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16.6 SIMULATION OF COMBUSTION IN SPARK-IGNITION ENGINES              367





                       Table 16.1 Specification of Engine Used for This Exercise
                       Engine swept volume                     1.6 L Engine
                       Nominal compression ratio               9.60
                       Engine speed                            3500.0 rev/min (58.333 rev/sec)
                       Molar fraction of residuals             0.050
                       Mixture strength                        1.000
                       (equivalence ratio)
                       Ignition angle                          692.0 Delay ¼ 1.0
                       Flame speed factor(actual/              4.000
                       laminar flame speed)

                       Data in bold have been changed during parameter study.



                                       Table 16.2 Compression Ratios
                                       Lower compression ratio     8.6
                                       Baseline compression ratio  9.6
                                       Higher compression ratio   10.6



               pressure. Also the higher compression ratio slightly increases the maximum temperature achieved in
               the burned and unburned zones, but actually reduces the release temperature (at exhaust valve opening
               (evo)).
                  This is because the peak temperature of the burned zone is reached earlier, and then the effective
               expansion ratio is bigger. The higher temperature and pressure at the end of the compression stroke also
               have an effect on the speed of the flame during the combustion. Hence, from these observations it can be


                                         120
                                                           Compression
                                         100               ratio
                                                           9.6
                                         80                10.6
                                     Pressure (bar)  60  40
                                                           8.6



                                             20


                                -50         0          50         100         150
                                                   Crankangle (deg atdc)
               FIGURE 16.12
               Variation of pressure with compression ratio.
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