This solution calculates the ratio between the molar flux of gas A during unidirectional diffusion through stagnant liquid B ($N_{A,UMD}$) and equimolar counter diffusion ($N_{A,EMD}$) in a binary gas-liquid system.
For equimolar counter diffusion (EMD), the molar flux of A ($N_{A,EMD}$) is proportional to the difference in mole fractions across the diffusion path. The formula is:
$ N_{A,EMD} = C_{total} D_{AB} \frac{(y_{A,bulk} - y_{A,interface})}{\delta} $
Where:
For unidirectional diffusion through stagnant B (UMD), where the molar flux of B ($N_B$) is zero, the molar flux of A ($N_{A,UMD}$) is given by:
$ N_{A,UMD} = \frac{C_{total} D_{AB}}{\delta} \ln\left(\frac{1-y_{A,interface}}{1-y_{A,bulk}}\right) $
The ratio $\frac{N_{A,UMD}}{N_{A,EMD}}$ is found by dividing the UMD flux by the EMD flux. Assuming $C_{total}$, $D_{AB}$, and $\delta$ are constant for both modes:
$ \frac{N_{A,UMD}}{N_{A,EMD}} = \frac{\frac{C_{total} D_{AB}}{\delta} \ln\left(\frac{1-y_{A,interface}}{1-y_{A,bulk}}\right)}{C_{total} D_{AB} \frac{(y_{A,bulk} - y_{A,interface})}{\delta}} $
This simplifies to:
$ \frac{N_{A,UMD}}{N_{A,EMD}} = \frac{\ln\left(\frac{1-y_{A,interface}}{1-y_{A,bulk}}\right)}{y_{A,bulk} - y_{A,interface}} $
The problem provides the following mole fractions:
Substitute these values into the ratio formula:
$ \frac{N_{A,UMD}}{N_{A,EMD}} = \frac{\ln\left(\frac{1 - 0.1}{1 - 0.2}\right)}{0.2 - 0.1} $
$ \frac{N_{A,UMD}}{N_{A,EMD}} = \frac{\ln\left(\frac{0.9}{0.8}\right)}{0.1} $
$ \frac{N_{A,UMD}}{N_{A,EMD}} = \frac{\ln(1.125)}{0.1} $
Calculate the natural logarithm:
$ \ln(1.125) \approx 0.117783 $
Now, compute the ratio:
$ \frac{N_{A,UMD}}{N_{A,EMD}} \approx \frac{0.117783}{0.1} \approx 1.17783 $
Rounding the result to two decimal places gives:
$ \frac{N_{A,UMD}}{N_{A,EMD}} \approx 1.18 $
Consider a non-reactive binary mixture of two ideal gases A and B in an isothermal horizontal closed tube. Due to the concentration difference at the two ends of the tube, equimolal counterdiffusion occurs along the axial direction. No concentration gradients exist in the radial direction. The profile for partial pressure of component A ($p_A$) as a function of axial distance $z$ is shown in the figure. The partial pressure of component B ($p_B$) approaches zero at $z = 0.8 \text{ m}$. At a location $z = z_1$ the partial pressures of the components A and B are equal. The value of $z_1$ (in m) is _____ (rounded off to two decimal places).
