Page 125 - APPLIED PROCESS DESIGN FOR CHEMICAL AND PETROCHEMICAL PLANTS, Volume 1, 3rd Edition
P. 125

Fluid Flow                                           109

                                                    AVERAGE  PRESSURE -LB. PER SQ. IN. ABSOLUTE
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                                                                           ' .x
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                                                  -14i
                                                       -f.,\ 0
                                           -  "  1-,.l   \ ,-....  ,�  -   \  u I\ I\   so�  ..L  .,   .  '   �   �-   \  \  1   !00!
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                                                     l..l
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                                                   .....  \...
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                                                    -"\,   "l"""' \  1  �  ....  L_1  �   t-- u  \   \   {   \   =   ·-  �
                                                   \  1  \   II  � I   =    --,,     1   I   \  \    =  ICO  II>
                                                                                                       700
                                                 I  \   \  \      ,-.......1..   ,\  ;, M.�   --i  1   c
                                            -r-    t--   t--   t--   r-   r-    i---..   t--   '   r-   t--
                                             r--,   i---..   -i--  - ......   -i--.   ...........  - .......   .....  i--.   .... t--   .... t--
                                        1()-             ...... -   ...........                      ,___  40000
                                        l!O-   r-   r--.      t--..       r--.   -i---..   -t--   r-   t--
                                          -  -i--.   -r-..   t--..   1--...   ,-.....   ......   .......   -i-   't.....   -t.....   - _oooo
                                                                                     -
                                        40             -,-.....               -i-          .._
                                          -   -i--.-   t--..   !-....   t-...   r--.   t--..     t.....   �
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                                                                                                 t.....  .=-8000
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                                                                                     ,-.....
                                                                                .......
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                                                         t--
                                        16-  -t--   t--   --   .......   ..... t--   t--   ......   t--   t--   -  2000
                                        14-.:   r-   r-       ,-.....   t--..   t--   <,   t---..   t--   I--...   =--1000
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                                                         .......
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                     .5                      r---..   :--...   ......   .....   t--   1--...   COPYRIGHT-WALWORTH  COIINH'l'-1157  !§   -
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                                             0.   2!  s • q'°  �  ci   Of                            i
                                                     •  q  q
                                                         PRESSURE  LOSS  IN Le. PER SQ. INCH PER  100 FEET
                                      Based  on  Babcock  Formula:  P = 0.000131  (I+  d ;!}
                                                                           3 6)
                         Figure 2-32.  Steam flow chart.  (By permission, Walworth Co.  Note: use for estimating only (this author).)
              The maximum possible velocity of a compressible fluid      P'  =  pressure,  Psi  abs  (Psia)
           in a pipe is sonic  (speed of sound)  velocity,  as:         �·  =  sonic  or critical velocity of flow of a gas, ft/sec
                                                                        V  1  =  specific volume of fluid, cu ft/lb at T and P'
                           0.000001959f (q'h) 2Sg  2                     g  =  acceleration of gravity= 32.2 ft/per/sec
            or,  �p I  l 00 ft  =                        (2-  78)
                                   d''p                          Thus the maximum flow in a  pipe occurs when  the veloc-
                                                                 ity  at the  exit becomes sonic.  The sonic  location  may  be
           where    k  =  ratio of specific heat for gas or vapor al constant
                       pressure                                  other than the exit,  can be at restrictive points in the sys-
                   R  =  individual gas constant =  MR/M  =  1544/M   tem,  or at control/  safety relief valves.
                   M  =  molecular weight
                  MR  = universal  gas constant =  1544             Shock waves  travel  at supersonic velocities and exhibit
                   T  =  temperature of gas,  R,  =  ( 460 +  °F)   a  near  discontinuity  in  pressure,  density,  and  tempera-
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