Page 238 - Characterization and Properties of Petroleum Fractions - M.R. Riazi
P. 238

T1: IML
              P2: IML/FFX
                           QC: IML/FFX
  P1: IML/FFX
  AT029-05
                                           August 16, 2007
                                                          17:42
         218 CHARACTERIZATION AND PROPERTIES OF PETROLEUM FRACTIONS
                                      (0)
                    TABLE 5.9—Values of Z
                                                                      1.2
                                                                1
                                                                            1.5
                             0.1
                                           0.4
                                                                                          3
                                                  0.6
                                                                                   2
                                                        0.8
               0.01
                                                                                                 5
                                    0.2
         T r → AT029-Manual 0.05 AT029-Manual-v7.cls  for use in Eq. (5.107) from the Lee-Kesler modification of BWR EOS (Eq. 5.109) [58].  7  10
         0.30  0.0029  0.0145  0.0290  0.0579  0.1158  0.1737  0.2315  0.2892  0.3479  0.4335  0.5775  0.8648  1.4366  2.0048  2.8507
         0.35  0.0026  0.0130  0.0261  0.0522  0.1043  0.1564  0.2084  0.2604  0.3123  0.3901  0.5195  0.7775  1.2902  1.7987  2.5539
         0.40  0.0024  0.0119  0.0239  0.0477  0.0953  0.1429  0.1904  0.2379  0.2853  0.3563  0.4744  0.7095  1.1758  1.6373  2.3211 --`,```,`,``````,`,````,```,,-`-`,,`,,`,`,,`---
         0.45  0.0022  0.0110  0.0221  0.0442  0.0882  0.1322  0.1762  0.2200  0.2638  0.3294  0.4384  0.6551  1.0841  1.5077  2.1338
         0.50  0.0021  0.0103  0.0207  0.0413  0.0825  0.1236  0.1647  0.2056  0.2465  0.3077  0.4092  0.6110  1.0094  1.4017  1.9801
         0.55  0.9804  0.0098  0.0195  0.0390  0.0778  0.1166  0.1553  0.1939  0.2323  0.2899  0.3853  0.5747  0.9475  1.3137  1.8520
         0.60  0.9849  0.0093  0.0186  0.0371  0.0741  0.1109  0.1476  0.1842  0.2207  0.2753  0.3657  0.5446  0.8959  1.2398  1.7440
         0.65  0.9881  0.9377  0.0178  0.0356  0.0710  0.1063  0.1415  0.1765  0.2113  0.2634  0.3495  0.5197  0.8526  1.1773  1.6519
         0.70  0.9904  0.9504  0.8958  0.0344  0.0687  0.1027  0.1366  0.1703  0.2038  0.2538  0.3364  0.4991  0.8161  1.1341  1.5729
         0.75  0.9922  0.9598  0.9165  0.0336  0.0670  0.1001  0.1330  0.1656  0.1981  0.2464  0.3260  0.4823  0.7854  1.0787  1.5047
         0.80  0.9935  0.9669  0.9319  0.8539  0.0661  0.0985  0.1307  0.1626  0.1942  0.2411  0.3182  0.4690  0.7598  1.0400  1.4456
         0.85  0.9946  0.9725  0.9436  0.8810  0.0661  0.0983  0.1301  0.1614  0.1924  0.2382  0.3132  0.4591  0.7388  1.0071  1.3943
         0.90  0.9954  0.9768  0.9528  0.9015  0.7800  0.1006  0.1321  0.1630  0.1935  0.2383  0.3114  0.4527  0.7220  0.9793  1.3496
         0.93  0.9959  0.9790  0.9573  0.9115  0.8059  0.6635  0.1359  0.1664  0.1963  0.2405  0.3122  0.4507  0.7138  0.9648  1.3257
         0.95  0.9961  0.9803  0.9600  0.9174  0.8206  0.6967  0.1410  0.1705  0.1998  0.2432  0.3138  0.4501  0.7092  0.9561  1.3108
         0.97  0.9963  0.9815  0.9625  0.9227  0.8338  0.7240  0.5580  0.1779  0.2055  0.2474  0.3164  0.4504  0.7052  0.9480  1.2968
         0.98  0.9965  0.9821  0.9637  0.9253  0.8398  0.7360  0.5887  0.1844  0.2097  0.2503  0.3182  0.4508  0.7035  0.9442  1.2901
         0.99  0.9966  0.9826  0.9648  0.9277  0.8455  0.7471  0.6138  0.1959  0.2154  0.2538  0.3204  0.4514  0.7018  0.9406  1.2835
         1.00  0.9967  0.9832  0.9659  0.9300  0.8509  0.7574  0.6355  0.2901  0.2237  0.2583  0.3229  0.4522  0.7004  0.9372  1.2772
         1.01  0.9968  0.9837  0.9669  0.9322  0.8561  0.7671  0.6542  0.4648  0.2370  0.2640  0.3260  0.4533  0.6991  0.9339  1.2710
         1.02  0.9969  0.9842  0.9679  0.9343  0.8610  0.7761  0.6710  0.5146  0.2629  0.2715  0.3297  0.4547  0.6980  0.9307  1.2650
         1.05  0.9971  0.9855  0.9707  0.9401  0.8743  0.8002  0.7130  0.6026  0.4437  0.3131  0.3452  0.4604  0.6956  0.9222  1.2481
         1.10  0.9975  0.9874  0.9747  0.9485  0.8930  0.8323  0.7649  0.6880  0.5984  0.4580  0.3953  0.4770  0.6950  0.9110  1.2232
         1.15  0.9978  0.9891  0.9780  0.9554  0.9081  0.8576  0.8032  0.7443  0.6803  0.5798  0.4760  0.5042  0.6987  0.9033  1.2021
         1.20  0.9981  0.9904  0.9808  0.9611  0.9205  0.8779  0.8330  0.7858  0.7363  0.6605  0.5605  0.5425  0.7069  0.8990  1.1844
         1.30  0.9985  0.9926  0.9852  0.9702  0.9396  0.9083  0.8764  0.8438  0.8111  0.7624  0.6908  0.6344  0.7358  0.8998  1.1580
         1.40  0.9988  0.9942  0.9884  0.9768  0.9534  0.9298  0.9062  0.8827  0.8595  0.8256  0.7753  0.7202  0.7761  0.9112  1.1419
         1.50  0.9991  0.9954  0.9909  0.9818  0.9636  0.9456  0.9278  0.9103  0.8933  0.8689  0.8328  0.7887  0.8200  0.9297  1.1339
         1.60  0.9993  0.9964  0.9928  0.9856  0.9714  0.9575  0.9439  0.9308  0.9180  0.9000  0.8738  0.8410  0.8617  0.9518  1.1320
         1.70  0.9994  0.9971  0.9943  0.9886  0.9775  0.9667  0.9563  0.9463  0.9367  0.9234  0.9043  0.8809  0.8984  0.9745  1.1343
         1.80  0.9995  0.9977  0.9955  0.9910  0.9823  0.9739  0.9659  0.9583  0.9511  0.9413  0.9275  0.9118  0.9297  0.9961  1.1391
         1.90  0.9996  0.9982  0.9964  0.9929  0.9861  0.9796  0.9735  0.9678  0.9624  0.9552  0.9456  0.9359  0.9557  1.0157  1.1452
         2.00  0.9997  0.9986  0.9972  0.9944  0.9892  0.9842  0.9796  0.9754  0.9715  0.9664  0.9599  0.9550  0.9772  1.0328  1.1516
         2.20  0.9998  0.9992  0.9983  0.9967  0.9937  0.9910  0.9886  0.9865  0.9847  0.9826  0.9806  0.9827  1.0094  1.0600  1.1635
         2.40  0.9999  0.9996  0.9991  0.9983  0.9969  0.9957  0.9948  0.9941  0.9936  0.9935  0.9945  1.0011  1.0313  1.0793  1.1728
         2.60  1.0000  0.9998  0.9997  0.9994  0.9991  0.9990  0.9990  0.9993  0.9998  1.0010  1.0040  1.0137  1.0463  1.0926  1.1792
         2.80  1.0000  1.0000  1.0001  1.0002  1.0007  1.0013  1.0021  1.0031  1.0042  1.0063  1.0106  1.0223  1.0565  1.1016  1.1830
         3.00  1.0000  1.0002  1.0004  1.0008  1.0018  1.0030  1.0043  1.0057  1.0074  1.0101  1.0153  1.0284  1.0635  1.1075  1.1848
         3.50  1.0001  1.0004  1.0008  1.0017  1.0035  1.0055  1.0075  1.0097  1.0120  1.0156  1.0221  1.0368  1.0723  1.1138  1.1834
         4.00  1.0001  1.0005  1.0010  1.0021  1.0043  1.0066  1.0090  1.0115  1.0140  1.0179  1.0249  1.0401  1.0747  1.1136  1.1773
         where BP c /RT c can be estimated from Eq. (5.71) or (5.72)  These equations are equivalent to the following equations as
                                                              provided by the API-TDB [59].
         through T r and ω. Equation (5.114) may be used at low P r
         and V r > 2or T r > 0.686 + 0.439P r [60] instead of complex
         Eqs. (5.108)–(5.111). The API-TDB [59] also recommends
                                                               V ci = Z ci RT ci /P ci
         the following relation, proposed by Pitzer et al. [56], for
         calculation of Z for gases at P r ≤ 0.2.              Z ci = 0.2905 − 0.085ω i
                                                                         N          N         N
                                                                    1                   1/3       2/3
                    P r                              −1       V mc =      x i V ci + 3  x i V ci  x i V ci
             Z = 1 +   (0.1445 + 0.073ω) − (0.33 − 0.46ω)T r        4  i=1        i=1        i=1
                    T r
                                                                           N            N            N
                 − (0.1385 + 0.5ω)T −2  − (0.0121 + 0.097ω)T −3       1
                                r                   r                                       1/3          2/3
                                                               T mc =       x i V ci T ci + 3  x i V ci  T ci  x i V ci  T ci
        (5.114)  − 0.0073ωT −8                                      4V mc  i=1        i=1           i=1
                          r
                                                                     N

         Obviously neither Eq. (5.113) nor (5.114) can be applied to  ω m =  x i ω i
         liquids.                                                   i=1
          The LK corresponding states correlations expressed by  P mc = Z mc RT mc /V mc = (0.2905 − 0.085ω m )RT mc /V mc
         Eq. (5.107) and Tables 5.9–5.11 can also be applied to mix-
         tures. Such correlations are sensitive to the input data for  (5.115)
         the pseudocritical properties. The mixing rules used to cal-
         culate mixture critical temperature and pressure may greatly  where x i is the mole fraction of component i, N is the number
         affect calculated properties specially when the mixture con-  of compounds in the mixture, and T mc , P mc , and V mc are the
         tains dissimilar compounds. Lee and Kesler proposed special  mixture pseudocritical temperature, pressure, and volume re-
         set of equations for mixtures for use with their correlations.  spectively. ω m is the mixture acentric factor and it is calculated


   Copyright ASTM International
   Provided by IHS Markit under license with ASTM             Licensee=International Dealers Demo/2222333001, User=Anggiansah, Erick
   No reproduction or networking permitted without license from IHS  Not for Resale, 08/26/2021 21:56:35 MDT
   233   234   235   236   237   238   239   240   241   242   243