Page 118 - APPLIED PROCESS DESIGN FOR CHEMICAL AND PETROCHEMICAL PLANTS, Volume 1, 3rd Edition
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102                       Applied Process Design for Chemical and Petrochemical  Plants

             Friction Drop for Flow of Vapors,  Gases, and Steam        q\ = rate of How,  cu fl/hr at standard conditions  (14. 7
             Figure 2-30                                                     psia and 60°F), SCFH.

             A.  The Darcy  rational relation  for compressible flow [3 J is:   1. When  calculated  Af>  total  <  10  percent  inlet  pres-
                                                                       sure, use p or V based on inlet or outlet conditions.
                           o. 000335 nv v                            2. When  calculated  LiP  total  >  10  percent inlet  pres-
                                     2
               �PI 100 rt  =  ------                      (2-77)
                                d 5                                    sure,  but< 40  percent,  use  average  p  or V based on
                                                                       inlet and outlet conditions.
                                              2
                           0.000001959f(q�  ) Sg                     3. When  calculated iiP  total,  P1  to  P2  is> 40%  of inlet
                                          2
             or,  �p I 100 ft=  ------------'--          (2-78)
                                    d"p                                pressure,  primarily for long lines,  use  the  following
                                                                       choices,  or break  the  line  into  segments  and calcu-
               The  general  procedures  outlined  previously  for han-
             dling  Iluids  involving  the  friction  factor,  f,  and  the  Re   late LiP for each as above.
             chart are used with the above relations.  This is applicable
             to  compressible  flow  systems  under the  following condi-   Also use Babcock formula given in another paragraph
             tions  [3].                                          for steam flow.

             where  Sg  =  specific gravity of gas relative to air  =  the ratio of   q'  h  =  24,700  [Yd /Sg]  (�P p 1/K)  12,  CFH @  14.7 psia
                                                                                  2
                                                                                               1
                       molecular weight of the gas to that of air.        and 60°F                              (2-79)
                                                                                                               w
                                                                                                              1600
                                         p  v
             AP/100 ft.  = 0.000 336  f  W2/d5p
                                                                                                              1000
                                            50                                                                800
                                            40                                                                600
                                                                                                               500
                                            30                                                                400
                                                                                                              300
                                                                                           d
                                            20                                                                 200
                                            15 2!
                                              s:                                                               100
                                              :::,
                                      0                                                                        80
                                      .....   10  1g_                                                          60  g
                                       0
                                       '-'
                                      :.0   9  -                                                               50  :::  �<>..
                                            8  gi
                                       :::,
                                      c...,                                                         f          40  �  �
                                       :;;   7�
                                       c,.   6   :.0                                                .05        30  �  '\;
                                              :::,
                                       "'     c...,                                                              :::,
                                      "C    5   ·=                                                  .04       20  &.   �
                                       c:
                                      s:    4  ·:;                                                               c::,   �
                                       :::,
                                              -c"
                                                                                                                 c::,
                                              ...
                                              ;::;:::                                               .03 �        c::,   �  -
                                                                                                                    ,,
                                              c:
                                              'ii:                                                    �       8  10  ·=  es
                                                                                                                 ':I:,"
                                                                                                                 ,S!  .....
                                                                                                      c
                                              �                                                       :c      6  .....  ...
                                                                                                      0
                                              0                                                     .OH�      5  0   �
                                              ....                                                    .....   4  .!!   �
                                                                                                      I
                                            1.s1                                                      ....    3  &l   �
                                              1i,                                                   .015         I   �
                                              u                                                                  :t:   <I
                                              ""
                                            1.0·2
                                            .9.,.�
                                            .8  I                                                   .01       1
                                            .7  c::,..                                                        .8
                                            .6
                                            .5                                                                .6
                                                                                                              .5
                                            .4                                                                .4
                                                                                                              .3
                                            .3
                                                                                                              .2
                                            .2
                                                                                                              .I
             Figure 2-30.  Pressure drop in compressible flow lines.  By permission, Crane Co., Technical Paper #410,  Engineering Div.  1957. Also see 1976
             edition.
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