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Irreversible engines—Closed cycles                            91


                                         γ
                                      π  2 γ 1Þ  > PRÞ _ W max           (7.19)
                                       ð
                                              ð
                                                         ð        gives
              Multiplying both sides of the inequality (7.19) by PRÞ _ W max
                                           γ     h        i 2
                                        π 2 γ 1Þ
                                          ð
                                ð  PRÞ _ W max  > ð  PRÞ _ W max         (7.20)
              With the use of Eqs. (7.16) and (7.17), we conclude that

                                    ð  PRÞ _ Φ min  > PRÞ _ W net ¼0     (7.21)
                                              ð
              Because the optimum pressure ratio corresponding to the minimum entropy
              generation rate is greater than the pressure ratio at which the power output is
              zero, the operation of the engine at minimum entropy production would
              yield a negative power.




                   7.3 Otto cycle
                   In the Otto cycle, the heat addition and removal processes take place at
              constant volume. The rates of heat transferred to and rejected from the air
              are obtained as

                                                          γ 1

                     _                                 CR     1
                             ð
                     Q ¼ _mc v T 3  T 2 Þ ¼ _mc v T 1 T R  1             (7.22)
                      H                                   η
                                                           com
                                          h                         i
                  _                                      	      1 γ
                         ð
                 Q ¼ _mc v T 4  T 1 Þ ¼ _mc v T 1 T R  1 η T R 1 CR      (7.23)
                   L                                exp
              where CR¼V 1 /V 2 denotes the compression ratio and the temperature at
              states 2 and 4 are determined using the following equations.
                                                 γ 1   1

                                  T 2 ¼ T 1 1+  CR                       (7.24)
                                                 η
                                                  com
                                       h       	           i
                                T 4 ¼ T 3 1 η          1 γ               (7.25)
                                             exp  1 CR
              The net power production and the thermal efficiency of the cycle are
              obtained as follows.
                                                                γ 1

                   _     _     _         	      1 γ          CR
                  W net ¼ Q  Q ¼ _mc v T 1 1 CR      η T R               (7.26)
                          H     L                     exp      η
                                                                com
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