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112  FLOW OF  FLUIDS



                    EXAMPLE 6.12
                    Adiabatic and Isothermal Elow of a Gas m a Pipeline
                 Steam at the rate of 7000 kg/hr with an inlet pressure of 23.2 barabs   = 0.9997,
                 and temperature of 220°C flows in a line that  is 77.7mm dia and
                 305 m long. Viscosity is Z8.5(10-6)N sec/m2 and specific heat ratio is   0.9997(23.2)(10’)(0.7715)
                 k = 1.31. For  the  pipe,  E/D = 0.0006.  The  pressure  drop  will  be
                 found in (a) isothermal flow; (b) adiabatic flow. Also, (c) the line   = 17.89(1@) N/mz,
                 diameter for sonic flow will be found.                  AP=23.2-  17.89=5.31 bar.
                    Vl = 0.0862 m3/kg,                                  (c)  Line diameter for sonic flow. The critical pressure ratio is
                     G = 7000/(3600)(n/4)(0.0777)2 = 410.07 kg/mz sec,
                                                                                     = 0.5439,  with k = 1.31,
                    f  = 1.6364/[ln(O.l35)(0.0006) + 6.5/1.2(106)]2 = 0.0187.   G=---  7000/3600  2.4757
                    Inlet sonic velocity:                                   (n/4)D2 -  D2  ’
                                                                        M --_
                                                                            GV, - 2.4757(0.0862) - 3.909(W4)
                    us, = qm= q1(1.31)(8314)493.2/18.02 = 546 m/sec         Us,     5460’   -   D2   .
                    MI = ul/uSl = GV,/usl = 410.07(0.0862)/546 = 0.0647.
                                                                        Equation (6.89) becomes
                    As  a preliminary calculation, the pressure drop will be found
                 by neglecting any changes in density:                  o.5439(vz/v1) = 1 + 0.1183M:[1  - (V2/V1)”],   (3)
                                                                        fL/D = 0.0187(305)/0 = 5.7035/D            (4)
                                                                                        =rhs of Eq. (6.88).
                     ... P2 = 23.2 - 5.32 = 17.88 bar.               Procedure
                     (a)  Isothermal flow. Use Eq. (6.76):           1. Assume D.
                                                                     2.  Find Ml  [Eq. (2)].
                    2P V G2                                          3. Find Vz/Vl  from Eq. (6.89) [Eq. (3)].
                           =
                    11 2(23.2)(105)(0.0862)(410.07)2 = 6.726(1010),
                       gc                                            4.  Find rhs of Eq. (6.88) [Eq. (l)].
                                                                     5.  Find D = 5.7035/[rhs of  Eq. (6.88)] [Eq. (4)].
                                                                     6.  Continue until steps 1 and 5 agree.
                       = lo5  538.24 - 6.726                         Some trials are:
                                                                                          Eq. (6.89)   Eq. (6.88)
                       = 17.13(1@) N/mz,                                   D       nn,     414      rhS      D
                 and                                                      0.06    0.1086   0.5457   44.482   0.1282
                    AP = 23.2 - 17.13 = 5.07 bar.                         0.07    0.0798   0.5449   83.344   0.06843
                                                                          0.0697   0.08046   0.5449   81.908   0.06963
                 When the Iogarithmic term is neglected,
                    Pz = 17.07(10)5 N/m2.                               :.  D = 0.0697 m.
                    (b)  Adiabatic flow. Use Eq. (6.88):                lG1
                                                                        20
                                                                        36
                                                                        4r3
                    0.0187(305) -- 1     2                              50
                      0.0777  - 2.62 (Om3l m)                           60
                                      -k
                                                                        r9
                                                                        7
                                                                        89
                    73.4 = 182.47[ 1 -   + 0.8817 In( gr,               98
                                                                       160
                                                                       119
                    :.  5 = 0.7715.
                      v,
                    Equation (6.89)  for the pressure:

                                                                       148  01515  Xi
                                                                       150  RETURN
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