Development and validation of an improved heat transfer calculation model for rough tubes
Desarrollo y validación de un modelo mejorado de cálculo de transferencia de calor para tubos rugosos
Yanan Camaraza-Medina1*, Michael Mortensen2, Yamilka Blanco-Garcia3
1University of Guanajuato, México.
2University of California, Santa Bárbara, USA.
3University of Moa, Holguín, Cuba.
*Corresponding author email: ycamaraza1980@gmail.com
Abstract:
An improved method for heat transfer calculation inside rough tubes
is provided. The model has been obtained from a second assessment
developed early by the authors on fluid flow in single-phase inside
rough tubes. The proposed correlation has been verified by comparison
with a total of 1 666 experimental available data of 34 different
fluids, including air, gases, water and organic liquids. The proposal
model covers a validity range for Prandtl number ranging from 0.65 to
4.52x104values of Reynolds number from 2.4x103
to 8.32x106, a range of relative roughness ranging from
5x10-2 to 2x10-6 and viscosity ratio from 0.0048
to 181.5. The proposed model provides a good correlation for
104≤Re and Re<104, with an average error of
18.3% for 70.4% of the data and 16.6% for 74.8% of the data,
respectively. The method presents a satisfactory agreement with the
experimental data in each interval evaluated; therefore, the model can
be considerate accurate enough for practical application. At the present
time, in the available technical literature, a method with similar
characteristics is unknown.
Keywords: friction factor; equivalent roughness heat transfer coefficient; average deviation; rough tubes; model.
Resumen:
Se presenta un método perfeccionado para el cálculo de la transferencia de calor en el interior de tubos rugosos. El modelo se ha obtenido a partir de una segunda evaluación desarrollada anteriormente por los autores sobre el flujo de fluidos en una sola fase en el interior de tubos rugosos. La correlación propuesta se ha verificado mediante comparación con un total de 1 666 datos experimentales disponibles de 34 fluidos diferentes, entre los que se incluyen aire, gases, agua y líquidos orgánicos. El modelo propuesto cubre un rango de validez para el número de Prandtl que va de 0,65 a 4,52 x 104, valores del número de Reynolds de 2,4 x103 a 8,32 x106, un rango de rugosidad relativa de 5 x10-2 a 2 x10-6 y una relación de viscosidad de 0,0048 a 181,5. El modelo propuesto proporciona una buena correlación para 104≤Re y Re<104, con un error medio del 18,3% para el 70,4% de los datos y del 16,6% para el 74,8% de los datos, respectivamente. El método presenta una concordancia satisfactoria con los datos experimentales en cada intervalo evaluado; por tanto, el modelo puede considerarse suficientemente preciso para su aplicación práctica. Actualmente, en la literatura técnica disponible se desconoce un método con características similares.
Palabras clave: factor de fricción; coeficiente de transferencia de calor de rugosidad equivalente; desviación media; tubos rugosos; modelo.
In many industrial processes, to obtain the average heat transfer coefficients is a frequent requirement of energy facilities. For this purpose, due to its simplicity and reasonable approximation, the Dittus-Boelter model is preferred. When the temperature difference is large enough to cause significant changes of viscosity, then the Sieder-Tate model is recommended (Binu and Jayanti 2018; Ataei-Dadavi et al. 2019).
The accuracy on the heat transfer prediction can be improved with the
use of two models derived from the Prandtl analogy: the equations of
Petukhov (1970) and Gnielinski (2013) for and
, respectively (Reis et al. 2018).
Recently, a new model that shows a satisfactory fit was proposed; with
validity range
(Camaraza-Medina, Cruz-Fonticiella and
García-Morales 2019).
In heat transfer equipment, tubes generally have a low surface
roughness, therefore, in calculations they are considered as smooth
. However, the continued use increases gradually
the aging and surface roughness of the tubes, which exerts a notable
effect on the fluid circulation, and therefore, on the average heat
transfer coefficient. The dimensionless roughness is a widely used term
that establishes the roughness pattern, and is given by Equation (1)
(Chen et al. 2019):
In Equation (1), is the relative roughness;
is the Reynolds number and
is the Darcy friction factor.
Nomenclature |
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|
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|
|
|
|
|
|
Constant defined in Equation (5) |
|
Prandtl number |
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Dimensional roughness (Equation (1)) |
|
Reynolds number |
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Constant defined in Equation (3) |
|
Modified Reynolds number |
||
Percentage of data that correlates under MAE values |
|
Average fluid temperature, °C |
||
Deviation percent, defined in Equation (7) |
|
TP |
Wall temperature, °C |
|
Modified Prandtl number, defined in Equation (5) |
|
|
|
|
Maximum error |
|
Greek symbols |
||
Mean absolute error, % |
|
|
|
|
Relative roughness |
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Heat transfer coefficient, kg∙m-1∙K-1∙s-1 |
||
Darcy friction factor |
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Experimental heat transfer coefficient, kg∙m-1∙K-1∙s-1 |
||
Constant defined in Equation (5) |
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Fluid dynamic viscosity at TF, kg∙m-1∙s-1 |
||
Nusselt number |
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Fluid dynamic viscosity at TP, kg∙m-1∙s-1 |
||
When, the surface roughness has a negligible influence
on the average heat transfer coefficient. However, for
, the surface roughness has a significant
influence, therefore, in the heat transfer calculations it must be
considered (Bazán, Bedin and Bozzoli 2016;
Rabiee et al. 2018).
In the technical literature, several works that describe comparisons
between available models are found; however, these do not consider the
effect of the friction factor on the average heat transfer coefficient.
Models derived from the Prandtl analogy and logarithmic adjustments as
Petukhov (1970), Gnielisnky (2013) and Camaraza et al. (2020)
respectively, include this effect, but only for (Camaraza-Medina, Hernandez-Guerrero
and Luviano-Ortiz 2020).
During the 1990’s, some works focused on improving the correlation
indexes in the available correlations offering an approximate techniques
for models derived from the Prandtl analogy (for this purpose, the
friction factor may be determined with the help of the Moody chart)
however, these models do not provide satisfactory results, because in
tests carried out, mean absolute error (MAE) of ±30% and
maximum errors near 80% have been found (Camaraza-Medina et
al. 2019a). For heat transfer calculations during fluid flow in
single-phase inside rough tubes, in the literature several correlations
are found; however, only a reduced range of relative roughness is
considered in these correlations (Song, Cui and Liu 2017).
An important research focused on transition and turbulent flow was
made by Bhatti-Shah (Bhatti and Shah 1987). In this work, the influence
of a turbulence dimensionless parameter (turbulent Prandtl number) is
considered, allowing to extend the validity range of the model and
improving the accuracy of the heat transfer calculations. Similarly, a
corrective term to consider the influence of dimensionless roughness on
the mean coefficient was included. This correlation has a mean deviation
of 20% with respect to the available experimental values and is suitable
for .
Recently, one model for improving the heat transfer calculations in rough tubes was developed. This correlation has a mean deviation of 18% with respect to the available experimental values and increases the validity range and the friction factor is estimated by means of a procedure for non-isothermal conditions (Medina, Fonticiella y Morales 2017, Camaraza-Medina et al. 2019b).
Currently, in the available literature there exists no study that provides MAE and Emax variations for the existing models, neither, the number of data that complies with a acceptable MAE values. For this purpose, in the present work, a total of 1 666 experimental data of 34 different fluids were compiled, including air, gases, water and organic liquids. Available experimental data were correlated with three known models in the literature, Bhatti-Shah, Gnielinski and the modified Gnielinski method (using Moody chart for the friction factor). A summary of the equations used and their validity range is given by Song, Cui and Liu (2017).
To develop a correlation for heat transfer calculation inside rough pipes, with a larger validity range with respect to known models, while providing lower indexes of MAE and Emax is the main objective of the present paper. Additionally, a description and tabulation of the main results using the correlation of the selected models and also the correlation proposed in the present work with available experimental data is offered as well.
The Prandtl model is taken in this research as a starting point, which is provided by Camaraza-Medina et al. (2020):
Equation (2) is suitable for turbulent
flow, however, for
transition flow
the modified Reynolds is
required. In this paper, the modified Reynolds is provided by:
In Equation (3), the exponent D has a logarithmic dependence, obtained by adjusting the experimental data (Figure 1). A regression analysis shows that the exponent D is given by:
In Equation (4) is the Darcy
friction factor, which is obtained according to recommendations provided
in Mondal and Field (2018).
Figura 1. Experimental data correlation with the Equation (4).
The experimental data used in the validation of the selected model were extracted from Medina et al. (2018) and summarized in Table 1, which presents a comparison of the proposed correlation with a wide range of experimental data.
Table 1. Comparison of equation (5) and available experimental data
Source |
Number of data |
Fluid |
e/d |
Pr |
Deviation percent |
||
Milman (1973) |
34 |
Air |
0.001 0.005 |
14 4810 |
0.68 0.7 |
0.64 1.66 |
14.6 -12.3 |
Rosson (1955) |
29 |
Turpentine |
0.001 0.005 |
13 109 |
14.3 29.8 |
0.41 2.43 |
10.7 -14.9 |
Borishanskiy et al. (1973) |
27 |
Water |
0.04 0.006 |
98 262 |
1.2 6.0 |
0.24 0.86 |
13.4 -9.1 |
28 |
Pentane |
0.005 0.0001 |
135 619 |
4.5 7.2 |
0.47 2.08 |
16.1 -19,6 |
|
Houng et al. (2019) |
23 |
Transformeroil |
0.025 0.001 |
3.1 10.3 |
32.1 1490 |
0.012 114.1 |
20.1 -16,7 |
49 |
Water |
0.04 0.000 |
7.2 620 |
1.9 10.6 |
0.19 5.1 |
14.3 -11.8 |
|
31 |
Ethyl iodide |
0.03 0.001 |
12.3 31.4 |
3.6 5.3 |
0.53 1.87 |
9.2 -10.4 |
|
|
33 |
Transformer oil |
0.01 0.008 |
3.9 10.1 |
45 1510 |
0.02 110.4 |
15.3 -17.1 |
Boyko (1965) |
42 |
Water |
0.008 0.0005 |
13.8 540 |
2 12 |
0.18 3.15 |
18.6 -13.9 |
Andreijin et al. (1965) |
26 |
Benzene |
0.001 0.0005 |
2.5 20.2 |
3.1 5 |
0.3 3.18 |
18.9 -7.6 |
Camaraza et al (2018) |
38 |
Water |
0.02 0.004 |
280 2200 |
0.93 11 |
0.19 3.96 |
15.3 -17.9 |
Efimok (1967) |
42 |
Nitrogen |
0.01 0.005 |
6 8100 |
0.68 0.75 |
0.15 6.5 |
19.8 -11.9 |
I’lin (1950) |
38 |
Air |
0.05 0.01 |
7 5100 |
0.68 0.7 |
0.65 1.65 |
16.3 -10.5 |
Kirilov (1969) |
49 |
Carbondioxide |
0.01 0.005 |
14 660 |
0.66 0.81 |
0.3 3.3 |
7.2 -10.7 |
Vukalovich (1963) |
21 |
Air |
0.01 0.005 |
12.5 3700 |
0.68 0.7 |
0.65 1.65 |
17.2 -10.5 |
Sabersky (1962) |
32 |
Water |
0.05 0.01 |
25 180 |
1 9.44 |
0.13 7.15 |
14.1 -5.9 |
Osipova (1964) |
44 |
Helium |
0.02 0.005 |
9 40 |
0.71 0.72 |
0.22 4.5 |
17.1 -12.3 |
47 |
Isobutene |
0.01 0.005 |
1200 5200 |
0,73 0,75 |
0.68 1.46 |
19.7 -16.4 |
|
28 |
Water |
0.0001 0.0005 |
18 550 |
0.9 9.4 |
0.19 0.77 |
16.2 -10.9 |
|
Amoroz et al. (2019) |
46 |
Methylformate |
0.04 0.001 |
12.6 245.1 |
3.7 7.0 |
0.38 2.63 |
7.1 -4.2 |
56 |
Water |
0.05 0.0001 |
980 8250 |
1 11.1 |
0.1 10.1 |
9.3 -12.4 |
|
47 |
Water |
0.015 0.0005 |
970 8320 |
1.2 10.4 |
0.13 7.48 |
10.4 -13.1 |
|
Aljamalet al. (2018) |
109 |
Water |
0.05 0.000002 |
450 7850 |
2.3 9.2 |
0.3 3.6 |
14.3 -16.1 |
43 |
Gasoline |
0.05 0.0001 |
70 6900 |
5.8 11.0 |
0.38 2.62 |
9.4 -11.4 |
|
Akers et al. (1970) |
21 |
Transformer oil |
0.008 0.0001 |
3.2 10.8 |
33.9 1540 |
0.01 115.2 |
19.3 -14.3 |
29 |
Glycerin |
0.04 0.01 |
2.4 9.0 |
1620 22150 |
0.018 55,4 |
19.2 -15.4 |
|
14 |
MC oil |
0.03 0.001 |
5 10.4 |
120 9800 |
0,07 133,3 |
14.8 -17.1 |
|
19 |
MK oil |
0.008 0.0001 |
5.2 8.6 |
580 38200 |
0.011 88.7 |
14.8 -11.6 |
|
Dipprey (1967) |
12 |
Butyl alcohol |
0.03 |
40 75 |
23 30 |
0.08 0.45 |
14.3 -12.2 |
Dorsch (1969) |
23 |
Gasoline |
0.05 0.015 |
70 6900 |
5.5 15.1 |
0.22 4.4 |
10.4 -6,1 |
23 |
Hydrogen |
0.004 0.0001 |
12 8200 |
0.65 0.73 |
0.48 3.28 |
12.4 -10.8 |
|
Camaraza et al. (2019) |
41 |
Water |
0.004 0.0001 |
4 200 |
2.2 9.4 |
0.27 3.68 |
10.9 -11.5 |
Karkalala (2012) |
54 |
Water |
0.002 0.005 |
1200 2800 |
1.2 5.9 |
0.24 0.96 |
5.3 -4.5 |
Mudawar et al. (2017) |
30 |
Engine Oil |
0.03 0.0001 |
2.4 10.1 |
318.8 45200 |
0.0056 181.5 |
19.1 -21.4 |
Carpenter (1957) |
19 |
Methanol |
0.001 0.00005 |
2.9 1112.1 |
2.2 7.7 |
0.1 9.9 |
9.4 -12.1 |
Vasserman (1962) |
22 |
Kerosene |
0.03 0.005 |
6.4 52.8 |
1.35 2.9 |
0.38 2.6 |
10.1 -2.3 |
19 |
Acetic acid |
0.03 0.005 |
3.0 988 |
8.5 14.2 |
0.8 1.2 |
4.7 -13.7 |
|
28 |
Acetaldehyde |
0.03 0.005 |
3.9 52.4 |
2.85 4.4 |
0.4 2.1 |
8.2 -7.9 |
|
31 |
Butanol |
0.03 0.005 |
5.4 102.6 |
22.5 3860 |
0.04 24.6 |
11.6 -16.7 |
|
17 |
Aniline |
0.03 0.005 |
4.4 1020 |
11.5 111 |
0.08 12.35 |
9.7 -13.5 |
|
15 |
Carbon disulfide |
0.03 0.005 |
13.7 76.6 |
2.3 3.2 |
0.59 1.68 |
11.2 -10.1 |
|
13 |
Ciclohexane |
0.03 0.005 |
36.2 89.3 |
11 19.9 |
0.5 1.9 |
12.3 -16.7 |
|
Jung et al. (2015) |
23 |
Transformer oil |
0.01 0.0015 |
2.8 8.6 |
34.9 4800 |
1.2 28.3 |
16.2 -17.5 |
Mortensen (2019) |
23 |
Ethanol |
0.04 0.01 |
21.4 1514 |
6.9 68.4 |
0.049 20.5 |
7.2 -8.4 |
28 |
Ethyl ether |
0.007 0.0001 |
520 2480 |
3.5 7.3 |
0.3 3.6 |
6.2 -10.1 |
|
27 |
Ethylamine |
0.008 0.0001 |
12.1 17.8 |
5.1 8.3 |
0.55 1.8 |
3.2 -6.1 |
|
31 |
Propylene |
0.04 0.01 |
125 284 |
2.8 3.2 |
0.27 3.66 |
9.1 -4.8 |
|
28 |
Dodecane |
0.04 0.025 |
72 96 |
10.7 28.2 |
0.4 3.3 |
11.1 -12.4 |
|
17 |
Decane |
0.05 0.015 |
16 47.2 |
6.8 17.1 |
0.25 4.1 |
6.3 -7.8 |
|
19 |
Ethyleneglycol |
0.01 0.02 |
6.3 12.1 |
69 510 |
0.12 8.1 |
17.1 -19.3 |
|
41 |
Methanol |
0.015 0.0001 |
8.7 234.5 |
5.9 15.1 |
0.32 3.1 |
8.2 -4.3 |
|
37 |
Ethanol |
0.05 0.001 |
9.2 106.8 |
13 52.5 |
0.17 5.73 |
13.4 -16.2 |
|
For all sources above |
1666 |
|
0.05 0.000002 |
2.4 8320 |
0.65 45200 |
0.0048 181.5 |
20.1 -21.4 |
The proposed correlation was obtained by means of a modeling process, applying superposition variables techniques on Equation (2) (Cancan et al. 2017; Shankar and Senadheera 2024). Adjustment and validation of the available experimental data allowed obtaining the new correlation, given by:
The constant used in Equation (5) takes values 0.25 and 0.11 for
fluid cooling or heating, respectively;
is the modified Prandtl number (Table 2);
is a constant value defined by Equation (6):
Table 2. Values of modified Prandtl number
Zone |
Validity range |
Value of constant |
1 |
||
2 |
||
3 |
Equation (5) is applicable in tubes if .When
, heat transfer coefficient can be obtained by
means of the smooth tubes criteria (Petukhov or Gnielinski). The
dimensional roughness
is described by Equation (1) (Huang et
al. 2016).
Figures 2 to 4 show the correlation between the experimental data and the models summarized in Table 2. Table 3 provides a detailed summary of the validity range, showing a satisfactory fit with Equation (5).
Figura 2. Functional adjustment of values E in Zone 1.
Figura 3. Functional adjustment of values E in Zone 2.
Figura 4. Functional adjustment of values E in Zone 3.
Tables 4 and 5 show the comparison between Equation (5) and the experimental data, for transitional and turbulent regime respectively, dividing into eight subintervals the validity range.
Table 3. Summary of validity range for equation (5)
Parameter |
Range |
Fluids |
Acetaldehyde, Acetic acid, Air, Aniline, Benzene, Butanol, Butyl alcohol, Carbon dioxide, Carbon disulfide, Ciclohexane, Decane, Dodecane, Engine oil, Ethanol, Ethyl ether, Ethyl iodide, Ethylamine, Ethylene glycol, Gasoline, Glycerin, Helium, Hydrogen, Isobutene, Kerosene, MC oil, Methanol, Methyl formate, MK oil, Nitrogen, Pentane, Propylene, Transformer oil, Turpentine and Water. |
0.65 to |
|
|
|
Table 4. Comparison between Equation (5) and experimental data for transitional regime
84.5% data |
||
83.2% data |
||
81.8% data |
||
79.7% data |
||
78.6% data |
||
76.5% data |
||
75.7% data |
||
74.8% data |
||
Table 5. Comparison between Equation (5) and experimental data for turbulent regime
80.2% data |
||
79.3% data |
||
77.9% data |
||
76.2% data |
||
75.1% data |
||
73.4% data |
||
71.8% data |
||
70.4% data |
||
In the examined correlations, the model proposed in this work has the larger validity range, therefore, to execute a comparative study, its validity range is divided in eight sub-intervals, summarized in Tables 4 and 5. The deviation percent (error) is computed with respect to the proposed correlation and is provided by Bae, Kim and Chung (2018):
In Equation (7) is the deviation percent,
and
are the heat transfer coefficients obtained with
Equation (5) and experimentally, respectively.
The mean absolute error (MAE) is calculated as Thomas et al. (2024):
In Equation (8) is the number
of experimental data available. In order to accomplish this correlation
study, the experimental available data were separated in two groups
(Table 6), for turbulent and transition zones.
The study was carried out with 1 666 experimental data. In Table 6,
the values of experimental data available for each
validity range of the model are summarized, in agreement with the
classification given in Tables 4 and 5.
The experimental data available are grouped in the eight intervals
given in Tables 4 and 5 and thus the data of each zone with the four
models selected for this study are correlated, obtaining for each model
the percentage values of data that correlates under MAE
valuesthe maximum error
and the MAE values.
Table 6. Summary of the values used by intervals
Interval |
||
1 |
207 |
482 |
2 |
266 |
615 |
3 |
307 |
708 |
4 |
354 |
784 |
5 |
377 |
843 |
6 |
391 |
938 |
7 |
412 |
1043 |
8 |
437 |
1229 |
In Figures 5 to 7, the values of MAE and
obtained in the correlation developed between
selected models and available experimental data are given in graphical
form.
The study shows that in the transition zone, the fundamentals results
used in the comparison concentrate on three fundamental elements,
described early (,
and MAE). In these, for
it is confirmed that the model proposed in the
present work has the best MAE adjustment values, showing an
average error of 11.1 % and 16.6 %, for 84.5 % and 74.8 % of the
available data for Intervals 1 and 8, respectively.
In the specialized literature (Shankar and Senadheera 2024) it is established that Bhatti-Shah's model correlates with an average error of 15 %; however, the results obtained in the present study show an average error of 13.5 % and 18.4 % for 81.6 % and 70.3 % of the data for Intervals 1 and 8, respectively, proving that the values obtained in the present study are slightly higher to the values commonly attributed in the literature.
The most unfavorable indicators are obtained using the models of Gnielinski, which provide MAE values of 23.2 % and 32.8 % for 72.5 % and 60.1 %, respectively of the experimental data, for Intervals 1 and 8, which agrees well with those results given by Shankar and Senadheera (2024).
The modified correlation of Gnielinski provides fairly acceptable adjustments of correlation, with MAE values of 18.9 and 25.9 % for 74.8 % and 62.9 % of the experimental data, respectively for Intervals 1 and 8; this indicates that Gnielinski’s model can be used for a rapid estimation of the heat transfer coefficients in the transition zone, which confirms the recommendations given by Thomas et al. (2024).
Equation (5) and Bhatti-Shah’s model, show the best index, with 84.5 % and 81.6 %, respectively, in
Interval 1, while these values decrease to 74.8 % and 70.3 % for
Interval 8. On the contrary, the modified correlation of Gnielinski and
the Gnielinski’s model, have the most unfavorable indexes, with 74.8 %
and 72.5 % respectively in Interval 1, decreasing to 62.9 % and 60.1 %
for Interval 8.
Figura 5. MAE values in the correlation data (transition zone).
Figura 6. values in the correlation data (transition
zone).
Figura 7. values in the correlation data (transition
zone).
The known technical literature does not contain recommendations that
suggest the maximum error with the use of a determined model. In the
present research, values of generated with the use of every model for the eight
studied intervals was obtained. For this purpose, a comparison between
available experimental data and the selected models was made.
Equation (5) and Bhatti-Shah’s model show the best index, with 16.9 % and 19.1 % respectively in
Interval 1, while these values increase to 32.3 % and 36.5 % for
Interval 8. On the contrary, the more unfavorable indexes are obtained
with the modified correlation of Gnielinski and Gnielinski’s model,
which provide
values of 27.3 % and 31.4 % respectively for
Interval 1, increasing to 54.7 % and 64.8 % in Interval 8.
Based on the results of this study, it is confirmed that the modified correlation of Gnielinski can be used reservedly to determine the heat transfer coefficients in the transition regime, being preferable not to extend their use beyond Interval 1.
In Figures 8 to 10, the values of MAE and
obtained in the correlation developed between the
selected models and the available experimental data are given in
graphical form.
The study shows that in the turbulent zone, the main results used in
the comparison concentrate on three fundamental elements, described
early (,
and MAE). In these, for
, it is confirmed that Equation (5) have the best
MAE adjustment values, showing an average error of 11.8 % and
18.3 % for 80.2 % and 70.4 % of the available data for Intervals 1 and
8, respectively.
In the specialized literature it is established that Bhatti-Shah's model correlates with an average error of 10 % and 15 % for Intervals 1 and 8 respectively; however, the results obtained in the present study show an average error of 13.8 % and 18.6 % for 77.9 % and 68.1 % of the data for Intervals 1 and 8, respectively, proving that the values obtained in the present study are slightly higher to the values commonly attributed in the literature.
The most unfavorable indicators are obtained using the model of Gnielinski, which provide MAE values respectively of 23.9 % and 36.6 % for 67.1 % and 56.8 % of the experimental data, respectively for Intervals 1 and 8, which agrees well with those results given by Thomas et al. (2024).
Equation (5) and Bhatti-Shah’s model show the best index, with 80.2 % and 77.9 % respectively in
Interval 1, while these values decrease to 70.4 % and 68.1 % for
Interval 8. On the contrary, the modified correlation of Gnielinski and
the Gnielinski’s model, have the most unfavorable indexes, with 70.2 %
and 67.1 % respectively in Interval 1, decreasing to 60.4 % and 56.8 %
for Interval 8.
Equation (5) and Bhatti-Shah’s model show the best index, with 17.3 % and 20.1 % respectively in
Interval 1, while these values increase to 34.1 % and 39.7 % for
Interval 8. On the contrary, the most unfavorable indicators are
obtained with the modified correlation of Gnielinski and Gnielinski’s
model, which provide
values of 28.7 % and 34.6 % respectively for
Interval 1, increasing to 56.8 % and 68.9 % in Interval 8.
The modified correlation of Gnielinski provides fairly acceptable adjustments of correlation, with MAE values of 19.2 % and 28.4 % for 70.2 % and 60.4 % of the experimental data, respectively for Intervals 1 and 8; this indicates that it can be used for a rapid estimation of the heat transfer coefficients in the turbulent zone, which confirms the recommendations given by Medina et al. (2017):
Figura 8. MAE values in the correlation data (turbulent zone).
Figura 9. values in the correlation data (turbulent
zone).
Figura 10. values in the correlation data (turbulent
zone).
Figure 11 shows (with a 20 % error band) the adjustment obtained in the correlation of available experimental data with the model proposed in the present work, and provided by Equation (5).
Figura 11. Correlation of Equation (5) with available experimental data.
· A new improved method for heat transfer calculation inside rough pipes has been proposed in the present work. The new correlation increases the validity range with respect to known models in the literature. The model presents a satisfactory agreement with the experimental data in each interval evaluated; therefore, can be considerate enough for use in practical applications. In available technical literature on the subject a model with similar characteristics is unknown.
·
For the transition zone, 437 experimental data were used,
verifying that the best adjustment was obtained by Equation (5), with a
MAE value of 11.1 % for 84.5 % of the data and of 16.9 % in the Interval 1, while for Interval 8,
a MAE value equal to 16.6 % for 74.8 % of the data and
of 32.3 % are obtained. The more unfavorable
indexes adjustment was achieved with Gnielinski’s model with a
MAE value of 23.2 % for 72.5 % of the data and
of 27.3 % in Interval
1, while for Interval 8, a MAE value equal to 32.8 % for 60.1 %
of the data and
of 54.7 % are obtained. The modified correlation
of Gnielinski can be used reservedly for heat transfer calculations in
the transition regime, being preferable not to extend their use beyond
Interval 1. The values obtained in the present study are slightly higher
to the values commonly attributed to Bhatti-Shah’s model.
·
For the turbulent zone, 1 229 experimental data were used,
verifying that the best adjustment was obtained by Equation (5), with a
MAE value of 11.8 % for 80.2 % of the data and of 17.3 % in Interval 1, while for Interval 8, a
MAE value of 18.3 % for 70.4 % of the data and
of 34.1 % are obtained. The more unfavorable
indexes adjustment was achieved with the Gnielinski’s model with a
MAE value of 23.9 % for 67.1 % of the data and
of 34.6 % in Interval 1, while for Interval 8, a
MAE value of 36.6 % for 56.8 % of the data and
of 68.9 % are obtained, (however, it can be used
for rapid estimations of the heat transfer coefficients in the turbulent
zone). The values obtained in the present study are slightly higher to
the values commonly attributed in the literature to the Bhatti-Shah’s
model.
· In this study, the models recognized in the literature as more precise (Bhatti-Shah and Gnielinski modified), showed a slightly larger uncertainty than the results obtained with the model proposed in the present work. Thus, Equation (5) is a better correlation, with a much better adjustment with the experimental data. Its use leads to a lower value of uncertainty in the calculation of the heat transfer coefficients in the turbulent and transitional regimes.
The authors are very grateful for the help provided by Professor S. Thomson, from the Department of Mathematics, Massachusetts Institute of Technology, USA.
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Información adicional
Conflicto de intereses
Los autores declaran que no existen conflictos de intereses
Contribución de autores
YCM: búsqueda bibliografía sobre la temática, concepción general y ejecución de la investigación, así como la escritura y revisión del informe final. MM: ejecución de trabajos de investigación y procesamiento y presentación de resultados. YBG: análisis de los resultados, escritura y revisión del informe final.
ORCID
YCM, https://orcid.org/0000-0003-2287-7519
MM, https://orcid.org/0000-0002-3293-7573
YBG, https://orcid.org/0000-0001-5420-662
Received: 10/01/2024
Accepted: 04/02/2024