Page 129 - APPLIED PROCESS DESIGN FOR CHEMICAL AND PETROCHEMICAL PLANTS, Volume 1, 3rd Edition
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Fluid Flow                                           115

                               Table 2-14                          For flow of gases and vapors through nozzles and orifices:
                     Typical Ratios of Specific Heats, k

                Compound                      k = qc,              q = YC’A          , cu ft/sec flow        (2-48)
                Air                              1.40
               Ammonia                           1.29
               Argon                             1.67           where  p = ratio of orifice throat diameter to inlet diameter
                Carbon Dioxide                   1.28                 C‘  = flow coefficient for nozzles and orifices (see Fig-
                Carbon Monoxide                  1.41                     ures 2-17 and 2-18), when used as per MME speci-
                Ethylene                         1.22                     fication for differential pressure
               Hydrochloric acid                 1.40                  p = fluid density, lb/cu  ft
               Hydrogen                          I .40                 A = cross-sectional flow area, sq ft
                Methane                          1.26
                Methyl Chloride                 1.20
               Nitrogen                         1.40             Note : fhe use of C’ eliminates the calculation of velocity of
                Oxygen                           1.40            approach. The flow coefficient C’ is C’ = C,/dmV
               Sulfur dioxide                   1.25             C  = discharge coefficient for orifices or nozzles [ 31.
                                                                   For compressible fluids flowing through nozzles and ori-
                                                                fices use Figures 2-17 and 2-18, using ht or AP as differen-
                                                                tial static head or pressure differential across taps located
                                                                one diameter upstream at 0.5 diameters downstream from
             Figures 2-38A and 2-38B are based on the perfect gas
           laws and for sonic conditions at the outlet end of a pipe.   the inlet face of orifice plate or nozzle, when values of C are
                                                                taken from Figures 2-17 and 2-18 [3]. For any fluid:
           For  gases/vapors  that  deviate from  these  laws,  such  as
           steam, the  same application will yj,eld about 5% greater
           flow rate. For improved accuracy, use the charts in Figures   q = C’A  ([2g (144) AP]/P)~’~, cu ft/sec flow   (2-48)
           2-38A and 2-38B to determine the downstream pressure
          when sonic velocity occurs. Then use the fluid properties   Note for liquids AP is upstream gauge pressure.
           at this condition of pressure and temperature in:       For  estimating  purposes  for  liquid  flow with  viscosity
                                                                similar to water through orifices and nozzles, the follow-
                                                                ing can be used  [53]:


                                                                   Q = 19.636C’dI2 &
           to determine the flow rate at this condition from:                        y’  - (21

             v = q/A  = 183.3 q/‘d2 = 0.0509 W/‘(dz) (P)   (2-91)
                                                                             d
                                                                                is
                                                                       where  2 greater than 0.3             (2- 92)
             d = internal diameter of pipe, in.                              di
             A= cross section of pipe, sq ft
             q = cu ft/sec  at flowing conditions
                                                                                           do  .
             T = temperature, R                                    Q = 19.636 C’d 02 fi where  -is   less than 0.3   (2-93)
             k = ratio of specific heats                                                   di
             P’ = pressure, psi ah
             W = flow, Ibs/hr                                    or  [3], W  = 157.6 dO2C’llh,p2
             v = velocity, mean or average, ft./sec                      = 1891 dO2C’&                       (2-94)

             These conditions are similar to flow through  orifices,   where   Q = liquid flow, gpm
          nozzles, and venturi tubes. Flow through nozzles and ven-    do = diameter of orifice or nozzle opening, in.
          turi devices is limited by the critical pressure ratio, r,  =   di = pipe inside diameter in which orifice or nozzle is
           downstream pressure/upstream  piressure at sonic condi-         installed, in.
           tions (see Figure 2-3SC)  ~                                hlL = differential head at orifice, ft liquid
                                                                       C’  = flow coefficient (see Figure 2-39 for water and
             For nozzles and venturi meters, the flow is limited by crit-   Figure 2-18 and 2-19 for vapors or liquids)
          ical pressure ratio and the minimum value of Y to be used.                            (text continued on page 118)
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