Page 55 - Mechanical Engineers' Handbook (Volume 4)
P. 55

44   Thermophysical Properties of Fluids

                          Table 27 (Continued)
                                                              Substance
                           T
                          (K)     CO      CO 2    H 2 O(g)  NO      NO 2     N 2      O 2     SO 2
                          2000   56740    91450    72690   57860    87260   56160    59200   91250
                          2100   60380    97500    77830   61530    92910   59760    62990   97080
                          2200   64020   103570    83040   65220    98580   63380    66800  102930
                          2300   67680   109670    88290   68910   104260   67010    70630  108790
                          2400   71350   115790    93600   72610   109950   70660    74490  114670
                          2500   75020   121930    98960   76320   115650   74320    78370  120560
                          2600   78710   128080   104370   80040   121360   77990    82270  126460
                          2700   82410   134260   109810   83760   127080   81660    86200  132380
                          2800   86120   140440   115290   87490   132800   85360    90140  138300
                          2900   89830   146650   120810   91230   138540   89050    94110  144240
                          3000   93540   152860   126360   94980   144270   92750    98100  150180
                          a
                          Converted and usually rounded off from JANAF Thermochemical Tables, NSRDS-NBS-37, 1971.
                          b To illustrate the term sensible enthalpy, which is the difference between the actual enthalpy and the enthalpy at the
                          reference temperature, 298.15 K (  25 C   77 F   537 R), the magnitude of the heat transfer, in kJ/kg mol fuel and
                          in kJ/kg fuel, will be calculated for the steady-state combustion of acetylene in excess oxygen, the reactants entering
                          at 298.15 K and the products leaving at 2000 K. All substances are in the gaseous phase.
                             The basic equation is
                                              Q   W    n ( h     h )
                                                                            si
                                                        i  ƒ   si   n ( h     h )
                                                                       ƒ
                                                                     i
                                                     P             R
                          where P signifies products and R reactants, s signifies sensible enthalpy, and the  h s are looked up in the table for the
                          appropriate temperatures.
                             If the actual reaction was
                                                  CH    11 ⁄2O → 2CO   HO   3O 2
                                                          2
                                                                2
                                                    2
                                                   2
                                                                   2
                          then W   0 and Q   2( 393,510   91,450)   1( 241,810   72,690)   3(0   59,200)   (226,740   0)    11 ⁄2(0
                          0)   604,120   ( 169,120)   177,600   226,740   822,380 kJ/mg mol. C 2 H 2   31,584 kJ/kg C 2 H 2 . Had the
                          fuel been burnt in air one would write the equation with an additional 3.76(5.5) N 2 on each side of the equation. In the
                          above, the enthalpy of formation of the stable elements at 298.15 K has been set equal to zero. For further information,
                          most undergraduate engineering thermodynamics texts may be consulted.
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