Mass Transfer-3 Mass Convection Figure (2) The development of

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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:
𝜌𝐴,𝑠 − 𝜌𝐴
= 0.99
𝜌𝐴,𝑠 − 𝜌𝐴,∞
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œ• 𝜌𝐴,𝑠 − 𝜌𝐴
(
)=0
πœ•π‘₯ 𝜌𝐴,𝑠 − 𝜌𝐴,𝑏
Where 𝜌𝐴,𝑏 is the bulk mean density of species A defined as:
𝜌𝐴,𝑏 =
1
∫ 𝜌𝐴 𝒱 𝑑𝐴𝑐
𝐴𝑐 π’±π‘Žπ‘£π‘’
𝐴
Therefore, the non dimensionalized concentration difference profile as well as the mass transfer
coefficient remains constant in the fully developed region.
𝜈
The corresponding number to π‘ƒπ‘Ÿ = 𝛼 in convective heat transfer, is Schmidt number in
convective mass transfer, it is defined as:
𝑆𝑐 =
𝑣
π‘€π‘œπ‘šπ‘’π‘›π‘‘π‘’π‘š 𝑑𝑖𝑓𝑓𝑒𝑠𝑖𝑣𝑖𝑑𝑦
=
𝐷𝐴𝐡
π‘€π‘Žπ‘ π‘  𝑑𝑖𝑓𝑓𝑒𝑠𝑖𝑣𝑖𝑑𝑦
Moreover, the dimensionless number Lewis number (Le) is defined as:
1
𝐿𝑒 =
𝑆𝑐
𝛼
π‘‡β„Žπ‘’π‘Ÿπ‘šπ‘Žπ‘™ 𝑑𝑖𝑓𝑓𝑒𝑠𝑖𝑣𝑖𝑑𝑦
=
=
π‘ƒπ‘Ÿ 𝐷𝐴𝐡
π‘€π‘Žπ‘ π‘  𝑑𝑖𝑓𝑓𝑒𝑠𝑖𝑣𝑖𝑑𝑦
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)]:
𝑗𝐴 =
π‘šΜ‡π΄
πœ•π‘€π΄
= −𝜌 𝐷𝐴𝐡
|
𝐴
πœ•π‘¦ 𝑦=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.
π‘šΜ‡π‘π‘œπ‘›π‘£ = β„Žπ‘šπ‘Žπ‘ π‘  𝐴 (𝜌𝐴,𝑠 − 𝜌𝐴,∞ ) = β„Žπ‘šπ‘Žπ‘ π‘  𝜌 𝐴 (𝑀𝐴,𝑠 − 𝑀𝐴,∞ )
Where hmass is the average mass transfer coefficient, in m/s; A is the surface area; 𝜌𝐴,𝑠 − 𝜌𝐴,∞ 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:
β„Žπ‘šπ‘Žπ‘ π‘ ,π‘Žπ‘£π‘’ =
1
∬ β„Žπ‘šπ‘Žπ‘ π‘  𝑑𝐴
𝐴
𝐴
The dimensionless Sherwood number (Sh) in mass transfer, is the corresponding number to
Nusselt number (Nu) in heat transfer. Sherwood number is defined as:
π‘†β„Ž =
β„Žπ‘šπ‘Žπ‘ π‘  𝐿
𝐷𝐴𝐡
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„Ž
𝑁𝑒
𝑆𝑑 = 𝜌 π‘π‘œπ‘›π‘£
= 𝑅𝑒 π‘ƒπ‘Ÿ
𝒱𝐢
𝑝
And
2
Mass transfer Stanton number: π‘†π‘‘π‘šπ‘Žπ‘ π‘  =
β„Žπ‘šπ‘Žπ‘ π‘ 
𝒱
π‘†β„Ž
= 𝑅𝑒 𝑆𝑐
Where 𝒱 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:
𝑁𝑒 = 𝑓(𝑅𝑒, π‘ƒπ‘Ÿ)
Sherwood number:
π‘†β„Ž = 𝑓(𝑅𝑒, 𝑆𝑐)
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:
βˆ†πœŒ
3
𝑔 (𝜌∞ − πœŒπ‘  )𝐿𝑐 3 𝑔 ( 𝜌 ) 𝐿𝑐
πΊπ‘Ÿ =
=
πœŒπ‘£ 2
𝑣2
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
βˆ†πœŒ
to temperature differences only, and thus we can replace ( 𝜌 ) by (β ΔT) for convenience, as we
did in natural convection heat transfer. However, in non homogenous fluids, density differences
βˆ†πœŒ
are due to the combined effect of temperature and concentration differences and 𝜌 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
𝑓
= 𝑆𝑑 π‘ƒπ‘Ÿ 3 = π‘†π‘‘π‘šπ‘Žπ‘ π‘  𝑆𝑐 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
𝑆𝑑
𝑆𝑐 3
=( )
π‘†π‘‘π‘šπ‘Žπ‘ π‘ 
π‘ƒπ‘Ÿ
Or
2
2
β„Žβ„Žπ‘’π‘Žπ‘‘
𝑆𝑐 3
𝛼 3
= 𝜌 𝐢𝑝 ( ) = 𝜌 𝐢𝑝 (
) = 𝜌 𝐢𝑝 𝐿𝑒 2/3
β„Žπ‘šπ‘Žπ‘ π‘ 
π‘ƒπ‘Ÿ
𝐷𝐴𝐡
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:
Q̇ sensible,transferred = Q̇latent,absorbed
Or
𝑄̇ = π‘šΜ‡π‘£ β„Žπ‘“π‘”
Figure (4) Various mechanisms of heat transfer
involved during the evaporation of water from the
surface of a lake.
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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)
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