Page 52 - Mechanical Engineers Reference Book
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Heat transfer  1141
                                                    tion and convection can be added to enable the heat transfer
                                                    rate to be determined in terms of the two fluid temperatures.
                                                      For a plane  surface (Figure 1.63)



                                                    For a tubular surface (Figure 1.64)



                                                    It can be seen that the added resistances  may be inverted  to
                                                    give an overall conductance which is known as a 'U-value'  or
                                                    overall heat transfer coefficient.
     Figure 1.61  Conduction through a single-layer cylindrical surface   For a plane surface




                                                    For a tubular surface



                                                    The heat transfer  rate is then  simply written
                                                      For a plane surface
                                                    Q  = UA(Tf, - Tf2, where A  is the area


                                                                                  Boundary   Fluid
                                                                                    layer   2

                   14
     Figure 1.152  Conduction through a multi-layer cylindrical surface
                                                                                          Bulk
      vary considerably (Table 1.9). Although the determination  of                       temperature
      h  is  crucial  to  convection  calculations  it  is  an  extremely                 Tf2
      difficult process,  and  accurate  prediction  of  convective  heat
      transfer  is not always possible.
       If  we  express  the  convection  equation  in  a  thermal  res-
      istance ,form suitable for plane surfaces



      it can biz  seen that the thermal  resistance  is (lih) m'  K WA1.   Figure 1.63  U-value for a plane surface
      For tubular surfaces it is again more convenient to work  per
      unit length.  so that
                                                                  Fluid 1,  Tf,
                                                                  Boundary layer, h1
      and the thermal resistance is (1/25-rh) m K W-'             Double-layer tube
                                                                  Boundary layer, h2
      Table 1.9 Range of values of surface heat transfer
      coefficient (W rr2 K-')                                     Fluid 2, Ti2
      Free convection   Gases   0.5  to  500
                    Liquids   50  to  2000
      Forced  convection  Gases   10  to  700
                    Liquids  100  to  10 000                       L=-l_+z In (rOuter/rlnner)   1
                                                                                         2ar2hz
                                                                   U'   2nrlhl    2nk   +  A
      1.7.2.3  Overall heat transfer coefficients
      A common heat transfer situation is a solid wall separating two
      fluids. and for this problem the thermal resistances for conduc-   Figure 1.64  U-value for a cylindrical surface
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