Research regarding thermal and hydrodynamic performance levels of surfaces with sinuous fins for automotive heat exchangers.
Nagi, Mihai ; Carabas, Ioan Daniel ; Ilies, Paul 等
1. INTRODUCTION
Compact aluminium heat exchangers were studied during the
experimental research, with sinuous fins of different thickness, 0,14;
0,16; 0,3; 0,5 mm. The influence of "entry effect" on thermal
and hydrodynamic performance for heat exchangers was identified.
2. THEORETICAL CONSIDERATION
If a small distance x (under 25% of the fin pitch) at fluid entry
is considered, this portion can be considered a flat wall surface and
fluid speed [w.sub.w] to be parallel to thee wall. A laminar flow layer
is observed (fig. 1), also called a hydraulic limit layer. This layer
has a very low thickness [section]x at fluid entry and increases as the
distance x is increased. This is known in literature as the "entry
effect"( Arjanikov & Maltev, 1954).
[FIGURE 1 OMITTED]
The thickness of the two layers can be considered to show a
parabolic variation, but different for the two,
[[delta].sub.x]--hydraulic limit layer thickness,
[[delta].sub.t]--thermal limit layer thickness.
These two dimensions can be correlated with the following equation,
as given by Plhausen (Ilies P et at., 2009):
[[partial derivative].sub.t] = [partial derivative]x/[cube root Pr]
(1)
Heat exchange between the fluid and the wall is most effective at
the entry end of the wall, where the thickness of the limit layer is
very small. A maximum value for the heat transfer coefficient "[[alpha].sub.x]" is noticed where the layer thickness is
close to zero. This is called as the "entry effect", and can
be induced on any surface, for a small given length (Bejan, 1973).
3. EXPERIMENTAL SETUP
A special installation was used for testing heat exchangers, a rig
that can simulate working conditions as close to reality as possible.
Multiple parameters were recorded at a very high level of precision. For
studying thermal and hydrodynamic performance testing, aluminium
water-air type heat exchangers were used, (Nagi et al., 1994) with
plates and bars (fig.2.) (Leca, 1983).
[FIGURE 2 OMITTED]
These heat exchangers had identical frontal areas, with rectangular
section water canals also with identical dimensions. Air passage ways
feature sinuous fins with a constant height of 8,8 mm, a pitch p of 3,5;
4; 5; 6,5 mm and matrix width G of 30; 45; 65; 95 and 115 mm (fig.3)
(Nagi, 1996).
[FIGURE 3 OMITTED]
4. PROCESSING EXPERIMENTAL DATA
Each device was tested in at least 30 functioning work regimes.
Data processing was done using the LabView 7.0 software, that
monitors testing parameters with an error of <2%, can plot graphs of
these parameters and controls the valve that regulates cold air flow.
Recorded data was stored in Excel files.
5. RESULTS
Diagrams in figures 3, 4 and 5 were plotted based on the results
obtained during experimental trials. Colborn j criteria for Reynolds
(Re) number were plotted in figure 3 and 4 for heat exchangers with p
=3.5 and 4 mm pitch, while figure 5 shows plotted results of the
friction coefficient cf for a Reynolds number ranging from 600 to 3600,
for sinuous fins compared to Kays and London type fins(Kays &London,
1984) (Nagi et al., 2006).
[FIGURE 3 OMITTED]
[FIGURE 4 OMITTED]
[FIGURE 5 OMITTED]
6. CONCLUSIONS
Heat exchange coefficient "[[alpha].sub.x]" shows a
maximum value when the thickness of limit layer is close to zero.
By plotting the variation of the Colborn j criteria as a function
of Re number, the obtained results were generalized. The obtained
results can be analyzed from the point of view of their quality as well
as quantity and the diagrams can be used with a high precision to design
similar sinuous fins without any regard to the condition of the
experimental trials. Colborn values are higher for short passage ways.
The differences in Colborn values for the same family of heat exchangers
and the same Re number are explained by the "entry effect". In
this manner, the theory regarding this effect was proven by experimental
trials.
Figure 5 shows that friction coefficient values for sinuous fins on
the air side are dependent only on the hydraulic diameter of the passage
ways. Hydrodynamic performance is better for sinuous fins (for the same
hydraulic diameter) compared to those tried by Kays and London (the Kays
and London fins are named sinuous but in fact they are discontinuous fins). This was to be expected, as thermal performance levels for
sinuous fins are slightly lower regarding those tested by Kays and
London (Nagi et al., 2008).
7. ACKNOWLEDGEMENTS
This work was partially supported by the strategic grant POSDRU
6/1.5/S/13, (2008) of the Ministry of Labour, Family and Social
Protection, Romania, co-financed by the European Social Fund--Investing
in People.
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