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Question 13.9: Water is to be cooled from 328 to 293 K by means of a counte......

Water is to be cooled from 328 to 293 K by means of a countercurrent air stream entering at 293 K with a relative humidity of 20 per cent. The flow of air is 0.68 m³/m²s and the water throughput is 0.26 kg/m²s. The whole of the resistance to heat and mass transfer may be assumed to be in the gas phase and the product, (h_{D}a), may be taken as 0.2 (m/s)(m²/m³), that is 0.2 s^{-1}.

What is the required height of packing and the condition of the exit air stream?

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Assuming the latent heat of water at 273 K = 2495 kJ/kg
specific heat of air = 1.003 kJ/kg K
and specific heat of water vapour = 2.006 kJ/kg K

the enthalpy of the inlet air stream,
H_{G1} = 1.003(293 – 273) + \mathscr{H}[2495 + 2.006(293 – 273)]
From Figure 13.4:
at θ = 293 K and 20 per cent RH, \mathscr{H} = 0.003 kg/kg, and hence
H_{G1} = (1.003 x 20) + 0.003[2495 + (2.006 x 20)]
= 27.67 kJ/kg
In the inlet air, water vapour = 0.003 kg/kg dry air
or: \frac{(0.003/18)}{(1/29)} = 0.005 kmol/kmol dry air

Thus flow of dry air = (1 – 0.005)0.68 = 0.677 m³/m²s
Density of air at 293 K = \left({\frac{29}{22.4}}\right)\left({\frac{273}{293}}\right) = 1.206 kg/m³

and mass flow of dry air = (1.206 x 0.677) = 0.817 kg/m²s
Slope of operating line: (L^{\prime}C_{L}/G^{\prime})={\frac{(0.26\times4.18)}{0.817}} = 1.33

The coordinates of the bottom of the operating line are:
\theta _{L1} = 293 K, H_{G1} = 27.67 kJ/kg
Hence on an enthalpy-temperature diagram, the operating line of slope 1.33 is drawn through the point (293, 27.67) = (\theta _{L1}, H_{G1}).

The top point of the operating line is given by \theta _{L2} = 328 K, and H_{G2} is found to be 76.5 kJ/kg (Figure 13.19). From Figures 13.4 and 13.5 the curve representing the enthalpy of saturated air as a function of temperature is obtained and drawn in. Alternatively, this plot may be calculated from:

H_{F}=C_{a}(\theta_{f}-273)+\mathscr{H}_{0}[C_{w}(\theta_{f}-273)+\lambda]  kJ/kg

The curve represents the relation between enthalpy and temperature at the interface, that is H_{f} as a function of θ_{f}.
It now remains to evaluate the integral ∫ dH_{G}/(H_{f}H_{G}) between the limits, H_{G1} = 27.7 kJ/kg and H_{G2} = 76.5 kJ/kg. Various values of H_{G} between these limits are selected and the value of θ obtained from the operating line. At this value of \theta _{1}, now \theta _{f}, the corresponding value of H_{f} is obtained from the curve for saturated air. The working is as follows:

A plot of 1/(H_{f}H_{G}) and H_{G} is now made as shown in Figure 13.20 from which the area under the curve = 0.65. This value may be checked using the approximate solution of CAREY and WILLIAMSON^{(14)}.
At the bottom of the column:
H_{G1} = 27.7 kJ/kg, H_{f1} = 57.7 kJ/kg ∴ ΔH_{1} = 30 kJ/kg

At the top of the column:
H_{G2} = 76.5 kJ/kg, H_{f2} = 355 kJ/kg  ∴ ΔH_{2} = 279 kJ/kg
At the mean water temperature of 0.5(328 + 293) = 310.5 K:
H_{Gm} = 52 kJ/kg, H_{f} = 145 kJ/kg ∴ ΔH_{m} = 93 kJ/kg

\frac{\Delta H_{m}}{\Delta H_{1}}=3.10,\quad\frac{\Delta H_{m}}{\Delta H_{2}}=0.333,

and from Figure 13.16: f = 0.79

Thus: \frac{(H_{G2}-H_{G1})}{f\,\Delta H_{m}}=\frac{(76.5-27.7)}{(0.79\times93)}=0.66

which agrees well with the value (0.65) obtained by graphical integration.

Thus, in equation 13.53:

z=\int_{1}^{2}\,\mathrm{d}z=\frac{G^{\prime}}{h_{D}a\rho}\int_{1}^{2}\frac{\mathrm{d}H_{G}}{(H_{f}-H_{G})}                      (13.53)

height of packing, z = \int_{H_{G1}}^{H_{G2}}\frac{\mathrm{d}H_{G}}{\left(H_{f}-H_{G}\right)}\frac{G^{\prime}}{h_{D }a\rho}

= \frac{(0.65\times0.817)}{(0.2\times1.206)}

= \underline{\underline{2.20\ m}}

Assuming that the resistance to mass transfer lies entirely within the gas phase, the lines connecting \theta _{L} and \theta _{f} are parallel with the enthalpy axis.

In Figure 13.18 a plot of H_{G} and θ_{G} is obtained using the construction given in Section 13.6.4 and shown in Figure 13.15. From this curve, the value of θ_{G2} corresponding toH_{G2} = 76.5 kJ/kg is 300 K. From Figure 13.5, under these conditions, the exit air has a humidity of 0.019 kg/kg which from Figure 13.4 corresponds to a relative humidity of 83 per cent.

H_{G} θ = \theta _{f} H_{f} (H_{f}H_{G}) 1/(H_{f}H_{G})
27.7 293 57.7 30 0.0330
30 294.5 65 35 0.0285
40 302 98 58 0.0172
50 309 137 87 0.0114
60 316 190 130 0.0076
70 323 265 195 0.0051
76.5 328 355 279 0.0035
13.4
13.19
13.5
13.20
13.16
13.18
13.15

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