Mass Transfer-3 Mass Convection Mass convection (or convective mass transfer), which is the transfer of mass between a surface and a moving fluid, is due to both mass diffusion and bulk fluid motion. The analogy between heat and mass convection holds for both forced and natural convection, laminar and turbulent flow, and internal and external flow. Similar to heat transfer, the concentration boundary Figure (1) The development of a concentration layer, as shown in figure (1), is defined as the region boundary layer for species A during external flow on where concentration gradient exists. In external flow, a flat surface. the thickness of the concentration boundary layer δc for spies A at a specified location on the surface is defined as the normal distance y from the surface at which: ππ΄,π − ππ΄ = 0.99 ππ΄,π − ππ΄,∞ In internal flow, there is a concentration entrance region, where concentration profile develops, until the concentration boundary thickness reaches the tube center [figure (2)]. The distance from the tube inlet to the location where the thickness reaches the center of the tube is called concentration entry length Lc, and the region beyond that point is called fully developed region, which is characterized by: Figure (2) The development of the velocity, thermal, and concentration boundary layers in internal flow. π ππ΄,π − ππ΄ ( )=0 ππ₯ ππ΄,π − ππ΄,π Where ππ΄,π is the bulk mean density of species A defined as: ππ΄,π = 1 ∫ ππ΄ π± ππ΄π π΄π π±ππ£π π΄ Therefore, the non dimensionalized concentration difference profile as well as the mass transfer coefficient remains constant in the fully developed region. π The corresponding number to ππ = πΌ in convective heat transfer, is Schmidt number in convective mass transfer, it is defined as: ππ = π£ ππππππ‘π’π πππππ’π ππ£ππ‘π¦ = π·π΄π΅ πππ π πππππ’π ππ£ππ‘π¦ Moreover, the dimensionless number Lewis number (Le) is defined as: 1 πΏπ = ππ πΌ πβπππππ πππππ’π ππ£ππ‘π¦ = = ππ π·π΄π΅ πππ π πππππ’π ππ£ππ‘π¦ At the surface (y=0), the mass transfer is by diffusion only because of no-slip boundary condition, and mass flux of species A at the surface can be expressed by Fick’s law as [figure (3)]: ππ΄ = πΜπ΄ ππ€π΄ = −π π·π΄π΅ | π΄ ππ¦ π¦=0 This is analogous to heat transfer at the surface being by conduction only and expressing it by Fourier’s law. The rate of heat convection for external flow was expressed conveniently by Newton’s law of cooling, whereas the rate of mass convection can be expressed as: Figure (3) Mass transfer at a surface occurs by diffusion because of the no-slip boundary condition, just like heat transfer occurring by conduction. πΜππππ£ = βπππ π π΄ (ππ΄,π − ππ΄,∞ ) = βπππ π π π΄ (π€π΄,π − π€π΄,∞ ) Where hmass is the average mass transfer coefficient, in m/s; A is the surface area; ππ΄,π − ππ΄,∞ is the mass concentration difference of species A across concentration boundary layer; and ρ is the average density of the fluid in the boundary layer. If the local mass transfer coefficient varies in the flow direction, the average mass transfer coefficient can be determined from: βπππ π ,ππ£π = 1 β¬ βπππ π ππ΄ π΄ π΄ The dimensionless Sherwood number (Sh) in mass transfer, is the corresponding number to Nusselt number (Nu) in heat transfer. Sherwood number is defined as: πβ = βπππ π πΏ π·π΄π΅ Where hmass is the mass transfer coefficient and DAB is the mass diffusivity. L is the characteristic length, depends on the flow geometry. Sometimes it is more convenient to express the heat and mass transfer coefficients in terms of dimensionless Stanton number as: Heat transfer Stanton number: β ππ’ ππ‘ = π ππππ£ = π π ππ π±πΆ π And 2 Mass transfer Stanton number: ππ‘πππ π = βπππ π π± πβ = π π ππ Where π± is the free stream velocity in external flow and bulk mean fluid velocity in internal flow. For a given geometry, the average Nusselt number in forced convection depends on the Reynolds and prandtl numbers, whereas the average Sherwood number depends on Reynolds and Schmidt numbers. That is: Nusselt number: ππ’ = π(π π, ππ) Sherwood number: πβ = π(π π, ππ) Where the functional form of f is the same for both Nusselt and Sherwood numbers in a given geometry, provided that the thermal and concentration boundary conditions are of the same type. Therefore, the Sherwood number can be obtained from the Nusselt number expression by simply replacing the prandtl number by Schmidt number. This shows that a powerful tool analogy can be in the study of natural phenomena [Table (1)]. In natural convection mass transfer, the analogy between the Nusselt and Sherwood numbers still holds, and thus Sh = f (Gr, Sc). Where the Grashof number in this case should be determined directly from: βπ 3 π (π∞ − ππ )πΏπ 3 π ( π ) πΏπ πΊπ = = ππ£ 2 π£2 Which is applicable to both temperature and/or concentration-driven natural convection flow. For homogenous fluids (i.e. fluids with no concentration gradients), density differences are due βπ to temperature differences only, and thus we can replace ( π ) by (β ΔT) for convenience, as we did in natural convection heat transfer. However, in non homogenous fluids, density differences βπ are due to the combined effect of temperature and concentration differences and π cannot be replaced by β ΔT in such cases. Analogy between Friction, Heat Transfer and Mass Transfer Coefficients Several attempts have been made for making analogy between heat and mass transfer, but the simplest and best known is the one of Chilton and Colburn as: 2 2 π = ππ‘ ππ 3 = ππ‘πππ π ππ 3 2 For 0.6 < Pr < 60 and 0.6 < Sc < 3000. This relation is known as the Chilton – Colburn analogy. From the forgoing equation; 3 2 ππ‘ ππ 3 =( ) ππ‘πππ π ππ Or 2 2 ββπππ‘ ππ 3 πΌ 3 = π πΆπ ( ) = π πΆπ ( ) = π πΆπ πΏπ 2/3 βπππ π ππ π·π΄π΅ This analogy is applied in case of laminar and turbulent flow. Mass Convection Relations To determine mass convection coefficients, it can be determined by either (1) using ChiltonColburn analogy or (2) using appropriate Nusselt number relations, replacing Nusselt number by Sherwood number, and Prandtl number by Schmidt number, as shown in Table (2). Simultaneous Heat and Mass Transfer As shown in Figure (4) and Table (3), and in general any mass transfer problem involving phase change (evaporation, sublimation, melting…etc) must also involve heat transfer and the solution of such problems needs to be analyzed by considering simultaneous heat and mass transfer. Accordingly: QΜ sensible,transferred = QΜlatent,absorbed Or πΜ = πΜπ£ βππ Figure (4) Various mechanisms of heat transfer involved during the evaporation of water from the surface of a lake. 4 Table (1) Analogy between the quantities that appear in the formulation and solution of heat convection and mass convection. Table (2) Sherwood number relations in mass convection for specified concentration at the surface corresponding to the Nusselt number relations in heat convection for specified surface temperature. Table (3) Various expressions for evaporation rate of a liquid into a gas through an interface area As under various approximations (subscript v stands for vapor, s for liquid-gas interface, and ∞ away from surface) 5