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Numerical Heat Transfer, Part A: Applications
An International Journal of Computation and Methodology
Volume 74, 2018 - Issue 4
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Articles

Performance study of finned tube evaporative air cooler based on experiment and numerical simulation

, , , &
Pages 1154-1174 | Received 28 Feb 2018, Accepted 14 Jun 2018, Published online: 17 Oct 2018
 

Abstract

The influence of air speed, spray density and tube bundle on wet air cooling of the fins are analyzed through numerical solution. The spray water droplets are released from the surface injection source in the discrete phase model (DPM). And the water film is formed in three-dimensional fins using Eulerian wall film model (EWF). The species transport model is coupled with EWF model to solve the phase transition and heat exchange. The heat exchange and pressure loss of tube bundle are evaluated through field synergy principle and Fanning friction factor, and a comprehensive performance factor is obtained. Based on the fins with outer diameter of 57 mm, 50 mm and 42 mm, the comprehensive factor and mass transfer coefficient of 57 mm fins are higher than that of other two fins under varied air flow rate and spray density. Besides, The increase in tube rows number weakens the mass exchange of unit area. When the Re exceeds 2,820, the comprehensive performance of finned tube bundle with more rows become worse.

Nomenclature
=

surface area (m−2)

=

phase change constant

=

drag coefficient

=

specific heat (kJ·kg−1·K−1)

=

diameter (m)

=

mass diffusivity coefficient (m·s−2)

=

force (N)

=

gravitational acceleration (m·s−2)

=

narrowest air unit flow (kg·m−2·s−1)

=

heat exchange coefficient (W·m−2·K−1 )

=

mass exchange coefficient (kg·m−2·s−1)

=

latent heat (kJ·kg−1)

=

enthalpy (kJ·kg−1)

=

thermal conducivity (W·m−1·K−1)

=

Lewis factor

=

mass flow rate (kg·s−1)

=

molar weight (kg·kmol−1)

=

Nusselt number

=

pressure (Pa)

=

Prandtl number

=

stress tensor (Pa)

=

momentum (kg·m·s−1)

=

energy source from air (J)

=

heat flow at boundary layer (W·m−2·s−1)

=

heat exchange (W)

=

temperature (K)

=

velocity (m·s−1)

=

water mass fraction in air (kgw·kga−1)

=

droplet distortion coefficient

=

the ratio of narrowest flow surface to the upwind surface

=

thickness (m)

=

viscosity (kg·m−1·s−1)

=

distance from cell to wall (m)

=

density (kg·m−3)

=

surface tension (kg·m−1)

a=

air

con=

condensation

D=

drag

f=

fluid

fgwo=

evaporation at 0 °C

i=

inlet

l=

liquid film

ma=

unit quality air

masw=

saturated air at water film temperature

Mix=

mixture

o=

outlet

p=

particle

s=

source

sat=

saturation

v=

vapor

vap=

evaporation

w=

water

=

tangential

Nomenclature
=

surface area (m−2)

=

phase change constant

=

drag coefficient

=

specific heat (kJ·kg−1·K−1)

=

diameter (m)

=

mass diffusivity coefficient (m·s−2)

=

force (N)

=

gravitational acceleration (m·s−2)

=

narrowest air unit flow (kg·m−2·s−1)

=

heat exchange coefficient (W·m−2·K−1 )

=

mass exchange coefficient (kg·m−2·s−1)

=

latent heat (kJ·kg−1)

=

enthalpy (kJ·kg−1)

=

thermal conducivity (W·m−1·K−1)

=

Lewis factor

=

mass flow rate (kg·s−1)

=

molar weight (kg·kmol−1)

=

Nusselt number

=

pressure (Pa)

=

Prandtl number

=

stress tensor (Pa)

=

momentum (kg·m·s−1)

=

energy source from air (J)

=

heat flow at boundary layer (W·m−2·s−1)

=

heat exchange (W)

=

temperature (K)

=

velocity (m·s−1)

=

water mass fraction in air (kgw·kga−1)

=

droplet distortion coefficient

=

the ratio of narrowest flow surface to the upwind surface

=

thickness (m)

=

viscosity (kg·m−1·s−1)

=

distance from cell to wall (m)

=

density (kg·m−3)

=

surface tension (kg·m−1)

a=

air

con=

condensation

D=

drag

f=

fluid

fgwo=

evaporation at 0 °C

i=

inlet

l=

liquid film

ma=

unit quality air

masw=

saturated air at water film temperature

Mix=

mixture

o=

outlet

p=

particle

s=

source

sat=

saturation

v=

vapor

vap=

evaporation

w=

water

=

tangential

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