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Chapter 7 · 4 hours

Introduction to Mass Transfer

Practice questions

Practice questions and answers

3 exam-style questions on this chapter, written for this site from the official syllabus. We haven’t found past IOE papers for this subject yet; if you have some, share them in the community.

  • Practice · 6 marks

State Fick's law of diffusion and compare it with Fourier's law. Derive the expression for the molar flux in steady equimolar counter diffusion of two ideal gases A and B between two large vessels connected by a tube of length L.

Answer

Fick's law

Mass transfer by molecular diffusion is the movement of a species because of a concentration difference. For a binary mixture, the molar flux of A in the xx direction (relative to the mixture as a whole) is

JA=−DABdCAdxJ_A = -D_{AB}\frac{dC_A}{dx}

where DABD_{AB} is the diffusion coefficient (m2^2/s), CAC_A the molar concentration (kmol/m3^3). The flux is toward lower concentration.

QuantityHeat conductionMass diffusion
Lawq′′=−k dT/dxq'' = -k\,dT/dxJA=−DAB dCA/dxJ_A = -D_{AB}\,dC_A/dx
Driving forceTemperature gradientConcentration gradient
Propertykk (or α\alpha)DABD_{AB}
Units of propertyW/m K (m2^2/s)m2^2/s

Typical DABD_{AB}: gases about 10−510^{-5} m2^2/s, liquids about 10−910^{-9} m2^2/s, solids 10−1010^{-10} to 10−1410^{-14} m2^2/s.

Equimolar counter diffusion

Two vessels, at the same total pressure PP and temperature TT, are connected by a tube of length LL. Gas A diffuses from vessel 1 (partial pressure pA1p_{A1}) to vessel 2 (pA2p_{A2}), and gas B diffuses in the opposite direction at the same molar rate: NA=−NBN_A = -N_B.

 [ vessel 1 ]=======L=======[ vessel 2 ]
   pA1 high        A -->       pA2 low
   pB1 low         <-- B       pB2 high

Since there is no net bulk flow, the flux is only diffusion:

NA=−DABdCAdxN_A = -D_{AB}\frac{dC_A}{dx}

At steady state NAN_A is constant. Integrate from x=0x = 0 (CA1C_{A1}) to x=Lx = L (CA2C_{A2}):

NA=DABL (CA1−CA2)N_A = \frac{D_{AB}}{L}\,(C_{A1}-C_{A2})

For ideal gases CA=pA/RˉTC_A = p_A/\bar R T, so

NA=DABRˉT L (pA1−pA2)N_A = \frac{D_{AB}}{\bar R T\,L}\,(p_{A1}-p_{A2})

with Rˉ=8.314\bar R = 8.314 kJ/kmol K (or 8314 J/kmol K, with pp in Pa). The concentration profile of A is linear in xx, as for conduction through a plane wall.

  • Practice · 6 marks

Water at 25 °C evaporates in a vertical glass tube of internal diameter 10 mm. The water surface is 150 mm below the open top of the tube. Dry air at 1 atm (101 325 Pa) and 25 °C blows across the top so that the vapour concentration there is zero. The saturation pressure of water at 25 °C is 3.17 kPa and the diffusion coefficient of water vapour in air is 0.256 x 10^-4 m^2/s. Treating the air as stagnant, find the molar flux of water vapour and the mass evaporated per hour. (M of water = 18 kg/kmol.)

Answer

Model

Water vapour (A) diffuses upward through stagnant air (B). Air does not move, so NB=0N_B = 0 and there is a net bulk flow of the mixture (Stefan flow). For steady state, constant temperature and pressure:

NA=DABPRˉT z ln⁡P−pA2P−pA1N_A = \frac{D_{AB}P}{\bar R T\,z}\,\ln\frac{P-p_{A2}}{P-p_{A1}}

where zz is the diffusion length, pA1p_{A1} the vapour pressure at the water surface and pA2p_{A2} at the top.

Data

  • P=101 325P = 101\,325 Pa, T=298T = 298 K, z=0.15z = 0.15 m
  • pA1=3170p_{A1} = 3170 Pa (saturated at the water surface), pA2=0p_{A2} = 0 (dry air at top)
  • DAB=0.256×10−4D_{AB} = 0.256\times10^{-4} m2^2/s, Rˉ=8.314\bar R = 8.314 J/mol K
  • Ac=π(0.01)2/4=7.854×10−5A_c = \pi(0.01)^2/4 = 7.854\times10^{-5} m2^2

Molar flux

DABPRˉTz=0.256×10−4×101 3258.314×298×0.15=6.98×10−3 mol/m2sln⁡101 325−0101 325−3170=ln⁡(1.0323)=0.03178NA=6.98×10−3×0.03178=2.22×10−4 mol/m2s\begin{aligned} \frac{D_{AB}P}{\bar RTz} &= \frac{0.256\times10^{-4}\times101\,325}{8.314\times298\times0.15} = 6.98\times10^{-3}\ \text{mol/m}^2\text{s}\\ \ln\frac{101\,325-0}{101\,325-3170} &= \ln(1.0323) = 0.03178\\ N_A &= 6.98\times10^{-3}\times0.03178 = 2.22\times10^{-4}\ \text{mol/m}^2\text{s} \end{aligned}

That is 2.22×10−72.22\times10^{-7} kmol/m2^2s.

Evaporation rate

n˙=NAAc=2.2185×10−4×7.854×10−5=1.742×10−8 mol/sm˙=n˙×18 g/mol=3.14×10−7 g/s=3.14×10−7×3600=1.13×10−3 g/h=1.13 mg/h\begin{aligned} \dot n &= N_AA_c = 2.2185\times10^{-4}\times7.854\times10^{-5} = 1.742\times10^{-8}\ \text{mol/s}\\ \dot m &= \dot n\times18\ \text{g/mol} = 3.14\times10^{-7}\ \text{g/s}\\ &= 3.14\times10^{-7}\times3600 = 1.13\times10^{-3}\ \text{g/h} = 1.13\ \text{mg/h} \end{aligned}

Answer: NA≈2.22×10−4 mol/m2N_A \approx 2.22\times10^{-4}\ \text{mol/m}^2s; evaporation rate about 1.131.13 mg per hour.

  • Practice · 6 marks

Define the convective mass transfer coefficient. Explain the Schmidt, Sherwood and Lewis numbers. State the analogy between momentum, heat and mass transfer (Chilton-Colburn) and give two correlations used for convective mass transfer.

Answer

Convective mass transfer coefficient

When a fluid flows over a surface from which species A is transferred, the flux is written in the form of Newton's law of cooling:

NA=hm (CAs−CA∞)N_A = h_m\,(C_{As}-C_{A\infty})

hmh_m (m/s) is the convective mass transfer coefficient, found from correlations just like hh.

Dimensionless numbers

NumberDefinitionMeaning
Schmidt, ScScνDAB\dfrac{\nu}{D_{AB}}Momentum diffusivity / mass diffusivity (mass analogue of PrPr)
Sherwood, ShShhmLDAB\dfrac{h_mL}{D_{AB}}Convective / diffusive mass transfer (analogue of NuNu)
Lewis, LeLeαDAB=ScPr\dfrac{\alpha}{D_{AB}} = \dfrac{Sc}{Pr}Thermal diffusivity / mass diffusivity
Stanton (mass), StmSt_mhmV=ShRe Sc\dfrac{h_m}{V}= \dfrac{Sh}{Re\,Sc}Mass transfer / mass capacity of the stream

Analogy between momentum, heat and mass transfer

Because all three processes are carried by the same molecular and eddy motion in the boundary layer, their equations are similar. Reynolds analogy (for Pr=Sc=1Pr = Sc = 1): f2=St=Stm\dfrac{f}{2}=St=St_m. For other fluids the Chilton-Colburn analogy applies (0.6<Pr<600.6 < Pr < 60, 0.6<Sc<30000.6 < Sc < 3000):

jH=St Pr2/3=f2=jM=Stm Sc2/3j_H = St\,Pr^{2/3}= \frac{f}{2}= j_M = St_m\,Sc^{2/3}

Hence, if hh is known, hmh_m follows from

hhm=ρcp Le2/3\frac{h}{h_m} = \rho c_p\,Le^{2/3}

Mass transfer can thus be predicted from heat transfer results by replacing Nu→ShNu \to Sh and Pr→ScPr \to Sc.

Correlations

  • Laminar flow over a flat plate: ShL=0.664 ReL1/2 Sc1/3Sh_L = 0.664\,Re_L^{1/2}\,Sc^{1/3}.
  • Turbulent flow in tubes: Sh=0.023 Re0.83 Sc1/3Sh = 0.023\,Re^{0.83}\,Sc^{1/3} (Gilliland-Sherwood form).
  • Flow past a sphere (Frossling): Sh=2+0.552 Re1/2Sc1/3Sh = 2 + 0.552\,Re^{1/2}Sc^{1/3}.

Written from the official syllabus. Questions and answers are written for this site; check them against your class notes.

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