Tugas PP lanjut – Shinta Leonita (0906635772)

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ADVANCED TRANSPORT PHENOMENA
Assignment 1
Shinta Leonita (0906635772)
Problem 1
A viscous fluid is in laminar flow in a slit formed by two parallel walls a distance 2B apart.
Make a differential momentum balance and obtain the expression for the distributions of
momentum flux and velocity. What is the ratio of average to maximum velocity in the slit?
Obtain the analog of the Hagen-Poiseuille law of the slit.
Answer:
Laminar flow in a narrow slit:
Figure 1. Flow Through a Slit, with B << W << L
From figure above, thickness of a system is Δx, length L, and listing the various distributions
to the momentum balance in the z-direction:
ο‚·
Rate of momentum in across slit surface at x
(π‘ŠπΏπœπ‘₯𝑧 )|π‘₯
ο‚·
Rate of momentum out across slit surface at x + Δx
(π‘ŠπΏπœπ‘₯𝑧 )|π‘₯+Δx
ο‚·
(1)
(2)
Rate of momentum in across beam surface at z = 0
(Δxπ‘Šπ‘£π‘§ )(πœŒπ‘£π‘§ )|𝑧=0
(3)
ο‚·
ο‚·
ο‚·
Rate of momentum out across beam surface at z = L
(Δxπ‘Šπ‘£π‘§ )(πœŒπ‘£π‘§ )|𝑧=𝐿
(4)
(Δxπ‘ŠπΏ)πœŒπ‘”
(5)
Gravity force acting on slit shell
Pressure force acting on beam surface at z = 0
(Δxπ‘Š)𝑝0
ο‚·
(6)
Pressure force acting on beam surface at z = L
−(Δxπ‘Š)𝑝𝐿
(7)
Momentum balance (assuming fluid is incompressible, vz is the same at z = 0 and z = L):
(π‘ŠπΏπœπ‘₯𝑧 )|π‘₯ − (π‘ŠπΏπœπ‘₯𝑧 )|π‘₯+Δx + (Δxπ‘Šπ‘£π‘§ )(πœŒπ‘£π‘§ )|𝑧=0 − (Δxπ‘Šπ‘£π‘§ )(πœŒπ‘£π‘§ )|𝑧=𝐿 + (Δxπ‘ŠπΏ)πœŒπ‘” +
Δxπ‘Š(𝑝0 − 𝑝𝐿 )
(8)
Dividing eq. (8) by WL Δx and take the limit as Δx goes to zero; this gives:
𝜏π‘₯𝑧 |π‘₯+Δx −𝜏π‘₯𝑧 |π‘₯
lim (
Δx
Δx→0
)=
(𝑝0 −𝑝𝐿 )
𝐿
+ πœŒπ‘”
(9)
The expression on the left side is the definition of the first derivative, and 𝑃 = 𝑝 + πœŒπ‘”β„Ž =
𝑝 − πœŒπ‘”π‘§. Hence eq. (9) may be written as:
𝑑
𝑑π‘₯
𝜏π‘₯𝑧 =
(𝑃0 −𝑃𝐿 )
(10)
𝐿
Integrating eq. (10) gives:
𝜏π‘₯𝑧 =
(𝑃0 −𝑃𝐿 )
𝐿
π‘₯ + 𝐢1
(11)
The constant C1 must be zero if the momentum flux is not to be infinite at x = 0. Hence the
momentum flux distribution is:
𝝉𝒙𝒛 =
(π‘·πŸŽ −𝑷𝑳 )
𝑳
Substituting Newton’s law of viscosity 𝜏π‘₯𝑧 = −πœ‡
𝑑𝑣𝑧
𝑑π‘₯
=−
𝑑𝑣𝑧
𝑑π‘₯
𝒙
(12)
to eq. (12) gives:
(𝑃0 −𝑃𝐿 )
πœ‡πΏ
π‘₯
(13)
Integrating eq. (13) gives:
(𝑃0 −𝑃𝐿 )
𝑣𝑧 = −
2πœ‡πΏ
π‘₯ 2 + 𝐢2
(14)
Because of the boundary condition that vz be zero at x = ±B, the constant C2 has the value
(𝑃0 −𝑃𝐿 )
2πœ‡πΏ
𝐡 2. Hence the velocity distribution is:
𝒗𝒛 =
(π‘·πŸŽ −𝑷𝑳 )
πŸππ‘³
𝒙 𝟐
π‘©πŸ [𝟏 − ( ) ]
𝑩
(15)
The maximum velocity vz,max at the middle of the slit occurs at x = 0 and has the value:
(𝑃0 −𝑃𝐿 )
𝑣𝑧,π‘šπ‘Žπ‘₯ =
2πœ‡πΏ
𝐡2
(16)
Hence the ratio of the average to the maximum velocity is then:
𝑣𝑧
𝑣𝑧,π‘šπ‘Žπ‘₯
π‘₯ 2
=1−( )
𝐡
𝑾 𝑩
⟨𝒗𝒛 ⟩
𝒗𝒛,π’Žπ’‚π’™
=
∫𝟎 ∫−𝑩[𝟏−(𝒙/𝑩)𝟐 ]π’…π’™π’…π’š
𝑾 𝑩
∫𝟎 ∫−𝑩 π’…π’™π’…π’š
𝟏
=
∫𝟎 (𝟏−πƒπŸ )𝒅𝝃
𝟏
∫𝟎 𝒅𝝃
(17)
𝟏
𝟐
πŸ‘
πŸ‘
= (𝟏 − ) =
(18)
The analog of the Hagen-Poiseuille law:
2
𝑄 = (2π΅π‘Š)⟨𝑣𝑧 ⟩ = (2π΅π‘Š) (3) 𝑣𝑧,π‘šπ‘Žπ‘₯
𝑸=
𝟐 (π‘·πŸŽ −𝑷𝑳 )π‘©πŸ‘ 𝑾
πŸ‘
𝝁𝑳
(19)
(20)
Problem 2
A droplet of substance A is suspended in a stream of gas B. The droplet radius is r1. We
postulate that there is a spherical stagnant gas film of radius r2. the concentration of A in the
gas phase is xA1 at r = r1 and xA2 at r = r2.
a) By a shell balance, show that for steady state diffusion r2NAr is a constant and set the
constant equal to r12NAr1 at the droplet surface.
b) Show that:
r12 N Ar1 ο€½ ο€­
cD AB 2 dx A
r
1 ο€­ x A  dr
c) Integrate that equation between the limits r1 and r2 to get:
N Ar1 ο€½ ο€­
cDAB  r2 οƒΆ xB 2
 οƒ· ln
r2 ο€­ r1   r1 οƒ·οƒΈ xB1
d) If a mass transfer coefficient kv is defined by NAr1 = kv (pA1 – pA2), show that:
kv ο€½
2cD AB / D
 p B ln
Answer:
Figure 2. Diffusion through a Spherical Film
(a) Showing that for steady state diffusion r2NAr is a constant and set the constant equal to
r12NAr1 at the droplet surface:
A mass balance on A over a spherical shell of thickness Δr is (in molar units) at a steady
state:
4πœ‹π‘Ÿ 2 . π‘π΄π‘Ÿ |π‘Ÿ=π‘Ÿ − 4πœ‹(π‘Ÿ + βˆ†π‘Ÿ)2 . π‘π΄π‘Ÿ |π‘Ÿ=π‘Ÿ+βˆ†π‘Ÿ = 0
(1)
(4πœ‹π‘Ÿ 2 . π‘π΄π‘Ÿ )|π‘Ÿ=π‘Ÿ − (4πœ‹π‘Ÿ 2 . π‘π΄π‘Ÿ )|π‘Ÿ=π‘Ÿ+βˆ†π‘Ÿ = 0
(2)
Or, equivalently:
Dividing eq. (2) by 4πΔr and take the limit as Δr goes to zero gives:
𝒅
𝒅𝒓
(π’“πŸ . 𝑡𝑨𝒓 ) = 𝟎
(3)
Eq. (3) may be integrated to give π‘Ÿ 2 . π‘π΄π‘Ÿ = 𝐢1 and we may use the boundary condition
that π‘π΄π‘Ÿ = π‘π΄π‘Ÿ1 at r = r1 (the gas liquid interface) to evaluate the constant and obtain that
r2NAr = r12NAr1
(b) Equation for the radial component in spherical coordinates is:
π‘π΄π‘Ÿ = −𝑐𝐷𝐴𝐡
𝑑π‘₯𝐴
π‘‘π‘Ÿ
+ π‘₯𝐴 (π‘π΄π‘Ÿ + π‘π΅π‘Ÿ )
(4)
If gas B is not moving, then π‘π΅π‘Ÿ may be set equal to zero and the equation may be solved
for the molar flux of A:
𝑐𝐷
π‘π΄π‘Ÿ = − 1−π‘₯𝐴𝐡
𝐴
𝑑π‘₯𝐴
(5)
π‘‘π‘Ÿ
Multiplying by r2 and using the result obtained in (a), then we get:
𝒄𝑫
π’“πŸπŸ π‘΅π‘¨π’“πŸ = − 𝟏−𝒙𝑨𝑩 π’“πŸ
𝑨
𝒅𝒙𝑨
𝒅𝒓
(6)
π‘Ÿ2
π‘₯
π‘Ÿ12 π‘π΄π‘Ÿ1 ∫π‘Ÿ1 1/π‘Ÿ 2 π‘‘π‘Ÿ = −𝑐𝐷𝐴𝐡 ∫π‘₯ 𝐴2
(c)
𝑑π‘₯𝐴
𝐴1 (1−π‘₯𝐴 )
(7)
Integrated that equation gives:
1
1
(1−π‘₯
1
2
)
𝐴2
π‘Ÿ12 π‘π΄π‘Ÿ1 ( − ) = 𝑐𝐷𝐴𝐡 𝑙𝑛
π‘Ÿ
π‘Ÿ
(1−π‘₯ )
π‘Ÿ2 −π‘Ÿ1
π‘Ÿ12 π‘π΄π‘Ÿ1 (
π‘΅π‘¨π’“πŸ =
1
1
1
2
π‘Ÿ2 π‘Ÿ1
𝒄𝑫𝑨𝑩
(π‘₯
)
) = 𝑐𝐷𝐴𝐡 𝑙𝑛 (π‘₯𝐡2)
(9)
𝐡1
𝒓
π’“πŸ −π’“πŸ
(8)
𝐴1
(𝒙
)
(π’“πŸ) 𝒍𝒏 (π’™π‘©πŸ )
𝟏
(π‘₯
(10)
π‘©πŸ
)
(d) At π‘Ÿ → ∞ π‘Ÿ12 π‘π΄π‘Ÿ1 (π‘Ÿ − π‘Ÿ ) = 𝑐𝐷𝐴𝐡 𝑙𝑛 (π‘₯𝐡2 )
𝐡1
π‘π΄π‘Ÿ1 =
(π‘₯
𝑐𝐷𝐴𝐡
π‘Ÿ1
𝑙𝑛
(π‘₯𝐡2 )
(π‘₯𝐡1 )
(11)
−π‘₯𝐡1 )
𝐡2 /π‘₯𝐡1 )
But, (π‘₯𝐡 )𝑙𝑛 = 𝑙𝑛(π‘₯𝐡2
Therefore,
π‘π΄π‘Ÿ1 =
π‘π΄π‘Ÿ1 =
π‘π΄π‘Ÿ1 =
𝑐𝐷𝐴𝐡
1
π‘Ÿ1
(π‘₯𝐡 )𝑙𝑛
𝑐𝐷𝐴𝐡
1
π‘Ÿ1
(π‘₯𝐡 )𝑙𝑛
𝑐𝐷𝐴𝐡
1
π‘Ÿ1
(𝑝𝐡 )𝑙𝑛
(π‘₯𝐡2 − π‘₯𝐡1 )
(12)
(π‘₯𝐴1 − π‘₯𝐴2 )
(13)
(𝑝𝐴1 − 𝑝𝐴2 )
(14)
But, π‘π΄π‘Ÿ1 = π‘˜π‘£ (𝑝𝐴1 − 𝑝𝐴2 )
So,
π’Œπ’— =
𝒄𝑫𝑨𝑩
π’“πŸ(𝒑 )
𝑩 𝒍𝒏
=
πŸπ’„π‘«π‘¨π‘©
𝑫(𝒑𝑩 )𝒍𝒏
(15)
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