Diffusion and Fick's Laws
Fick's First Law (Steady-State Diffusion)
Molar flux (equimolar counterdiffusion):
\[J_A = -D_{AB} \frac{dC_A}{dz}\]
- JA = molar flux of component A (mol/m²·s or lbmol/ft²·h)
- DAB = diffusivity of A in B (m²/s or ft²/h)
- CA = molar concentration of A (mol/m³ or lbmol/ft³)
- z = distance in direction of diffusion (m or ft)
Mass flux form:
\[j_A = -D_{AB} \frac{d\rho_A}{dz}\]
- jA = mass flux of component A (kg/m²·s or lb/ft²·h)
- ρA = mass concentration of A (kg/m³ or lb/ft³)
For gases (ideal gas):
\[J_A = -\frac{D_{AB}}{RT} \frac{dp_A}{dz}\]
- pA = partial pressure of A (Pa or psia)
- R = universal gas constant (8.314 J/mol·K or 1545 ft·lbf/lbmol·°R)
- T = absolute temperature (K or °R)
Fick's Second Law (Unsteady-State Diffusion)
\[\frac{\partial C_A}{\partial t} = D_{AB} \frac{\partial^2 C_A}{\partial z^2}\]
- t = time (s or h)
- Applies when concentration changes with time
- Assumes constant diffusivity
Diffusion Through Stagnant Film
One-dimensional diffusion of A through stagnant B:
\[N_A = \frac{D_{AB} P}{RT(z_2 - z_1)} \ln\left(\frac{P - p_{A2}}{P - p_{A1}}\right)\]
- NA = molar flux of A (mol/m²·s or lbmol/ft²·h)
- P = total pressure (Pa or psia)
- pA1, pA2 = partial pressures of A at positions z₁ and z₂
- z₂ - z₁ = diffusion path length (m or ft)
Alternative form using log mean:
\[N_A = \frac{D_{AB} P}{RT \Delta z} \frac{(p_{A1} - p_{A2})}{(p_{B})_{lm}}\]
where the log mean of inert component B:
\[(p_B)_{lm} = \frac{p_{B2} - p_{B1}}{\ln(p_{B2}/p_{B1})}\]
Equimolar Counterdiffusion
\[N_A = \frac{D_{AB}}{RT \Delta z}(p_{A1} - p_{A2})\]
- Applies when equal molar amounts of A and B diffuse in opposite directions
- Net molar flux is zero (NA = -NB)
Diffusivity Estimation
Gas Diffusivity
Fuller-Schettler-Giddings Equation:
\[D_{AB} = \frac{0.00143 T^{1.75}}{P M_{AB}^{0.5}[(\Sigma v)_A^{1/3} + (\Sigma v)_B^{1/3}]^2}\]
- DAB = diffusivity (cm²/s)
- T = temperature (K)
- P = pressure (atm)
- MAB = (2/MA + 2/MB)-1, reduced molecular weight
- Σv = sum of atomic diffusion volumes
Temperature and pressure correction:
\[D_{AB,2} = D_{AB,1} \left(\frac{T_2}{T_1}\right)^{1.75} \left(\frac{P_1}{P_2}\right)\]
Liquid Diffusivity
Wilke-Chang Equation:
\[D_{AB} = \frac{7.4 \times 10^{-8} (\phi M_B)^{0.5} T}{\mu_B V_A^{0.6}}\]
- DAB = diffusivity (cm²/s)
- φ = association parameter for solvent B (2.6 for water, 1.9 for methanol, 1.5 for ethanol, 1.0 for unassociated solvents)
- MB = molecular weight of solvent B (g/mol)
- T = temperature (K)
- μB = viscosity of solvent B (cP)
- VA = molar volume of solute A at normal boiling point (cm³/mol)
Temperature correction for liquid diffusivity:
\[\frac{D_2}{D_1} = \frac{T_2 \mu_1}{T_1 \mu_2}\]
Mass Transfer Coefficients
Film Theory
Gas phase mass transfer coefficient:
\[k_y = \frac{D_{AB}}{\delta}\]
Liquid phase mass transfer coefficient:
\[k_x = \frac{D_{AB}}{\delta}\]
- ky = gas phase mass transfer coefficient (mol/m²·s or lbmol/ft²·h)
- kx = liquid phase mass transfer coefficient (mol/m²·s or lbmol/ft²·h)
- δ = film thickness (m or ft)
Flux Equations Using Mass Transfer Coefficients
Gas phase (mole fraction driving force):
\[N_A = k_y (y_A - y_{Ai})\]
Gas phase (partial pressure driving force):
\[N_A = k_G (p_A - p_{Ai})\]
Liquid phase (mole fraction driving force):
\[N_A = k_x (x_{Ai} - x_A)\]
Liquid phase (concentration driving force):
\[N_A = k_L (C_{Ai} - C_A)\]
- yA = mole fraction of A in bulk gas
- yAi = mole fraction of A at interface
- xA = mole fraction of A in bulk liquid
- xAi = mole fraction of A at interface
Overall Mass Transfer Coefficients
Gas phase overall coefficient:
\[\frac{1}{K_y} = \frac{1}{k_y} + \frac{m}{k_x}\]
\[\frac{1}{K_G} = \frac{1}{k_G} + \frac{H}{k_L}\]
Liquid phase overall coefficient:
\[\frac{1}{K_x} = \frac{1}{mk_y} + \frac{1}{k_x}\]
\[\frac{1}{K_L} = \frac{1}{Hk_G} + \frac{1}{k_L}\]
- Ky, KG = overall gas phase mass transfer coefficients
- Kx, KL = overall liquid phase mass transfer coefficients
- m = slope of equilibrium line (y* = mx)
- H = Henry's law constant (p = Hx)
Relationship Between Coefficients
\[k_G = k_y c_{total,gas}\]
\[k_L = k_x c_{total,liquid}\]
\[K_G = K_y c_{total,gas}\]
\[K_L = K_x c_{total,liquid}\]
- ctotal = total molar concentration (mol/m³ or lbmol/ft³)
Convective Mass Transfer Correlations
Dimensionless Numbers
Schmidt Number:
\[Sc = \frac{\mu}{\rho D_{AB}} = \frac{\nu}{D_{AB}}\]
- Sc = ratio of momentum diffusivity to mass diffusivity
- μ = dynamic viscosity (Pa·s or lb/ft·s)
- ρ = density (kg/m³ or lb/ft³)
- ν = kinematic viscosity (m²/s or ft²/s)
Sherwood Number:
\[Sh = \frac{k_c L}{D_{AB}}\]
- Sh = ratio of convective to diffusive mass transfer
- kc = mass transfer coefficient (m/s or ft/s)
- L = characteristic length (m or ft)
- Analogous to Nusselt number in heat transfer
Reynolds Number:
\[Re = \frac{\rho v L}{\mu} = \frac{v L}{\nu}\]
- v = velocity (m/s or ft/s)
Flat Plate (Laminar Flow)
\[Sh_L = 0.664 Re_L^{0.5} Sc^{1/3}\]
- Valid for ReL < 5="" ×="">
- Sc > 0.6
- L = length of plate
Flat Plate (Turbulent Flow)
\[Sh_L = 0.037 Re_L^{0.8} Sc^{1/3}\]
- Valid for 5 × 10⁵ <>L <>
- 0.6 < sc=""><>
Flow in Tubes (Laminar)
Short tubes (developing flow):
\[Sh_D = 1.86 \left(Re_D Sc \frac{D}{L}\right)^{1/3} \left(\frac{\mu_b}{\mu_w}\right)^{0.14}\]
- Valid for ReD <>
- D = tube diameter
- L = tube length
- μb = viscosity at bulk conditions
- μw = viscosity at wall conditions
Long tubes (fully developed):
\[Sh_D = 3.66\]
- For constant wall concentration
- Valid when L/D is large
Flow in Tubes (Turbulent)
Chilton-Colburn analogy:
\[Sh = 0.023 Re^{0.8} Sc^{1/3}\]
- Valid for Re > 10,000
- 0.6 < sc=""><>
- L/D > 60
Sieder-Tate form:
\[Sh_D = 0.027 Re_D^{0.8} Sc^{1/3} \left(\frac{\mu_b}{\mu_w}\right)^{0.14}\]
Flow Around Spheres
Ranz-Marshall correlation:
\[Sh_d = 2.0 + 0.6 Re_d^{0.5} Sc^{1/3}\]
- Valid for 1 <>d <>
- d = sphere diameter
- First term (2.0) represents pure molecular diffusion
Packed Beds
Wilson-Geankoplis correlation:
\[j_D = \frac{Sh}{Re Sc^{1/3}} = 1.09 Re^{-2/3}\]
- Valid for 0.0016 < re=""><>
- 165 < sc=""><>
\[j_D = 0.250 Re^{-0.31}\]
Interphase Mass Transfer (Two-Phase Systems)
Equilibrium Relationships
Henry's Law:
\[p_A = H x_A\]
- pA = partial pressure of A in gas phase (Pa or psia)
- H = Henry's law constant (Pa or psia)
- xA = mole fraction of A in liquid phase
- Applies to dilute solutions
Alternative form:
\[y_A = m x_A\]
- m = H/P = equilibrium constant
- yA = mole fraction of A in gas phase
Raoult's Law:
\[p_A = x_A P_A^{sat}\]
- PAsat = vapor pressure of pure A (Pa or psia)
- Applies to ideal solutions
Two-Resistance Theory
Overall flux with gas phase driving force:
\[N_A = K_y a (y_A - y_A^*)\]
\[N_A = K_G a (p_A - p_A^*)\]
Overall flux with liquid phase driving force:
\[N_A = K_x a (x_A^* - x_A)\]
\[N_A = K_L a (C_A^* - C_A)\]
- a = interfacial area per unit volume (m²/m³ or ft²/ft³)
- yA* = gas phase mole fraction in equilibrium with bulk liquid
- xA* = liquid phase mole fraction in equilibrium with bulk gas
Absorption and Stripping
Operating Line for Absorption Column
Material balance:
\[L(x_2 - x_1) = G(y_1 - y_2)\]
Operating line equation:
\[y = \frac{L}{G}x + \left(y_1 - \frac{L}{G}x_1\right)\]
- L = molar flow rate of liquid (mol/s or lbmol/h)
- G = molar flow rate of gas (mol/s or lbmol/h)
- x₁ = inlet liquid mole fraction (bottom)
- x₂ = outlet liquid mole fraction (top)
- y₁ = inlet gas mole fraction (bottom)
- y₂ = outlet gas mole fraction (top)
Minimum Liquid-to-Gas Ratio
\[\left(\frac{L}{G}\right)_{min} = \frac{y_1 - y_2}{x_2^* - x_1}\]
- x₂* = liquid mole fraction in equilibrium with y₁
- At minimum L/G, infinite stages are required
Height of Transfer Unit (HTU)
Gas phase HTU:
\[H_{OG} = \frac{G}{K_G a S}\]
\[H_G = \frac{G}{k_G a S}\]
Liquid phase HTU:
\[H_{OL} = \frac{L}{K_L a S}\]
\[H_L = \frac{L}{k_L a S}\]
- HOG = overall gas phase height of transfer unit (m or ft)
- HG = gas phase height of transfer unit (m or ft)
- HOL = overall liquid phase height of transfer unit (m or ft)
- HL = liquid phase height of transfer unit (m or ft)
- S = column cross-sectional area (m² or ft²)
Number of Transfer Units (NTU)
Gas phase NTU (dilute systems):
\[N_{OG} = \int_{y_2}^{y_1} \frac{dy}{y - y^*}\]
For linear equilibrium (y* = mx + b) and constant L/G:
\[N_{OG} = \frac{\ln\left[\left(\frac{y_1 - mx_1 - b}{y_2 - mx_1 - b}\right)\left(1 - \frac{mG}{L}\right) + \frac{mG}{L}\right]}{1 - \frac{mG}{L}}\]
When mG/L = 1:
\[N_{OG} = \frac{y_1 - y_2}{y - y^*}\]
where (y - y*) is the average driving force.
Liquid phase NTU:
\[N_{OL} = \int_{x_1}^{x_2} \frac{dx}{x^* - x}\]
Column Height
\[Z = H_{OG} \times N_{OG}\]
\[Z = H_{OL} \times N_{OL}\]
- Z = packed height of column (m or ft)
Relationship Between HTU Values
\[H_{OG} = H_G + \frac{mG}{L} H_L\]
\[H_{OL} = H_L + \frac{L}{mG} H_G\]
Absorption Factor
\[A = \frac{L}{mG}\]
- A = absorption factor (dimensionless)
- A > 1.0 indicates favorable absorption
- A < 1.0="" indicates="" stripping="">
For stripping:
\[S = \frac{mG}{L} = \frac{1}{A}\]
Kremser Equation (Isothermal Absorption)
Number of theoretical stages for absorption:
\[N = \frac{\ln\left[\left(\frac{y_1 - mx_1}{y_2 - mx_1}\right)\left(1 - \frac{1}{A}\right) + \frac{1}{A}\right]}{\ln A}\]
When A = 1:
\[N = \frac{y_1 - mx_1}{y_2 - mx_1} - 1\]
For stripping:
\[N = \frac{\ln\left[\left(\frac{x_2 - y_1/m}{x_1 - y_1/m}\right)\left(1 - S\right) + S\right]}{\ln S}\]
- N = number of theoretical stages
- Assumes constant L, G, m, and temperature
Distillation
Vapor-Liquid Equilibrium
Relative volatility:
\[\alpha_{AB} = \frac{y_A/x_A}{y_B/x_B} = \frac{K_A}{K_B}\]
- αAB = relative volatility of A to B
- KA = yA/xA = equilibrium ratio for A
- KB = yB/xB = equilibrium ratio for B
For binary system (A + B = 1):
\[y_A = \frac{\alpha x_A}{1 + (\alpha - 1)x_A}\]
- Assumes constant relative volatility
McCabe-Thiele Method
Rectifying section operating line:
\[y_{n+1} = \frac{R}{R+1} x_n + \frac{x_D}{R+1}\]
- R = reflux ratio (LD/D)
- xD = distillate composition (mole fraction)
- LD = liquid flow in rectifying section
- D = distillate flow rate
Slope of rectifying line:
\[slope = \frac{R}{R+1} = \frac{L_D}{V}\]
y-intercept of rectifying line:
\[y_{int} = \frac{x_D}{R+1}\]
Stripping section operating line:
\[y_m = \frac{L_S}{V_S} x_m - \frac{W x_W}{V_S}\]
- LS = liquid flow in stripping section
- VS = vapor flow in stripping section
- W = bottoms flow rate
- xW = bottoms composition (mole fraction)
Alternative form:
\[y_m = \frac{L_S}{L_S - W} x_m - \frac{W x_W}{L_S - W}\]
Minimum Reflux Ratio
At feed stage (for saturated liquid feed):
\[R_{min} = \frac{x_D - y_f^*}{y_f^* - x_f}\]
- xf = feed composition (liquid mole fraction)
- yf* = vapor composition in equilibrium with xf
Underwood equation for minimum reflux:
\[R_{min} + 1 = \frac{\alpha_A x_{D,A}}{\alpha_A - \theta} + \frac{\alpha_B x_{D,B}}{\alpha_B - \theta}\]
where θ is found from:
\[\frac{\alpha_A x_{F,A}}{\alpha_A - \theta} + \frac{\alpha_B x_{F,B}}{\alpha_B - \theta} = 1 - q\]
- Valid for multicomponent systems
- q = thermal condition of feed
Feed Line (q-Line)
Feed line equation:
\[y = \frac{q}{q-1} x - \frac{x_f}{q-1}\]
Slope of feed line:
\[slope = \frac{q}{q-1}\]
Thermal condition parameter:
\[q = \frac{H_V - H_F}{H_V - H_L}\]
- HV = enthalpy of saturated vapor
- HF = enthalpy of feed
- HL = enthalpy of saturated liquid
Values of q:
- q = 1: saturated liquid feed (slope = ∞, vertical line)
- q = 0: saturated vapor feed (slope = 0, horizontal line)
- q > 1: subcooled liquid feed
- 0 < q="">< 1:="" partially="" vaporized="">
- q < 0:="" superheated="" vapor="">
Total Reflux
Fenske equation (minimum number of stages):
\[N_{min} = \frac{\ln\left[\frac{x_D}{1-x_D} \cdot \frac{1-x_W}{x_W}\right]}{\ln \alpha}\]
- Nmin = minimum number of theoretical stages at total reflux
- Does not include reboiler
- Assumes constant relative volatility
Actual Number of Stages
Gilliland correlation:
\[Y = 1 - \exp\left[\frac{(1 + 54.4X)(X - 1)}{11 + 117.2X}\right]\]
where:
\[X = \frac{R - R_{min}}{R + 1}\]
\[Y = \frac{N - N_{min}}{N + 1}\]
- N = actual number of theoretical stages
- R = actual reflux ratio
Column Efficiency
Overall column efficiency:
\[E_O = \frac{N}{N_{actual}}\]
- N = number of theoretical stages
- Nactual = actual number of trays
Murphree tray efficiency (vapor basis):
\[E_{MV} = \frac{y_{n+1} - y_n}{y_{n+1}^* - y_n}\]
- yn+1 = actual vapor composition leaving stage n
- yn = actual vapor composition entering stage n
- yn+1* = equilibrium vapor composition with liquid leaving stage n
Murphree tray efficiency (liquid basis):
\[E_{ML} = \frac{x_n - x_{n-1}}{x_n^* - x_{n-1}}\]
Material Balance
Overall material balance:
\[F = D + W\]
Component material balance:
\[F x_F = D x_D + W x_W\]
- F = feed flow rate (mol/s or lbmol/h)
- D = distillate flow rate (mol/s or lbmol/h)
- W = bottoms flow rate (mol/s or lbmol/h)
Distribution Coefficient
\[K_D = \frac{C_{A,extract}}{C_{A,raffinate}}\]
- KD = distribution coefficient
- CA,extract = concentration of A in extract phase
- CA,raffinate = concentration of A in raffinate phase
Single-Stage Extraction
Fraction extracted:
\[E = \frac{V K_D}{V K_D + F}\]
- E = extraction efficiency (fraction of solute extracted)
- V = volume of extract phase (solvent)
- F = volume of raffinate phase (feed)
Multistage Crosscurrent Extraction
Fraction remaining after n stages:
\[x_n = x_0 \left(\frac{F}{V K_D + F}\right)^n\]
- xn = concentration remaining after n stages
- x₀ = initial concentration
- n = number of stages
Multistage Countercurrent Extraction
Operating line:
\[y_{n+1} = \frac{F}{S} x_n + \left(y_1 - \frac{F}{S} x_0\right)\]
- F = raffinate flow rate
- S = solvent (extract) flow rate
- y = solute concentration in extract phase
- x = solute concentration in raffinate phase
Minimum solvent-to-feed ratio:
\[\left(\frac{S}{F}\right)_{min} = \frac{x_0 - x_N}{y_1^* - y_0}\]
- y₁* = extract composition in equilibrium with x₀
- Requires infinite stages
Adsorption
Adsorption Isotherms
Langmuir isotherm:
\[q = \frac{q_m b C}{1 + b C}\]
- q = amount adsorbed per unit mass of adsorbent (mol/kg or lb/lb)
- qm = monolayer capacity
- b = Langmuir constant (related to adsorption energy)
- C = equilibrium concentration in fluid phase
- Assumes monolayer coverage and uniform surface
Freundlich isotherm:
\[q = K_F C^{1/n}\]
- KF = Freundlich capacity factor
- n = Freundlich intensity parameter (typically n > 1)
- Empirical equation
Linear isotherm:
\[q = K C\]
- K = partition coefficient
- Valid at low concentrations
BET isotherm (multilayer adsorption):
\[\frac{p}{V(p_0 - p)} = \frac{1}{V_m C_{BET}} + \frac{(C_{BET} - 1)p}{V_m C_{BET} p_0}\]
- V = volume of gas adsorbed at pressure p
- Vm = volume for monolayer coverage
- p₀ = saturation pressure
- CBET = BET constant (related to heat of adsorption)
Breakthrough Curve Analysis
Mass transfer zone (MTZ) length:
\[L_{MTZ} = v_0 (t_b - t_s)\]
- LMTZ = length of mass transfer zone
- v₀ = superficial velocity
- tb = breakthrough time
- ts = stoichiometric (equilibrium) time
Column capacity:
\[q_{total} = \int_0^{t_{sat}} C_0 Q (1 - \frac{C}{C_0}) dt\]
- qtotal = total amount adsorbed
- C₀ = inlet concentration
- C = outlet concentration
- Q = volumetric flow rate
- tsat = saturation time
Crystallization
Supersaturation
Absolute supersaturation:
\[\Delta C = C - C^*\]
Relative supersaturation:
\[S = \frac{C - C^*}{C^*}\]
Supersaturation ratio:
\[\sigma = \frac{C}{C^*}\]
- C = actual concentration
- C* = saturation (equilibrium) concentration
Crystal Growth Rate
Overall growth rate:
\[G = \frac{dL}{dt}\]
- G = linear growth rate (m/s or μm/h)
- L = characteristic crystal size
Mass transfer controlled growth:
\[G = k_d (C - C^*)\]
- kd = mass transfer coefficient
Nucleation Rate
Primary homogeneous nucleation:
\[B = k_n \exp\left(-\frac{\Delta G_{crit}}{kT}\right)\]
Secondary nucleation:
\[B = k_n M_T^j N^b (C - C^*)^i\]
- B = nucleation rate (number/m³·s)
- MT = magma density (mass of crystals per volume of slurry)
- N = agitation rate
- j, b, i = empirical exponents
Population Balance
For steady-state MSMPR (Mixed Suspension Mixed Product Removal) crystallizer:
\[n = n_0 \exp\left(-\frac{L}{G\tau}\right)\]
- n = population density at size L (number/m⁴)
- n₀ = population density of nuclei (L = 0)
- τ = residence time
Relationship between nucleation and growth:
\[n_0 = \frac{B^0}{G}\]
- B⁰ = nucleation rate at zero size
Crystal Size Distribution
Dominant crystal size (MSMPR):
\[L_{dominant} = 3G\tau\]
Mass-average size:
\[\overline{L}_m = 4G\tau\]
Yield
Theoretical yield (cooling crystallization):
\[Y = F(x_F - x_M)\]
- Y = mass of crystals produced
- F = feed mass
- xF = feed concentration (mass fraction)
- xM = mother liquor concentration at final temperature
Humidification and Drying
Psychrometric Properties
Humidity (absolute humidity):
\[H = \frac{mass_{water}}{mass_{dry air}} = \frac{M_{H_2O}}{M_{air}} \frac{p_{H_2O}}{P - p_{H_2O}}\]
\[H = 0.622 \frac{p_{H_2O}}{P - p_{H_2O}}\]
- H = absolute humidity (kg H₂O/kg dry air or lb H₂O/lb dry air)
- pH₂O = partial pressure of water vapor (Pa or psia)
- P = total pressure (Pa or psia)
- MH₂O = 18 g/mol
- Mair = 29 g/mol
Saturation humidity:
\[H_s = 0.622 \frac{p_{H_2O}^{sat}}{P - p_{H_2O}^{sat}}\]
- Hs = saturation humidity at given temperature
- pH₂Osat = saturation vapor pressure at temperature T
Relative humidity:
\[RH = \frac{p_{H_2O}}{p_{H_2O}^{sat}} \times 100\%\]
\[RH = \frac{H(P - p_{H_2O}^{sat})}{H_s(P - p_{H_2O})} \times 100\%\]
Percentage humidity:
\[H_{pct} = \frac{H}{H_s} \times 100\%\]
Humid volume:
\[v_H = \left(\frac{1}{M_{air}} + \frac{H}{M_{H_2O}}\right)\frac{RT}{P}\]
\[v_H = \left(0.0345 + 0.0568 H\right)\frac{T}{P}\]
- vH = humid volume (m³/kg dry air or ft³/lb dry air)
- T = absolute temperature (K or °R)
- Second equation: T in K, P in atm, vH in m³/kg
Humid heat:
\[c_s = c_{p,air} + H c_{p,H_2O}\]
\[c_s = 1.005 + 1.88 H\]
- cs = humid heat (kJ/kg dry air·K or Btu/lb dry air·°F)
- cp,air = 1.005 kJ/kg·K (0.24 Btu/lb·°F)
- cp,H₂O = 1.88 kJ/kg·K (0.45 Btu/lb·°F)
Adiabatic Saturation and Wet Bulb Temperature
Adiabatic saturation equation:
\[H_s - H = \frac{c_s (T - T_{as})}{\lambda_{as}}\]
- Tas = adiabatic saturation temperature
- λas = latent heat of vaporization at Tas
For air-water system (Lewis number ≈ 1):
\[T_{wb} \approx T_{as}\]
- Twb = wet bulb temperature
- Wet bulb and adiabatic saturation temperatures are approximately equal for air-water
Dew point temperature:
- Temperature at which pH₂Osat = pH₂O
- Air becomes saturated if cooled to dew point
Enthalpy of Humid Air
\[H_{humid} = c_s T + H \lambda_0\]
\[H_{humid} = 1.005 T + H(2501 + 1.88 T)\]
- Hhumid = enthalpy of humid air (kJ/kg dry air or Btu/lb dry air)
- λ₀ = latent heat at reference temperature (0°C or 32°F)
- Second equation: T in °C, Hhumid in kJ/kg dry air
Drying Rate
Constant rate period:
\[R_c = k_y (H_s - H_\infty)\]
- Rc = constant drying rate (kg/m²·s or lb/ft²·h)
- ky = mass transfer coefficient
- Hs = saturation humidity at surface temperature
- H∞ = bulk air humidity
Falling rate period (linear):
\[R = R_c \frac{X - X_e}{X_c - X_e}\]
- X = free moisture content (kg H₂O/kg dry solid)
- Xc = critical moisture content
- Xe = equilibrium moisture content
Drying time (constant rate period):
\[t_c = \frac{L_s (X_0 - X_c)}{R_c}\]
- Ls = mass of dry solid per unit area (kg/m² or lb/ft²)
- X₀ = initial moisture content
Drying time (falling rate period):
\[t_f = \frac{L_s (X_c - X_e)}{R_c} \ln\left(\frac{X_c - X_e}{X_f - X_e}\right)\]
- Xf = final moisture content
- Valid for linear falling rate period
Membrane Separation
Permeability and Flux
Gas permeation flux:
\[J_i = \frac{P_i}{l}(p_{i,feed} - p_{i,permeate})\]
- Ji = flux of component i (mol/m²·s or cm³(STP)/cm²·s)
- Pi = permeability of component i (mol·m/m²·s·Pa or Barrer)
- l = membrane thickness (m or cm)
- pi = partial pressure (Pa or atm)
Permeance:
\[Q_i = \frac{P_i}{l}\]
- Qi = permeance (mol/m²·s·Pa or GPU)
- 1 GPU = 10⁻⁶ cm³(STP)/cm²·s·cmHg
Selectivity (ideal separation factor):
\[\alpha_{ij} = \frac{P_i}{P_j}\]
- αij = ideal selectivity for i over j
Reverse Osmosis
Water flux:
\[J_w = A(\Delta P - \Delta \pi)\]
- Jw = water flux (m³/m²·s or gal/ft²·day)
- A = water permeability coefficient (m³/m²·s·Pa or gal/ft²·day·psi)
- ΔP = transmembrane pressure difference (Pa or psi)
- Δπ = osmotic pressure difference (Pa or psi)
Salt flux:
\[J_s = B(\Delta C)\]
- Js = salt flux (kg/m²·s)
- B = salt permeability coefficient (m/s)
- ΔC = concentration difference (kg/m³)
Osmotic pressure (van't Hoff equation):
\[\pi = i M R T\]
- π = osmotic pressure (Pa or psi)
- i = van't Hoff factor (number of ions per molecule)
- M = molar concentration (mol/L or mol/m³)
Ultrafiltration and Microfiltration
Flux through membrane:
\[J = \frac{\Delta P}{\mu (R_m + R_f)}\]
- J = permeate flux (m/s or gal/ft²·day)
- μ = viscosity (Pa·s or cP)
- Rm = membrane resistance (1/m)
- Rf = fouling resistance (1/m)
Concentration polarization:
\[\frac{C_w}{C_b} = \exp\left(\frac{J}{k}\right)\]
- Cw = concentration at membrane wall
- Cb = bulk concentration
- k = mass transfer coefficient (m/s)
Single-Stage Leaching
Material balance:
\[F + S = E + R\]
\[F x_F + S x_S = E y_E + R x_R\]
- F = feed solids flow rate
- S = solvent flow rate
- E = extract (overflow) flow rate
- R = raffinate (underflow) flow rate
- x, y = mass fractions of solute
Multistage Countercurrent Leaching
Operating line (similar to extraction):
\[y_{n+1} = \frac{R}{E} x_n + \left(y_1 - \frac{R}{E} x_0\right)\]
Number of ideal stages:
- Use graphical methods (equilibrium stages on x-y diagram)
- Similar approach to absorption/extraction
Ion Exchange
Exchange Capacity
Exchange capacity:
\[Q = \frac{mol_{exchanged}}{kg_{resin}}\]
- Q = exchange capacity (eq/kg or meq/g)
- Typically expressed as milliequivalents per gram
Breakthrough
Stoichiometric capacity:
\[V_s = \frac{Q \cdot W}{C_0}\]
- Vs = stoichiometric volume (L or gal)
- W = mass of resin (kg or lb)
- C₀ = influent concentration (eq/L or meq/mL)
Usable capacity:
\[V_b = V_s - V_{MTZ}/2\]
- Vb = volume at breakthrough
- VMTZ = volume of mass transfer zone
Evaporation
Single Effect Evaporation
Material balance:
\[F = L + V\]
\[F x_F = L x_L\]
- F = feed rate
- L = liquid (concentrate) rate
- V = vapor rate
- x = solute mass fraction
Energy balance:
\[F h_F + Q = L h_L + V H_V\]
- hF = specific enthalpy of feed
- hL = specific enthalpy of liquid product
- HV = specific enthalpy of vapor
- Q = heat input
Economy (steam economy):
\[Economy = \frac{V}{S}\]
- V = mass of water evaporated
- S = mass of steam used
Multiple Effect Evaporation
Overall economy:
\[Economy_{overall} = \frac{\sum V_i}{S_1}\]
- Vi = vapor from effect i
- S₁ = steam to first effect
- Economy increases approximately linearly with number of effects
Boiling point rise (BPR):
\[BPR = T_{solution} - T_{pure water}\]
- Due to concentration and hydrostatic head
- Dühring's rule: plots used to estimate BPR
Analogies Between Heat and Mass Transfer
Reynolds Analogy
\[\frac{k_c}{v} = \frac{h}{\rho c_p v}\]
\[Sh = Nu\]
- Valid for Pr = Sc = 1
- kc = mass transfer coefficient (m/s)
- v = velocity (m/s)
- h = heat transfer coefficient (W/m²·K)
Chilton-Colburn Analogy
\[j_D = j_H = \frac{f}{2}\]
\[j_D = \frac{Sh}{Re \cdot Sc^{1/3}} = St_D \cdot Sc^{2/3}\]
\[j_H = \frac{Nu}{Re \cdot Pr^{1/3}} = St \cdot Pr^{2/3}\]
- jD = Chilton-Colburn j-factor for mass transfer
- jH = Chilton-Colburn j-factor for heat transfer
- f = Fanning friction factor
- StD = Stanton number for mass transfer = kc/v
- St = Stanton number for heat transfer = h/(ρcpv)
- Valid for 0.6 < sc,="" pr=""><>
Lewis Number
\[Le = \frac{Sc}{Pr} = \frac{\alpha}{D_{AB}}\]
- Le = Lewis number
- α = thermal diffusivity (m²/s)
- For air-water, Le ≈ 1