๐Ÿ”„ Mass Diffusion โ€” Fick's Law & Stagnant Film

Calculate binary molar and mass diffusion rates. Compare Equimolar Counter-Diffusion (Fick's law) with evaporation through a Stagnant Gas (Stefan's diffusion).

๐Ÿ”„ Film Diffusion Schematic & Profile Simulation

๐Ÿ“ Configuration

โš™๏ธ Diffusion Mode
๐ŸŒก๏ธ System Parameters
๐Ÿ“ Boundary Conditions (Solute A)
โš›๏ธ Species Data
Equations & Presets:

Quick Presets:
- Evaporation of water in stagnant air (25ยฐC)
- Helium and Nitrogen counter-diffusion

ECD Molar Flux:
$$N_A = \frac{D_{AB}}{R T L} (P_{A1} - P_{A2})$$
Stagnant B Molar Flux:
$$N_A = \frac{D_{AB} P}{R T L P_{B,lm}} (P_{A1} - P_{A2})$$

๐Ÿ“Š Results & Visualization

๐Ÿ“Š Calculation Output
โœ… Verified ๐Ÿ“ฅ Download

๐Ÿ“ˆ Molar Concentration Profile C_A(x)

๐Ÿ“ˆ Mole Fraction Profile y_A(x)

Molar Diffusion Flux (N_A) 5.9080e-3 mol/mยฒยทs Mass Flux (n_A): 2.3650e-2 g/mยฒยทs
Mass Transfer Coefficient (hm) 3.6000e-4 m/s Total Concentration: 41.57 mol/mยณ
Diffusion Path (L) 0.2000 m ECD Model
============================================================
      MASS DIFFUSION CALCULATION ENGINE
============================================================

  Calculation Mode         = Equimolar Counter-Diffusion
  Mode Code                =  1
  Temperature              =        20.00 deg-C
  Total Pressure           =       101.33 kPa
  Binary Diffusivity D_AB  =   7.2000E-05 m2/s
  Film Thickness (L)       =       0.2000 m
  Molecular Weight M_A     =         4.00 g/mol

--- BOUNDARY CONDITIONS -------------------------------------
  Boundary 1 Partial P_A1  =      60.0000 kPa
  Boundary 2 Partial P_A2  =      20.0000 kPa
  Boundary 1 Mole Frac yA1 =     0.592154
  Boundary 2 Mole Frac yA2 =     0.197385

--- ENGINE RESULTS ------------------------------------------
  Total Concentration C    =      41.5712 mol/m3
  Mass Transfer Coeff (hm) =     0.000360 m/s
  Molar Flux of A (N_A)    =   5.9080E-03 mol/m2.s
  Mass Flux of A (n_A)     =   2.3650E-02 g/m2.s

--- LOCAL PROFILE ALONG FILM --------------------------------
  x [m]       y_A [-]       C_A [mol/m3]  P_A [kPa]
  -----------------------------------------------------------
  0.0000      0.592154         24.6165       60.0000
  0.0050      0.582285         24.2063       59.0000
  0.0100      0.572415         23.7960       58.0000
  0.0150      0.562546         23.3857       57.0000
  0.0200      0.552677         22.9754       56.0000
  0.0250      0.542808         22.5652       55.0000
  0.0300      0.532939         22.1549       54.0000
  0.0350      0.523069         21.7446       53.0000
  0.0400      0.513200         21.3343       52.0000
  0.0450      0.503331         20.9241       51.0000
  0.0500      0.493462         20.5138       50.0000
  0.0550      0.483592         20.1035       49.0000
  0.0600      0.473723         19.6932       48.0000
  0.0650      0.463854         19.2830       47.0000
  0.0700      0.453985         18.8727       46.0000
  0.0750      0.444115         18.4624       45.0000
  0.0800      0.434246         18.0521       44.0000
  0.0850      0.424377         17.6419       43.0000
  0.0900      0.414508         17.2316       42.0000
  0.0950      0.404639         16.8213       41.0000
  0.1000      0.394769         16.4110       40.0000
  0.1050      0.384900         16.0008       39.0000
  0.1100      0.375031         15.5905       38.0000
  0.1150      0.365162         15.1802       37.0000
  0.1200      0.355292         14.7699       36.0000
  0.1250      0.345423         14.3597       35.0000
  0.1300      0.335554         13.9494       34.0000
  0.1350      0.325685         13.5391       33.0000
  0.1400      0.315815         13.1288       32.0000
  0.1450      0.305946         12.7186       31.0000
  0.1500      0.296077         12.3083       30.0000
  0.1550      0.286208         11.8980       29.0000
  0.1600      0.276339         11.4877       28.0000
  0.1650      0.266469         11.0774       27.0000
  0.1700      0.256600         10.6672       26.0000
  0.1750      0.246731         10.2569       25.0000
  0.1800      0.236862          9.8466       24.0000
  0.1850      0.226992          9.4363       23.0000
  0.1900      0.217123          9.0261       22.0000
  0.1950      0.207254          8.6158       21.0000
  0.2000      0.197385          8.2055       20.0000

--- CORRELATIONS USED ---------------------------------------
  Fick's First Law for Equimolar Counter-Diffusion (linear gradient).
  Total concentration computed from ideal gas equation of state.

๐Ÿ“˜ Calculation Methodology

Mathematical Model & Equations

For binary gas mixtures, Fick's first law defines the diffusion flux of A relative to the average velocity. For a stagnant gas ($N_B=0$), the bulk flow (advection) enhances the transport of A:

$$N_A = -D_{AB} C \frac{dy_A}{dx} + y_A(N_A + N_B)$$ $$N_A = \frac{D_{AB} C}{L} \ln\left(\frac{1 - y_{A2}}{1 - y_{A1}}\right) \quad (\text{for } N_B = 0)$$

Worked Engineering Example

Evaporation Preset:
A tube containing water at 25ยฐC ($T_f = 298.15\text{ K}$) evaporating into dry air ($P_{A2} = 0$). Water vapor pressure is $P_{A1} = 3.17\text{ kPa}$. Total pressure is $P = 101.3\text{ kPa}$. path length $L = 0.1\text{ m}$. $D_{AB} = 2.6 \times 10^{-5}\text{ m}^2/\text{s}$.

Solution:
1. Calculate boundary mole fractions:
$$y_{A1} = \frac{3.17}{101.3} = 0.0313, \quad y_{A2} = 0$$ 2. Calculate total molar concentration:
$$C = \frac{P}{RT} = \frac{101300}{8.314 \times 298.15} = 40.87\text{ mol/m}^3$$ 3. Evaluate stagnant log-mean pressure of air B:
$$P_{B1} = P - P_{A1} = 98.13\text{ kPa}, \quad P_{B2} = P - P_{A2} = 101.3\text{ kPa}$$ $$P_{B,lm} = \frac{101.3 - 98.13}{\ln(101.3/98.13)} = 99.71\text{ kPa}$$ 4. Compute molar flux $N_A$:
$$N_A = \frac{2.6 \times 10^{-5} \times 101.3}{8.314 \times 298.15 \times 0.1 \times 99.71} \times 3.17 \times 10^3 = 3.39 \times 10^{-4}\text{ mol/m}^2\text{s}$$

Standard Assumptions & References

Assumptions: Steady state, 1D diffusion along $x$-direction, ideal gas mixture behavior, and constant pressure and temperature across the film.

References:

  • Welty, J. R., Wicks, C. E., Wilson, R. E., & Rorrer, G. L. Fundamentals of Momentum, Heat, and Mass Transfer. Wiley.
  • Geankoplis, C. J. Transport Processes and Separation Process Principles. Prentice Hall.