Page 11 - Fundamentals of The Finite Element Method for Heat and Fluid Flow
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INTRODUCTION
                        defined as being one of forced convection. A mixed convection state is one in which both
                        natural and forced convections are present. Convection heat transfer also occurs in boiling
                        and condensation processes.                                             3
                           All bodies emit thermal radiation at all temperatures. This is the only mode that does
                        not require a material medium for heat transfer to occur. The nature of thermal radiation
                        is such that a propagation of energy, carried by electromagnetic waves, is emitted from the
                        surface of the body. When these electromagnetic waves strike other body surfaces, a part
                        is reflected, a part is transmitted and the remaining part is absorbed.
                           All modes of heat transfer are generally present in varying degrees in a real physical
                        problem. The important aspects in solving heat transfer problems are identifying the sig-
                        nificant modes and deciding whether the heat transferred by other modes can be neglected.



                        1.3 The Laws of Heat Transfer

                        It is important to quantify the amount of energy being transferred per unit time and for that
                        we require the use of rate equations.
                           For heat conduction, the rate equation is known as Fourier’s law, which is expressed
                        for one dimension as
                                                               dT
                                                       q x =−k                               (1.1)
                                                               dx
                                                                2
                        where q x is the heat flux in the x direction (W/m ); k is the thermal conductivity (W/mK,
                        a property of material, see Table 1.1)and dT/dx is the temperature gradient (K/m).
                           For convective heat transfer, the rate equation is given by Newton’s law of cooling as

                                                      q = h(T w − T a )                      (1.2)
                                                             2
                        where q is the convective heat flux; (W/m ); (T w − T a ) is the temperature difference
                                                                                              2
                        between the wall and the fluid and h is the convection heat transfer coefficient, (W/m K)
                        (film coefficient, see Table 1.2).
                           The convection heat transfer coefficient frequently appears as a boundary condition in
                        the solution of heat conduction through solids. We assume h to be known in many such
                        problems. In the analysis of thermal systems, one can again assume an appropriate h if not
                        available (e.g., heat exchangers, combustion chambers, etc.). However, if required, h can
                        be determined via suitable experiments, although this is a difficult option.
                           The maximum flux that can be emitted by radiation from a black surface is given by
                        the Stefan–Boltzmann Law,thatis,
                                                                4
                                                        q = σT w                             (1.3)
                                                         2
                        where q is the radiative heat flux, (W/m ); σ is the Stefan–Boltzmann constant (5.669 ×
                                      4
                                    2
                        10 −8 ), in W/m K and T w is the surface temperature, (K).
                           The heat flux emitted by a real surface is less than that of a black surface and is given by
                                                                4
                                                        q =  σT w                            (1.4)
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