Comparison with a producer design software

The model performance with 2 different airside correlations (Wang et al. [12] for wavy fins and Wang et al. [10] for plain fins) was compared with Type1223new and the producer design software Guntner Product Calculator (GPC) of the company Guntner GmbH. Two staggered tube lay outs available in GPC (HX 1 and HX 2, heat exchanger length of 1.25 m and height 1 m, 10 passes) with wavy fins (corrugation angle = 15°) were considered. For both geometries the heat transfer rate, calculated by the model with the correlation for wavy fins, is about 10% for HX 1 and less than 5% for HX 2 lower than that of the GPC, (Fig. 4). It has to be noted, that transverse tube pitch Pt in HX 1 is out of the validity range of the correlation for wavy fins, extrapolation of the correlation is in general not recommended. The heat transfer rate, calculated by the model for plain fins, is lower than the GPC heat transfer rate too (Fig. 4), which is plausible. However, HX 1 is also out of the validity range of the plain fin correlation, the deviation of this correlation to the GPC for HX 1 is even smaller than that of the wavy fin correlation, probably because of the less complex structure. Unlike these correlations, Type1223new with the Elmahdy and Biggs [5] correlation for plain fins gives higher heat transfer rate values than the GPC. It is, however, unfeasible that plain fins have higher heat transfer coefficient than wavy fins (compare with [20]).

Подпись: Fig. 4 Heat transfer rate calculated by the model (as plain and wavy fins), Type1223new and GPC for different air flow rates and two geometries (left for HX 1, right for HX 2).

The airside pressure drop, determined with the correlations for plain and wavy fins, is significantly lower than that, calculated by the GPC, Fig. 5. Whereas liquid-side pressure drop calculation slightly overestimate the pressure drop calculated by the GPC and is in agreement with the GPC when calculated as smooth tubes.

image274,image275
image276

Fig. 5 Airside pressure drop calculated by the model (as plain and wavy fins) and GPC for different air flow
rates and two geometries (left for HX 1, right for HX 2).

2. Conclusion

A model for fin-and-tube heat exchangers, which is based on empirical heat transfer and flow friction correlations, is presented here. The selected correlations are developed with larger data base and have complete description of the reduction method than the one used in Type1223new. In general one needs to be careful with empirical correlations, especially with complex ones, and one needs to prove simulation results. It is not recommended to extrapolate the correlations for configuration outside of the validity range. If configuration outside of the validity shall be simulated (e. g. for optimization of heat exchanger configuration) it appears to be sensible to use less complex correlations, e. g. Wang et al. [10] instead of Wang et al. [12].

Acknowledgements

The authors would like to express their gratitude to the Volkswagen Foundation, Germany for the financial support.

Nomenclature

Af

m2

minimum flow area

Q

W

heat transfer rate

Aface

m2

frontal area

Re

Reynolds number

Ai

m2

tube inside surface area

T

°C

temperature

Ao

m2

total airside surface area

U

W/m2K

heat transfer coefficient

C

W/K

heat capacity rate

Sf

m

fin thickness

Dc

m

collar diameter

є

heat exchanger effectiveness

Di

m

tube inner diameter

n

fin efficiency

Do

m

tube outer diameter

0

0

fin corrugation angle

f

friction factor

P

kg/m3

density

G

kg/m2s

air mass flux based on

z

ratio of minimum flow area

minimum flow area

to face area

j

=Nu/(RePr1/3)

Subscripts

Colburn factor

k

W/mK

thermal conductivity

1

airside inlet

N

number of tube rows

2

airside outlet

Pi

m

longitudinal tube pitch

i

tube inner side

Pt

m

transverse tube pitch

m

mean

Pr

Prandtl number

min

minimum value

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