Page 37 - Fundamentals of The Finite Element Method for Heat and Fluid Flow
P. 37

SOME BASIC DISCRETE SYSTEMS
                        known). The solution of the remaining equations will give the temperature distribution
                        for both the fluids, that is, T 2 ,T 3 ,T 4 ,T 5 ,T 6 ,T 7 ,T 8 and T 9 for the incoming hot fluid and
                        T 11 ,T 12 ,T 13 ,T 14 ,T 15 ,T 16 ,T 17 and T 18 for the coolant.     29
                           With the calculated exit temperatures T 9 and T 18 , the effectiveness of the heat exchanger
                        can be calculated.
                        2.3 Transient Heat Transfer Problem (Propagation
                              Problem)


                        In a transient, or propagation, problem, the response of a system changes with time. The
                        same methodology used in the analysis of a steady state problem is employed here, but
                        the temperature and element equilibrium relations depend on time. The objective of the
                        transient analysis is to calculate the temperatures with respect to time.
                           Figure 2.8 shows an idealized case of a heat treatment chamber. A metallic part is
                        heated to an initial temperature, T p , and is placed in a heat treatment chamber in which an
                        inert gas such as nitrogen is present. Heat is transferred from the metallic part to the gas
                        by convection. The gas in turn loses heat to the enclosure wall by convection. The wall
                        also receives heat by radiation from the metallic part directly as the gas is assumed to be
                        transparent. The wall loses heat to the atmosphere by radiation and convection.
                           The unknown variables in the present analysis are the temperature of the metallic part
                        T p , the temperature of the gas T g , and the temperature of the enclosure wall T w .
                           For simplicity, we are using a lumped-parameter approach, that is, the temperature
                        variation within the metal, gas and wall is ignored.
                           Let c p , c g and c w be the heat capacities of the metallic part, the gas and the wall
                        respectively. The heat balance equations with respect to time can be derived as follows:
                           For the metallic part,
                                           dT p                         4    4
                                         c p  =− hA p (T p − T g ) +   p σA p (T − T )      (2.39)
                                                                        p
                                                                             w
                                           dt
                           For the gaseous part,
                                             dT g
                                           c g   = h p A p (T p − T g ) − h g A g (T g − T w )  (2.40)
                                              dt

                                                              Gas
                                                  Convection +       Convection +
                                    Wall, T w
                                                   radiation          radiation
                                  Gas, T g
                                 Metallic part    Metallic  Radiation       Convection +
                                    T p            part                 Wall  radiation  Atmosphere



                              Figure 2.8 Heat treatment chamber and associated heat transfer processes
   32   33   34   35   36   37   38   39   40   41   42