Abstract
This work simulates the heat and mass transfer of the fuel droplets evaporated in a hot medium. The proposed model includes the vaporization of multi-component fuel droplet, in laminar forced convection. The results show that the various components, of different molecular weights, vaporize at different temperatures. Furthermore, the non-miscibility of the mixture of the hydrocarbons liquid droplet is observed. The profile of the regression of the droplet square diameter does not follow the \(d^{2}\) law and presents three evaporation rates rather than a single one. New correlations for the evaporation rate versus Reynolds and Schmidt numbers are proposed for different air velocities, different initial droplet radii, and different initial mass fractions.
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Abbreviations
- B :
-
Spalding number
- \(C_{p}\) :
-
Specific heat (\(\hbox {J}\,\hbox {kg}^{-1}\,\hbox {K}^{-1}\))
- D :
-
Diffusion coefficient (\(\hbox {m}^{2}\,\hbox {s}^{-1}\))
- d :
-
Droplet diameter (m)
- K :
-
Evaporation rate (\(\hbox {mm}^{2}\,\hbox {s}^{-1}\))
- \({<}{K}{>}\) :
-
Average evaporation rate (\(\hbox {mm}^{2}\,\hbox {s}^{-1}\))
- L :
-
Latent heat (\(\hbox {J\,kg}^{-1}\))
- M :
-
Molar mass (\(\hbox {kg\,kmol}^{-1}\))
- Nu :
-
Nusselt number
- P :
-
Pressure (atm)
- Pr :
-
Prandtl number
- r :
-
Droplet radius (m)
- Re :
-
Reynolds number
- Sc :
-
Schmidt number
- Sh :
-
Sherwood number
- t :
-
Time (s)
- T :
-
Temperature (K)
- u :
-
Air velocity (\(\hbox {m\,s}^{-1}\))
- Y :
-
Mass fraction
- \(\eta \) :
-
\(r/r_{s}\)
- \(\lambda \) :
-
Thermal conductivity (\(\hbox {W\,m}^{-1}\,\hbox {K}^{-1}\))
- \(\rho \) :
-
Density (\(\hbox {kg\,m}^{-3}\))
- a :
-
Air
- crit :
-
Critical
- f :
-
Fuel
- ebn :
-
Boiling
- fT :
-
Heat transfer limit
- fM :
-
Mass transfer limit
- g :
-
Gas
- i :
-
Component
- L :
-
Liquid
- l :
-
Liquid
- M :
-
Mass
- s :
-
Surface
- T :
-
Thermal
- VS :
-
Saturated vapor
- v :
-
Vapor
- \(\infty \) :
-
Ambient medium
- 0:
-
Initial
- *:
-
Defined
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Dgheim, J., Abdallah, M. & Nasr, N. Enhanced Evaporation of Droplet of Ternary Component Under the Effect of Thermo-physical and Transport Properties Variability. Arab J Sci Eng 43, 2181–2194 (2018). https://doi.org/10.1007/s13369-017-2561-8
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DOI: https://doi.org/10.1007/s13369-017-2561-8