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80                                           3 Basics of Gas Combustion

            where DU ¼ increase in the internal energy of the system (J), Q ¼ heat added to the
            system (J), and W ¼ work done by the system on the surroundings (J).
              Since combustion takes place in a relatively short period of time, it allows us to
            conduct a simplified analysis without complex integration, considering a combus-
            tion reaction starting with reactants at state 1 (pressure P 1 and temperature T 1 ).
            After a constant pressure combustion the products are at state 2 (P 2 ; T 2 ). The system
            is at constant pressure (P 1 ¼ P 2 ¼ P), therefore, work is done by the system on the
            surroundings, where W ¼ PðV 2   V 1 Þ. Applying first law of thermodynamics,

                                  U 2   U 1 ¼ Q   PðV 2   V 1 Þ          ð3:47Þ

            which leads to the heat produced by the combustion process as

                                                ð
                                    ð
                                Q ¼ U 2 þ PV 2 Þ   U 1 þ PV 1 Þ          ð3:48Þ
              Note that the enthalpy of a system at certain status is defined as
                                        H ¼ U þ PV                       ð3:49Þ

            where H = the total enthalpy of the system (J), U ¼ the internal energy of the
            system (J), and V ¼ the volume of the system.
              Therefore, the heat added to the system is the total enthalpy difference

                                       Q ¼ H 2   H 1                     ð3:50Þ

              The total enthalpy at status j ¼ 1 or 2 is the summarization of the enthalpy of all
            the compounds,

                                           X
                                      H j ¼   n i h i ðT j Þ             ð3:51Þ

              Then Eq. (3.50) becomes

                                    X           X
                                          ðÞ
                                Q ¼    n i h i T 2    n i h i T 1        ð3:52Þ
                                                      ðÞ
                                     P           R
            where n ¼ mole amount of the component in fuel–air mixture or the product,
            hðTÞ¼ enthalpy of a component at temperature T in J/mole. Subscripts i; P and R
            stand for the ith component, product, and reactant, respectively.
              The combustion system can be defined as exothermic, isothermal or endothermic
            based on the heat of reaction as follows:

                                8
                                  Q \ 0  exothermic reaction
                                <
                                  Q ¼ 0  isothermal reaction
                                :
                                  Q [ 0  endothermic reaction
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