylindrical geometry; the right image provides a cross-sectional view of the same domain, highlighting the mesh distribution in the annular region.The image displays two geometric structures. On the left, there is a three-dimensional twisted form characterized by a mesh-like pattern composed of hexagonal shapes. The twists and angles create a complex visual texture. On the right, a two-dimensional circular shape is shown, also featuring a mesh with hexagonal patterns. This circular form appears to be a cross-section of the twisted structure, emphasizing the geometric relationship between the two shapes. Both illustrations provide a detailed view of the geometry, highlighting the intricacies of their designs.

Detail of the adopted mesh

Source: Authors’ own work

Figure 6.
Mesh visualization of the computational domain: the left image shows a 3D helical structure with fine hexagonal mesh elements along the surface of twisted fins inside a cylindrical geometry; the right image provides a cross-sectional view of the same domain, highlighting the mesh distribution in the annular region.The image displays two geometric structures. On the left, there is a three-dimensional twisted form characterized by a mesh-like pattern composed of hexagonal shapes. The twists and angles create a complex visual texture. On the right, a two-dimensional circular shape is shown, also featuring a mesh with hexagonal patterns. This circular form appears to be a cross-section of the twisted structure, emphasizing the geometric relationship between the two shapes. Both illustrations provide a detailed view of the geometry, highlighting the intricacies of their designs.

Detail of the adopted mesh

Source: Authors’ own work

Close modal

The simulated configurations are listed in Table 1. All the simulations were run under the same boundary and test conditions defined in subsection 2.2.

Table 1.

Simulated geometrical conditions

SimulationsSimulated geometryAim
1Single-finned module (Figure 2)Grid independence analysis
2Sterilizer (Figure 3)Experimental validation
3First triple-tube annular passage + curve; four-finned modulesEvaluating the thermal enhancement of different configurations with respect to the reference geometry (nonfinned)
4First triple-tube annular passage + curve; eight-finned modules
5First triple-tube annular passage + curve; nonfinned
Source(s): Authors’ own work

The uncertainties related to the collected experimental quantities were assessed to understand the robustness of the present study approach. Specifically, the uncertainty related to the fluid pressure drops resulted from considerations related to the employment of two absolute pressure transducers, as previously highlighted in Figure 3. Hence, the uncertainty δPdifferential to be attributed to the pressure drop between the P1 and P2 locations read as δPdifferential=2·δPabsolute2, where δPabsolute is the uncertainty referred to the single pressure transducer. For the adopted equipment, δPdifferential was computed equal to 0.14 bar.

For what concerns fluid temperature acquisitions, provided that the temperature at the locations T1, T2 and T3 (according to Figure 3) is evaluated as the average between the signals acquired by the four pt100 sensors at each monitored section, the uncertainty of mean section temperatures is considered as the uncertainty of the single temperature measurement, i.e. 0.3°C. Such a conservative uncertainty choice is driven by the fact that the measured temperature at different fluid positions in the generic tube section is highly variable.

Grid independence analysis was performed to ensure the reliability of the numerical results by considering a single-finned module of length l. The geometrical characteristics of the adopted grid were progressively refined, as reported in Table 2, until the chosen quantities, namely, the Nusselt number and the friction factor, stabilized.

Table 2.

Characteristics of the adopted grids for the single-finned module

GridABCDE
Minimum size [m]0.0020.00170.00120.00080.00065
Maximum size [m]0.0060.0050.00370.00220.00135
Inflation layers1015151720
Number of elements4.49E + 058.27E + 051.46E + 062.99E + 066.90E + 06
Source(s): Authors’ own work

All the grids presented an orthogonal quality higher than 0.3. For grid independence analysis, the friction factor f and the Nusselt number Nu were chosen as meaningful quantities to be monitored. Their definitions are reported below:

(13)
(14)

where ΔPxx+Δx is the pressure drop between two consecutive axial coordinates x and x+Δx, h is the convective heat transfer coefficient and k is the fluid thermal conductivity. For the present case of imposed temperature at the inner/outer surfaces of the annulus, h was estimated, for each annulus section of length Δx, by means of the following expression:

(15)

where Q is the thermal power exchanged, Atot is the total heat transfer area, Tb,in and Tb,out are the bulk temperatures at the inlet and outlet, respectively, of the considered annulus section, while ΔTlm is the logarithmic mean temperature difference, defined as:

(16)

In Figure 7(a)–(b), Nu and f are plotted against the number of elements. Because both quantities stabilized for grids having about 3 million elements, the geometrical features of grid C were used for the present study. Such a choice allows a good trade-off between accuracy of the results and needed computational cost.

Figure 7.
Side-by-side plots from the grid independence study: (a) the Nusselt number (Nu) plotted against the number of grid elements; (b) the friction factor (f) plotted versus the number of grid elements. Data points A to E represent different mesh densities.In both graphs, the horizontal axis represents the number of grid elements, ranging from zero to eight million. The first graph, labelled lowercase a in parentheses, presents a decreasing trend in the variable N subscript u. The values begin at approximately forty-eight point two and decline to about forty-six point eight as the number of grid elements increases. Data points labelled A through E are plotted and connected by a dashed line to illustrate the downward trend. The second graph, labelled lowercase b in parentheses, shows an increasing trend in the variable f, starting at approximately forty-three point seven and rising to around forty-four point five. This graph also includes points A through E connected by a dashed line.

Grid independence analysis

Source: Authors’ own work

Figure 7.
Side-by-side plots from the grid independence study: (a) the Nusselt number (Nu) plotted against the number of grid elements; (b) the friction factor (f) plotted versus the number of grid elements. Data points A to E represent different mesh densities.In both graphs, the horizontal axis represents the number of grid elements, ranging from zero to eight million. The first graph, labelled lowercase a in parentheses, presents a decreasing trend in the variable N subscript u. The values begin at approximately forty-eight point two and decline to about forty-six point eight as the number of grid elements increases. Data points labelled A through E are plotted and connected by a dashed line to illustrate the downward trend. The second graph, labelled lowercase b in parentheses, shows an increasing trend in the variable f, starting at approximately forty-three point seven and rising to around forty-four point five. This graph also includes points A through E connected by a dashed line.

Grid independence analysis

Source: Authors’ own work

Close modal

Experimental results are first presented to underline temperature evolution and pressure drops in the real system. Reduced experimental data are therefore adopted to thoroughly validate the numerical method. Finally, numerical results are adopted to better understand the flow features characterizing the proposed solution, as well as its impact on the heat transfer augmentation features, frictional losses and overall thermal mixing.

In the present section, the experimental data collected during in-situ monitoring of the tomato concentrate processing plant is presented. In Figure 8, the temperature signals, acquired at the three locations T1, T2 and T3, according to Figure 3 over the observation window, are shown. To note, the temperature is here expressed in dimensionless form θ = T/Twall. At the first acquisition point [Figure 8(a)], the temperatures referred to the sensors having medium and long penetration lengths are close to the inlet temperature, θinlet = Tinlet/Twall = 0.65, suggesting that the fluid core is still at much lower temperature than the wall. On the contrary, the fluid close to the wall is already significantly warmed up, as confirmed by the sensor having short penetration length (red solid line). At the second acquisition point [Figure 8(b)], all the temperature data exhibit a noticeable increase. The beneficial effects of the finned modules on the overall mixing and thermalization of the process fluid is perceivable by the fact that the sensor having long penetration length (black solid line) approaches here the one having short penetration length, suggesting that the fluid recirculation promoted by fins successfully forces the fluid in contact with the heating walls to flow closer to the core of the annular passage. Thanks to such a recirculation effect, overheating of tomato concentrate is mitigated, whereas colder fluid could be effectively redirected toward the heating walls, allowing better efficiency of the sterilization process. Finally, at the last acquisition point [Figure 8(c)], the fluid temperature at the four sensors locations exhibits good homogenization, being the recorded signals close to each other. Such evidence confirms the capability of the finned modules to enhance fluid mixing and, consequently, its thermalization during the sterilization process. From the experimental temperature signals provided, the temperature stratification characterizing the fluid flow during thermal treatment is evident, especially closer to the HE inlet. Such a critical issue will be numerically dealt with by analyzing the effect of different geometrical configurations on heat transfer augmentation in subsection 5.3.

Figure 8.
Three time series plots labeled (a), (b), and (c), showing normalized temperature readings (θ) from four Pt100 sensors (S, M1, M2, L) over a duration of 2000 seconds. Each subplot corresponds to a different location in the system (T1, T2, T3), with color-coded lines representing sensor positions around the pipe cross-section as previously shown in Figure 3.Each graph shows the relationship between time, measured in seconds on the horizontal axis, and a variable denoted by the Greek letter theta on the vertical axis. The vertical axis ranges from zero to one, and the horizontal axis spans from zero to two thousand seconds, with increments of five hundred seconds. Each graph includes multiple coloured lines representing different data series. A red line indicates P t one hundred subscript S, a magenta line represents P t one hundred subscript M I, a blue line signifies P t one hundred subscript M two, and a black line corresponds to P t one hundred subscript L.

Pt100 sensors signals over time referred to the (a) T1, (b) T2 and (c) T3 locations, according to Figure 3 

Source: Authors’ own work

Figure 8.
Three time series plots labeled (a), (b), and (c), showing normalized temperature readings (θ) from four Pt100 sensors (S, M1, M2, L) over a duration of 2000 seconds. Each subplot corresponds to a different location in the system (T1, T2, T3), with color-coded lines representing sensor positions around the pipe cross-section as previously shown in Figure 3.Each graph shows the relationship between time, measured in seconds on the horizontal axis, and a variable denoted by the Greek letter theta on the vertical axis. The vertical axis ranges from zero to one, and the horizontal axis spans from zero to two thousand seconds, with increments of five hundred seconds. Each graph includes multiple coloured lines representing different data series. A red line indicates P t one hundred subscript S, a magenta line represents P t one hundred subscript M I, a blue line signifies P t one hundred subscript M two, and a black line corresponds to P t one hundred subscript L.

Pt100 sensors signals over time referred to the (a) T1, (b) T2 and (c) T3 locations, according to Figure 3 

Source: Authors’ own work

Close modal

The gauge pressure signals, synchronized with the temperature signals of Figure 8, were also reduced to evaluate the pressure drop along the HE. In Figure 9, the pressure drops per unit length between the first and the second pressure measurement locations, ΔP = P1 – P2, are shown, being LP = 2 L +2Lc, according to Figure 3. The high viscosity of processed tomato concentrate results in high pressure losses, further increased by the presence of the finned modules. Despite the intrinsic noise of the signal, the pressure drops exhibit a slight variation over time, which is probably due to small deviations of the plant from its nominal conditions of mass flow rate at the inlet of the sterilizer during functioning.

Figure 9.
Line plot showing the pressure drop per unit length (ΔP/L) between sensors P1 and P2 over a 2000-second interval.The horizontal axis is labeled t in square brackets s, indicating time in seconds, and ranges from zero to two thousand seconds. The vertical axis is labeled delta P divided by L subscript P in square brackets k P a per m, representing pressure difference per unit length in kilopascals per metre. The graph features a continuous line with varying vertical values, indicating fluctuations in the pressure difference over time.

Pressure drops per unit length between P1 and P2 (reference of Figure 3) over time

Source: Authors’ own work

Figure 9.
Line plot showing the pressure drop per unit length (ΔP/L) between sensors P1 and P2 over a 2000-second interval.The horizontal axis is labeled t in square brackets s, indicating time in seconds, and ranges from zero to two thousand seconds. The vertical axis is labeled delta P divided by L subscript P in square brackets k P a per m, representing pressure difference per unit length in kilopascals per metre. The graph features a continuous line with varying vertical values, indicating fluctuations in the pressure difference over time.

Pressure drops per unit length between P1 and P2 (reference of Figure 3) over time

Source: Authors’ own work

Close modal

By adopting experimental pressure data, the assumption drawn in subsection 2.2 for negligible viscous dissipation was verified. Specifically, such an assumption holds when the Brinkman number is limited (Gratão et al., 2006). When a non-Newtonian flow in developed, constant wall temperature conditions is considered, the Brinkman number assumes the generalized form below (Coelho and Pinho, 2009):

(17)

where the wall shear stress can be defined as a function of the friction factor, τwall=fW2ρ8. By assuming the flow fully developed between the two pressure locations P1 and P2, and by estimating f through the recorded ΔP/LP (Figure 9), Brg results lower than 10−2, hence confirming the negligible viscous dissipations in the fluid flow.

The numerical approach has been validated by means of the data experimentally acquired on the analyzed industrial plant. Specifically, all the experimental samples were averaged over the observation window. The same locations of the sensors experimentally used were considered for the extraction of numerical results. Specifically, temperature and pressure data were exported by performing surface averages at the sections of interest. In Table 3, numerical and experimental temperature and pressure data are listed. Percentage deviations between numerical (datnum) and experimental (datexp) data were additionally computed as PD=datnumdatexpdatexp×100, and reported.

Table 3.

Comparison between numerical and experimental data

Variable Numerical dataExperimental dataPD (%)
ΔP (kPa/m)31.0532.133.4
θ10.780.754.0
θ20.840.840
θ30.890.872.3
Source(s): Authors’ own work

As noticeable, the percentage deviations between numerical and experimental data are limited, suggesting a very good agreement between the adopted pieces of data and, consequently, a high reliability of the used numerical approach. To provide an additional piece of validation of the numerical scheme, the average dimensionless temperature assumed by the simulated flow along the heat exchanger is plotted in Figure 10, together with the experimental data for comparison. Here, it is noticeable that the temperature trend along the dimensionless axial coordinate is coherent with the imposed heating conditions. The model is further confirmed to well approximate the temperature evolution in the real experimental system, discretized at the monitoring sections. The numerical method was thus considered as fully validated because it reflected with good accuracy the values of pressure drops and dimensionless temperatures recorded during the industrial plant operation.

Figure 10.
Scatter plot comparing numerical (black circles) and experimental (red stars) average dimensionless fluid temperatures (θ) along the dimensionless axial coordinate (x*) of the heat exchanger.The scatter plot illustrates two sets of data points: numerical values represented by open circles and experimental values indicated by red stars. The horizontal axis, labelled x star, ranges from zero to six, while the vertical axis, labelled theta, ranges from zero point seven to zero point nine, with increments of point one. Data points are scattered in an upward trend, indicating a relationship between the two variables. Each data point is distinctly marked to differentiate between numerical and experimental data, aiding in visual analysis without any grid lines in the background.

Comparison between numerical and experimental average dimensionless fluid temperatures along the dimensionless axial coordinate of the HE

Source: Authors’ own work

Figure 10.
Scatter plot comparing numerical (black circles) and experimental (red stars) average dimensionless fluid temperatures (θ) along the dimensionless axial coordinate (x*) of the heat exchanger.The scatter plot illustrates two sets of data points: numerical values represented by open circles and experimental values indicated by red stars. The horizontal axis, labelled x star, ranges from zero to six, while the vertical axis, labelled theta, ranges from zero point seven to zero point nine, with increments of point one. Data points are scattered in an upward trend, indicating a relationship between the two variables. Each data point is distinctly marked to differentiate between numerical and experimental data, aiding in visual analysis without any grid lines in the background.

Comparison between numerical and experimental average dimensionless fluid temperatures along the dimensionless axial coordinate of the HE

Source: Authors’ own work

Close modal

After successfully validating the numerical method against experimental data, the main thermofluid dynamics features promoted by the finned modules were numerically investigated. To note, all the simulations were carried out by considering mass flow rate of 1.3 kg/s, such as the same mass flow rate treated by the industrial plant during nominal operation. First, a local analysis of the results allowed a better representation of the flow and thermal characteristics through finned geometries. The effectiveness of the proposed solution was therefore analyzed in terms of heat transfer augmentation and fluid thermalization with respect to the reference geometry, such as the nonfinned annulus under same operating conditions. Geometrical arrangements presenting four- and eight-finned modules, respectively, were investigated during the thermal and hydrodynamic entrance region, i.e. in the first triple-tube passage, and compared to identify the optimal configuration from a thermofluidic standpoint.

5.3.1 Local flow and thermal characteristics.

The finned geometry of the HE was first analyzed in terms of local features of the fluid flow. Streamlines are shown in Figure 11(a) for a representative finned module. As noticeable, the finned geometry induces significant variations of the fluid path: the fluid crosses the first part of the module, undergoing swirling effects which are believed to augment the heat transfer capabilities of the system (Mousavi Ajarostaghi et al., 2022). Moreover, the middle section of the module ensures a drastic change in fluid flow direction, probably allowing better fluid mixing and overall thermalization. In Figure 11(b), velocity contours are shown along the finned module. Here, it can be noted that the velocity contours at the two ends of the module reflect the ones expected for an unperturbed annular flow, being the velocity in the core of the annulus highly uniform.

Figure 11.
Two-part visualization of fluid dynamics in a finned heat exchanger module: (a) streamlines, illustrating the complex flow paths around the twisted fins; (b) a central 3D model of the module surrounded by six cross-sectional slices showing velocity contours (u*) at different axial positions.The flow pattern is composed of intertwined surfaces that indicate directional movement. Below this illustration are three circular distributions, each paired with a colour scale for u asterisk, also ranging from zero to two, showing how the variable varies across each circular region. Section b presents a central three-dimensional twisted geometry positioned above four circular distributions. Each of these circular distributions includes its own colour scale for u asterisk, ranging from zero to two. Arrows extend from the central twisted geometry to each circular distribution, visually indicating the connections or influence between them. The layout emphasises variation in flow characteristics and distribution across different geometric configurations.

(a) Streamlines and (b) dimensionless velocity contours along a representative finned module of the studied HE

Source: Authors’ own work

Figure 11.
Two-part visualization of fluid dynamics in a finned heat exchanger module: (a) streamlines, illustrating the complex flow paths around the twisted fins; (b) a central 3D model of the module surrounded by six cross-sectional slices showing velocity contours (u*) at different axial positions.The flow pattern is composed of intertwined surfaces that indicate directional movement. Below this illustration are three circular distributions, each paired with a colour scale for u asterisk, also ranging from zero to two, showing how the variable varies across each circular region. Section b presents a central three-dimensional twisted geometry positioned above four circular distributions. Each of these circular distributions includes its own colour scale for u asterisk, ranging from zero to two. Arrows extend from the central twisted geometry to each circular distribution, visually indicating the connections or influence between them. The layout emphasises variation in flow characteristics and distribution across different geometric configurations.

(a) Streamlines and (b) dimensionless velocity contours along a representative finned module of the studied HE

Source: Authors’ own work

Close modal

Close to the finned module, the fins effect becomes more and more evident. The fluid is circumferentially accelerated, being forced to follow the fins paths. In the middle of the finned sections, i.e. at the fins’ interruption and consequent path inversion, high nonuniformity of fluid velocity occurs. Such an interruption is in fact expected to greatly enhance heat transfer, according to previous studies on interrupted fins (El Maakoul et al., 2020; Mohsen et al., 2021).

In Figure 12, the dimensionless temperature contours along a representative module are shown. Here, the temperature referred to the fluid in contact with the heating walls is much higher than that in the core of the annulus. This confirms the fact that the high Prandtl characterizing the investigated flow prevents heat diffusion into the fluid core, penalizing its proper thermalization. Nonetheless, the temperature contours through the finned module exhibit the presence of warm spots away from the inner and outer walls, probably due to the joint effect of enhanced inner convection promoted by the fins and heat transfer through the fins. The latter is, however, believed to play a minor role in the overall heat transfer processes due to low thermal conductivity of stainless steel. Finally, downstream the fins, the warm spots in the fluid tend to progressively disappear, probably due to inner conduction in the fluid core.

Figure 12.
Visualization of dimensionless temperature distribution (θ) in a finned heat exchanger module. The central 3D model shows twisted fins, while six surrounding cross-sectional slices display temperature contours at different axial positions. Color gradients range from blue (θ = 0) to red (θ = 1), highlighting thermal boundary layers and heat transfer evolution along the flow path.The image features a central three-dimensional twisted structure with grey shading. Surrounding it are four concentric rings, each displaying color gradients representing specific data values, ranging from zero to one. Each ring has a corresponding color scale legend at the top, using red and blue hues to indicate values from 0 to 1. The structure and the surrounding rings are connected by thin lines. This layout allows for clear comparison among the rings, showcasing variations in data within the context of the central twisted form.

Dimensionless temperature contours along a representative finned module of the studied HE

Source: Authors’ own work

Figure 12.
Visualization of dimensionless temperature distribution (θ) in a finned heat exchanger module. The central 3D model shows twisted fins, while six surrounding cross-sectional slices display temperature contours at different axial positions. Color gradients range from blue (θ = 0) to red (θ = 1), highlighting thermal boundary layers and heat transfer evolution along the flow path.The image features a central three-dimensional twisted structure with grey shading. Surrounding it are four concentric rings, each displaying color gradients representing specific data values, ranging from zero to one. Each ring has a corresponding color scale legend at the top, using red and blue hues to indicate values from 0 to 1. The structure and the surrounding rings are connected by thin lines. This layout allows for clear comparison among the rings, showcasing variations in data within the context of the central twisted form.

Dimensionless temperature contours along a representative finned module of the studied HE

Source: Authors’ own work

Close modal

5.3.2 Heat transfer enhancement.

After achieving a better local description of the thermofluid dynamics characterizing the finned solution, the heat transfer efficiency of the finned HE was quantified by estimating the Nusselt number and the friction factor along the entrance region of the HE, such as from the inlet of the sterilizer up to the end of the first curve. In particular, the study on the hydrodynamic and thermal entrance region of the system is of practical importance to design compact HEs (Batra and Sudarsan, 1992).

In Figure 13, the Nusselt number for the finned (eight and four modules) and nonfinned configurations is shown against the dimensionless axial coordinate, defined as x*=x/L.

Figure 13.
Line plot showing the variation of the Nusselt number (Nu) along the dimensionless axial coordinate (x*) for three configurations: 8 finned modules (red dashed line with stars), 4 finned modules (blue dashed line with stars), and a non-finned annulus (black dashed line with stars).The vertical axis represents N subscript u values, ranging from approximately ten to forty-five. The horizontal axis represents x star values, ranging from zero point two to one, with increments of zero point two. Three distinct curves are shown on the graph: a dashed red line represents eight modules, a dashed blue line represents four modules, and a dashed black line represents a non-finned annulus. Each curve is marked with a corresponding symbol, and a legend within the graph identifies the meaning of each line style and symbol. All three curves show a general decrease in N subscript u as x star increases, with variations in trend across the three configurations.

Nusselt number as a function of the dimensionless axial coordinate

Source: Authors’ own work

Figure 13.
Line plot showing the variation of the Nusselt number (Nu) along the dimensionless axial coordinate (x*) for three configurations: 8 finned modules (red dashed line with stars), 4 finned modules (blue dashed line with stars), and a non-finned annulus (black dashed line with stars).The vertical axis represents N subscript u values, ranging from approximately ten to forty-five. The horizontal axis represents x star values, ranging from zero point two to one, with increments of zero point two. Three distinct curves are shown on the graph: a dashed red line represents eight modules, a dashed blue line represents four modules, and a dashed black line represents a non-finned annulus. Each curve is marked with a corresponding symbol, and a legend within the graph identifies the meaning of each line style and symbol. All three curves show a general decrease in N subscript u as x star increases, with variations in trend across the three configurations.

Nusselt number as a function of the dimensionless axial coordinate

Source: Authors’ own work

Close modal

For x* = 0.25, all configurations show similar Nusselt numbers, suggesting that the first thermal entrance is not significantly affected by fins. At increasing dimensionless axial coordinate, both the finned geometries present higher Nu with respect to the nonfinned configuration, highlighting the efficacy of fins in terms of passive heat transfer enhancement. The provided values of Nu in the enhanced configuration are in line with those typically found for similar applications adopting scraped surface HEs (Solano et al., 2023; Triki et al., 2021), denoting comparable heat transfer augmentation at the cost of obvious higher energy consumption than the proposed finned solution. Nonetheless, the configuration with eight-finned modules exhibits the highest thermal performance as long as the flow develops (Nu almost twice the one of the nonfinned geometry at x* = 1). This is due to the greater flow perturbance achieved by the higher number of finned modules, which establishes a more effective boundary layer disruption. The effect of different numbers of finned modules on the friction factor is further reported in Figure 14.

Figure 14.
Line plot showing the friction factor (f) as a function of the dimensionless axial coordinate (x*) for three configurations: 8 finned modules (red dashed line with stars), 4 finned modules (blue dashed line with stars), and a non-finned annulus (black dashed line with stars).The graph presents three distinct curves indicating variations in function f as a response to the variable x-star, which ranges from zero point two to one on the horizontal axis. The vertical axis measures f, with values ranging from thirty to fifty. The three curves are represented with different styles: a dashed red line for eight modules, a dashed blue line for four modules, and a dashed black line for a non-finned annulus. Each curve is marked with star symbols at various points along the x-star axis. A legend in the upper right corner identifies the corresponding styles for each module configuration.

Friction factor as a function of the dimensionless axial coordinate

Source: Authors’ own work

Figure 14.
Line plot showing the friction factor (f) as a function of the dimensionless axial coordinate (x*) for three configurations: 8 finned modules (red dashed line with stars), 4 finned modules (blue dashed line with stars), and a non-finned annulus (black dashed line with stars).The graph presents three distinct curves indicating variations in function f as a response to the variable x-star, which ranges from zero point two to one on the horizontal axis. The vertical axis measures f, with values ranging from thirty to fifty. The three curves are represented with different styles: a dashed red line for eight modules, a dashed blue line for four modules, and a dashed black line for a non-finned annulus. Each curve is marked with star symbols at various points along the x-star axis. A legend in the upper right corner identifies the corresponding styles for each module configuration.

Friction factor as a function of the dimensionless axial coordinate

Source: Authors’ own work

Close modal

As expected, for the same test conditions, the presence of more finned modules results in higher friction factors, whereas the nonfinned geometry exhibits the lowest friction factor. The computed values of friction factor are in agreement with those expected for non-Newtonian flows under laminar conditions, as reported in Madlener et al. (2009).

In the light of the presented figures of merit, the configuration having eight-finned modules highlights better thermal performances, at the cost of higher friction factor according to the well-established analogy between heat and momentum transfer (Mahulikar and Herwig, 2008). To quantify the effect of pressure drops over heat transfer enhancement of the two configurations, the performance index η was computed for both the finned geometries as (Gomaa et al., 2017):

(18)

where the subscript 0 refers to the reference geometry (nonfinned annulus). η is plotted against the dimensionless axial coordinate in Figure 15. Here, η is less than unity for the first length of the entrance length, i.e. x* < 0.6, confirming that the presence of fins does not play any beneficial role at the beginning of the entrance region. This could be due to the considered high Prandtl number, for which the hydrodynamic boundary layer develops much faster than the thermal boundary layer (Batra and Sudarsan, 1992).

Figure 15.
Line plot showing the performance index (η) as a function of the dimensionless axial coordinate (x*) for two configurations: 8 finned modules (red dashed line with stars) and 4 finned modules (blue dashed line with stars).The horizontal axis represents x star, ranging from zero point two to one, while the vertical axis represents the variable ranging from zero point eight to one point three. The graph displays two data sets using dashed lines: a red dashed line represents data for eight modules, and a blue dashed line represents data for four modules. Each data line includes star-shaped markers indicating specific data points. A legend in the upper left corner identifies the colour and symbol used for each module configuration.

Performance index η estimated for the eight- and four-finned modules

Source: Authors’ own work

Figure 15.
Line plot showing the performance index (η) as a function of the dimensionless axial coordinate (x*) for two configurations: 8 finned modules (red dashed line with stars) and 4 finned modules (blue dashed line with stars).The horizontal axis represents x star, ranging from zero point two to one, while the vertical axis represents the variable ranging from zero point eight to one point three. The graph displays two data sets using dashed lines: a red dashed line represents data for eight modules, and a blue dashed line represents data for four modules. Each data line includes star-shaped markers indicating specific data points. A legend in the upper left corner identifies the colour and symbol used for each module configuration.

Performance index η estimated for the eight- and four-finned modules

Source: Authors’ own work

Close modal

However, for x* > 0.7, η becomes greater than unity, suggesting better thermofluidic performances of the internal annulus presenting fins. Specifically, the use of four-finned modules results in a maximum η of about 1.15, while the annulus presenting eight-finned modules exhibits the highest η in the entrance region (maximum of about 1.23 at x* = 1). Such a configuration is hence confirmed to be superior in terms of heat transfer augmentation, despite the increased pressure losses.

5.3.3 Thermal mixing.

The analysis on overall heat transfer augmentation achieved through the present passive, finned solutions were completed by the evaluation of their thermal mixing efficiency. This is, in fact, a fundamental parameter to ensure proper thermal processing of the food product without degrading its chemical and functional properties (Sawale et al., 2024; Sikorski, 2006). Hence, the effectiveness of the proposed finned modules in terms of thermalization of the process fluid was investigated by estimating a thermal mixing parameter ψ, defined as follows (Kouadri et al., 2021):

(19)

where σi and σi,0 are the temperature standard deviation in the generic cross section i related to the finned configuration, and the temperature standard deviation evaluated at the same section for the reference, nonfinned geometry. To note, when the temperature standard deviation in the finned annulus equals the one in the nonfinned annulus, ψ = 0 (minimum mixing improvement achievable), whereas ψ = 1 when the temperature standard deviation of the finned annulus equals zero (maximum mixing improvement achievable).

In Figure 16, ψ is shown as a function of the dimensionless axial coordinate. Here, the thermal mixing parameter is always greater than zero, and it keeps increasing along the axial coordinate for every configuration, suggesting that the presence of fins can effectively increase the fluid thermalization with respect to the nonfinned configuration. The geometry presenting eight-finned modules always exhibits higher values of ψ, with a maximum of 0.11, suggesting not only greater heat transfer, as per subsection 5.3.2, but also higher thermal mixing of the working fluid, thus proving its superior thermal performance.

Figure 16.
Line plot showing the mixing parameter (ψ) as a function of the dimensionless axial coordinate (x*) for two configurations: 8 finned modules (red dashed line with stars) and 4 finned modules (blue dashed line with stars).The graph illustrates a relationship between two variables, x-star on the horizontal axis and psi on the vertical axis. The x-star axis ranges from zero point two to one point two, with increments not labelled. The psi axis extends from zero to zero point twenty-five, with increments marked at intervals of zero point five. There are two curves: a red dashed line representing eight modules and a blue dashed line representing four modules. The data points for each module type are indicated with star markers, accompanied by a legend at the top left corner defining each line. The lines exhibit distinct trends as they progress, with the red line generally appearing at a higher psi value compared to the blue line across the x-star range.

Mixing parameter as a function of the dimensionless axial coordinate

Source: Authors’ own work

Figure 16.
Line plot showing the mixing parameter (ψ) as a function of the dimensionless axial coordinate (x*) for two configurations: 8 finned modules (red dashed line with stars) and 4 finned modules (blue dashed line with stars).The graph illustrates a relationship between two variables, x-star on the horizontal axis and psi on the vertical axis. The x-star axis ranges from zero point two to one point two, with increments not labelled. The psi axis extends from zero to zero point twenty-five, with increments marked at intervals of zero point five. There are two curves: a red dashed line representing eight modules and a blue dashed line representing four modules. The data points for each module type are indicated with star markers, accompanied by a legend at the top left corner defining each line. The lines exhibit distinct trends as they progress, with the red line generally appearing at a higher psi value compared to the blue line across the x-star range.

Mixing parameter as a function of the dimensionless axial coordinate

Source: Authors’ own work

Close modal

It is worth noticing that, for x* > 1, i.e. in the curve, ψ undergoes a sharp increase, hence suggesting that, despite the curved connections are considered as adiabatic, their effect on the fluid thermal mixing is extremely beneficial. To provide a better insight into such increased thermal mixing, a dimensionless temperature contour of the curve section is shown in Figure 17. When the heating section interrupts, the fluid expands in the curve, and the threads close to the hot, inner wall proceed along the core of the curved section. This results in the formation of a hot fluid trail, continuously warmed up by the ending tip of the inner tube of the HE. Hence, despite the inner convection does not substantially increase due to low accelerations induced by curvature, the fluid experiences higher thermal mixing due to section variation and continuous warming up of the fluid core.

Figure 17.
Cross-sectional contour plot showing the dimensionless temperature (θ) distribution in a curved geometry. Color gradient ranges from blue (θ = 0) to red (θ = 1), highlighting higher temperatures near internal obstacles and lower temperatures toward the outer wall.The image presents a circular gradient visualisation where two central shapes are surrounded by concentric rings of colour. The gradient transitions smoothly from shades resembling red, yellow, green, and blue, indicating values that range from zero on the outer edge to one at the center. On the right side of the image is a colour scale, illustrating value increments from zero to one. The scale features distinct colour transitions, adding clarity to the corresponding values in the gradient.

Temperature contour referred to the curve section

Source: Authors’ own work

Figure 17.
Cross-sectional contour plot showing the dimensionless temperature (θ) distribution in a curved geometry. Color gradient ranges from blue (θ = 0) to red (θ = 1), highlighting higher temperatures near internal obstacles and lower temperatures toward the outer wall.The image presents a circular gradient visualisation where two central shapes are surrounded by concentric rings of colour. The gradient transitions smoothly from shades resembling red, yellow, green, and blue, indicating values that range from zero on the outer edge to one at the center. On the right side of the image is a colour scale, illustrating value increments from zero to one. The scale features distinct colour transitions, adding clarity to the corresponding values in the gradient.

Temperature contour referred to the curve section

Source: Authors’ own work

Close modal

A TTHE for tomato concentrate sterilization was experimentally and numerically tested via CFD to assess heat transfer enhancement achievable by interrupted, staggered fins in the internal annulus. The industrial plant was instrumented with pressure and temperature transducers at varying locations to monitor the main characteristics of the tomato concentrate thermal processing. The governing equations and corresponding boundary conditions were implemented in an ANSYS© Fluent environment. The rheological behavior of tomato concentrate was modeled by means of a power-law model, with consistency coefficient dependent on temperature. After a grid independence analysis on a single-finned module, the geometrical features of the optimal grid were used to simulate the entire sterilizer. The numerical data were compared with experimental ones to achieve a proper validation of the numerical approach. The maximum deviation between experimental and numerical data was equal to 4%. The features of the considered flow through a representative finned module were locally investigated by means of dimensionless velocity and temperature contours. Different geometrical configurations, i.e. finned system with eight-finned modules, finned system with four-finned modules and nonfinned annulus, were therefore simulated in the entrance region to assess the heat transfer augmentation promoted by fins. The Nusselt number Nu and the friction factor f were assessed as functions of the dimensionless axial coordinate. The geometry having superior thermal performances and, at the same time, introducing limited pressure losses was selected by means of the performance index η. The thermal mixing achieved by fins was finally evaluated through a thermal mixing parameter ψ.

The following main outcomes can be drawn:

  • The presence of fins induces a swirling flow, capable of enhancing heat transfer. Moreover, the staggered configuration promotes better fluid mixing due to higher perturbation of the fluid stream.

  • In the entrance region, the annulus having eight-finned modules present the highest Nu (almost twice the one of the nonfinned geometry), despite the highest friction factor.

  • The performance index η for the eight-finned modules reaches a maximum of about 1.23, while the use of four-finned modules guarantees a η of about 1.15. The use of closer finned modules is thus confirmed to be beneficial in terms of overall heat transfer performances of the HE under the operating conditions investigated.

  • The fluid thermal mixing resulting from the finned configurations is always greater than zero, suggesting that fins not only promote heat transfer but also fluid thermalization. Up to the curved section, the ψ reaches a maximum of about 0.11 for the geometry presenting eight-finned modules. However, in the curve, ψ undergoes a much steeper increase, reaching a maximum of about 0.22. Such behavior could account for the change in the tube cross section, coupled with trailing thermal effects resulting from the upstream heating section.

To conclude, the adopted finned geometries presented superior performances than the nonfinned annulus due to their boundary layer disruption and thermal mixing effects. Having more frequent finned modules along the HE, i.e. shorter distance between modules, promoted heat transfer enhancement, whereas guaranteeing limited pressure losses. The present study can be used to design more efficient HEs for food processing, especially when good thermal mixing and consequent uniform treatment are required. In fact, this represents a critical aspect in the food industry, where strict temperature targets are needed to achieve a satisfactory degree of microbial and enzyme inactivation and organoleptic characteristics preservation, hence underlining the extreme relevancy of the proposed heat transfer enhancement method for such industrial applications.

In future works, the finned module will be optimized by varying its geometrical features, such as the twist rate. Also, the reported flow and thermal patterns taking place in the curve could be considered to develop novel passive methodologies for maximizing fluid mixing and thermalization at such locations.

The Authors would like to acknowledge financial support from PNRR-M4C2- I1.1 – MUR Call for proposals n.104 of 02-02-2022 - PRIN 2022 - ERC sector PE8- Project title: MOOD4HEX - MOr-phology Optimized Design for HEs - Project Code 2022SJP2A5 - CUP Code D53D23004040006 - Funded by the European Union – NextGenerationEU and and from the CFT Group, Parma, Italy (CFT Leaders InnovateLink to a PDF of the cited article.).

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