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1/40  Mechanical engineering principles
         1.7  Heat transfer                            Single layer Plane surface

         1.7.1  Introduction
         Whenever  a temperature difference occurs there is an energy
         flow from the higher temperature to the lower. A study of heat
         transfer  is concerned  with  the  determination  of  the  instana-
         neous rates of energy flow in all situations. We determine heat
         transfer  rates in watts.  These rates  will  be constant  in situa-
         tions where the temperature difference  remains constant but
         variable  (transient)  when  the  temperature  difference  varies   I  k'z I
         either due to the  heat  transfers  or to other  energy  changes
         such as internal  chemical reaction.             x1    x2
          There are three modes of  heat transfer:
                                                       Figure 1.59  One-dimensional conduction through a single-layer
         1.  Conduction, which is  of  greatest  interest  in  solid bodies   plane wall
            but also occurs in fluids where it is often overshadowed by
            convection;
         2.   Convection, which occurs in fluids when  energy  is trans-   Multi layer plane surface
            ferred due to the motion of  the fluid:
         3.   Radiation, which occurs between two systems at different
            temperatures which need  not be in contact provided any
            intervening medium is transparent to the radiation.
          In practice,  all three modes occur simultaneously  and it is
         necessary to draw up a balance at a boundary.  For example,
         energy may be conducted to the surface of an electric storage
         heater and is then convected and radiated to the surroundings.
         Thus calculations can become complex, and in this particular
         case where  energy  is  added  at  certain  times  this is  a  conti-
         nuously varying situation.
          Three approaches  to heat transfer will be discussed below:   x3       x4
         1.  A simple method suitable for many estimations;   Figure 1.60  One-dimensional conduction through a multi-layer plane
         2.  A more detailed  appraisal of  the field;   wall
         3.  Comments on the use of  computers.

         1.7.2  Basic principles of heat transfer'"16   similar  way  to  electrical  resistances  so that  for  a multilayer
                                                        plane  surface  there  are  a  number  of  resistances  in  series
         1.7.2.1  Conduction                            (Figure 1.60). Thus we can write
         Fourier's  law for conduction states                         Ax
                                                        Q'  = (Tl - T4)/-&-
                dT
         @'= -k-
                dx                                      Cylindrical surfaces  For tubes it is more convenient to eva-
                                                        luate heat transfer rates per unit length, and integration gives
         The thermal conductivity  k(Wm-'K-l)  is  a  property  of  the
         material which varies with temperature but for small tempera-   Q' = (TI - T2)/- In r21rl = AT/- In r21rl
         ture ranges is usually considered constant.  Typical values are
         shown in Table 1.8. With constant k Fourier's equation can be   2nk12   2ak12
         integrated  for four common situations.        (see Figure  1.61), and in this case the thermal resistance  is
                                                               in
                                                                 m
                                                                   K
         Table 1.8                                      (2) w-1.
                                                        Q'  = (Tl - 7.d x(
         Substance         Thermal conductivity,  Wm-'  K-',  at 20" C   For a multilayer tube, thermal resistances  are added to give
         Aluminium         204                                          In  (ro"terlrln"er)
         Iron              52                                              2ak
         Facing brick       1.3                         (see Figure  1.62).
         Water              0.597
         Air                0.026  (100 kPa)            I. 7.2.2  Convection
         Glass wool         0.04
                                                        The fundamental  equation for  convective  heat  transfer  at a
                                                        solid-fluid  interface is
         Plane surfaces  Integration gives
                                                        where  0 is  the  temperature  difference  between  surface  and
                                                        fluid. The surface heat transfer  coefficient h (W m-'  K-')  is
                                                        not  a property  of  the fluid or the surface but depends on the
         (see Figure 1.59). The quantity (Axlk) is known as the thermal   flow pattern, the fluid properties md the surface shape. The
         resistance in m2 K W-l. Thermal resistances can be added in a   coefficient  has  to be  determined for  each situation  and can
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