Page 227 - Chemical engineering design
P. 227

10 7

                                                      e/d  0.05  0.04  0.03  0.02  0.015  0.01  0.008  0.006  0.004  0.002  0.001  0.0006  0.0002  0.0001  0.00001  0.000005  89  7
                                                                                                6
                                                                                                5  4
                                                Pipe roughness                                  3  2








                                                                                                10 6
                                                                                                89
                                                                                                7
                                                                                                6
                                                                                                5
                                                                                                4
                                                                                                3


                                                                                                2



                                                                                                10 5  m   roughness
                                                                                                9
                                                                                                8
                                                                                                7         relative
                                                                                                6
                                                                                                5   Reynolds number Re =  udr
                                ru 2  2                                                         4         and

                                L  d                                          Smooth pipes      3  2      number
                                 Equation 5.3, ∆p f  = 8f                                       9  8  7  10 4  Reynolds  versus












                                                                                                4  6  5   friction
                                                                                                          Pipe
                                                                                                3
                                                    zone
                                                                                                          5.7.
                                                     Critical
                                                                                                2
                                                                                                          Figure
                                                                                                10 3
                                                                                                9
                                                                                                8
                                                                                                7
                                                                                                6  5
                                                                Laminar flow                    4  3





                                                                                                2



                                                                                                10 2
                         0.1  0.09  0.08  0.07  0.06  0.05  0.04  0.03  0.02  0.015  0.01  0.0095  0.0090  0.0085  0.0080  0.0075  0.0070  0.0065  0.0060  0.0055  0.0050  0.0045  0.0040  0.0035  0.0030  0.00275  0.0025  0.00225  0.0020  0.00175  0.0015  0.00125  0.001  0.0009  0.0008  0.0007  0.0006  0.0005


                                                           f
   222   223   224   225   226   227   228   229   230   231   232