A three-dimensional numerical model is developed to investigate the effect of turbulence on mass transfer from a single droplet exposed to a freestream of air. The freestream temperature, turbulence intensity and Reynolds number are varied to provide a wide range of test conditions, whereas the ambient pressure is kept atmospheric. The turbulence terms in the conservation equations of the gas-phase are modelled by using the shear-stress transport (SST) model. A Cartesian grid based blocked-off technique is used in conjunction with the finite-volume method to solve numerically the governing equations of the gas and liquid-phases. This study showed that the vaporization Damkohler number proposed in the literature to correlate the effect of turbulence on the droplet's vaporization rate is invalid at air temperatures higher than room temperature. Additionally, an attempt is made to correlate the effect of the freestream turbulence on the droplet's mass transfer rate by using Sherwood number over a wide range of freestream temperatures. (c) 2006 Elsevier Masson SAS. All rights reserved.
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Tecnol Nacl Mexico, IT Pachuca, Div Estudios Posgrad & Invest, Pachuca, Hgo, MexicoTecnol Nacl Mexico, IT Pachuca, Div Estudios Posgrad & Invest, Pachuca, Hgo, Mexico
Serrano-Arellano, J.
Lopez, F. N. Demesa
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Tecnol Nacl Mexico, IT Pachuca, Div Estudios Posgrad & Invest, Pachuca, Hgo, MexicoTecnol Nacl Mexico, IT Pachuca, Div Estudios Posgrad & Invest, Pachuca, Hgo, Mexico
Lopez, F. N. Demesa
Aguilar-Castro, K. M.
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Univ Juarez Autonoma Tabasco, Div Academ Ingn & Arquitectura, Cunduacan, MexicoTecnol Nacl Mexico, IT Pachuca, Div Estudios Posgrad & Invest, Pachuca, Hgo, Mexico
Aguilar-Castro, K. M.
Belman-Flores, J. M.
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Univ Guanajuato, Dept Ingn Mecan, Div Ingn, Grp Invest IRSE, Salamanca, MexicoTecnol Nacl Mexico, IT Pachuca, Div Estudios Posgrad & Invest, Pachuca, Hgo, Mexico
机构:
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang UniversityNational Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University
Tao Zhi
Cheng Zeyuan
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National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang UniversityNational Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University
Cheng Zeyuan
Zhu Jianqin
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National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang UniversityNational Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University
Zhu Jianqin
Li Haiwang
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National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang UniversityNational Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University