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104                                                       Chapters


           tl2,2 =  f(t2)                                             (3.2.17)
           h, = f(t 3')                                                (3.2.18)

           h 4 = f(t 4)                                                (3.2.19)
           Economic Relations

           t 4 - t wl' = 9.0 °F                                        (3.2.20)

           m 3' / m, = 2.09 Ibmol water/lbmol air                      (3.2.21)
           Variables

           Vi,i -  Yi,2 -  Y2,i -  Yz,2 - Yiw- in] - m 2 - rat - p lw  - p 2>is  - Ah vw - hj  - h 2 - h 3 - h 4 - h (il  - h 1]2 -
           h 2,i - h 2, 2 - t 2 - t 4
            Degrees of Freedom

           F = 21-21=0


           tions 3.2.15  and 3.2.17). Equations 3.2.18 and 3.2.19  give the  enthalpies  for pure
           water.
                Finally,  Table  3.2.1  contains  two  economic  relations  or  rules-of-thumb.
           Equation  3.2.20  states  that  the  approach  temperature  differences  for  the  water,
           which is the difference  between the exit water temperature and the  wet-bulb tem-
           perature of the inlet air, is 5.0 °C (9 °F). The wet-bulb temperature of the surround-
           ing  air  is  the  lowest  water  temperature  achievable by  evaporation.  Usually,  the
           approach  temperature  difference  is  between 4.0  and  8.0  °C.  The  smaller  the  ap-
           proach temperature difference,  the larger the cooling tower, and hence the more it
           will cost.  This increased tower cost must be balanced against the economic bene-
           fits  of colder water. These are: a reduction in the water flow rate for process cool-
           ing  and  in the  size  of heat exchangers for the plant because  of  an increase  in  the
           log-mean-temperature  driving  force.  The  other  rule-of-thumb,  Equation  3.2.21,
            states that the optimum mass ratio of the water-to-air flow rates is usually between
           0.75 to  1.5 for mechanical-draft towers [14].
                As  before,  prime  all  the  known  variables  in  the  equations  listed  in  Table
           3.2.1.  The table  shows that there  are twenty-one unknowns and  equations, result-
           ing in zero degrees of freedom.  Thus, we have completely defined the problem.
                 Before obtaining numerical answers, we must derive equations for the func-
           tional relationships expressed in Table 3.2.1, which are given in Table 3.2.2. Equa-
           tion 3.2.27 is the psychrometric relation, derived by Bird et al. (3.15). This relation







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