Page 389 - Mechanical Engineers' Handbook (Volume 4)
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378   Cooling Electronic Equipment

                          Flow Resistance
                          The transfer of heat to a flowing gas or liquid that is not undergoing a phase change results
                          in an increase in the coolant temperature from an inlet temperature of T to an outlet tem-
                                                                                   in
                          perature of T , according to
                                    out
                                                  q   ˙mc (T out    T )  (W)                  (18)
                                                         p
                                                                in
                          Based on this relation, it is possible to define an effective flow resistance, R ,as
                                                                                      fl
                                                           1
                                                     R           (K/W)                        (19)
                                                      fl
                                                          mc  p
                                                          ˙
                          where m  is in kg/s.
                               ˙
           1.4  Radiative Heat Transfer
                          Unlike conduction and convection, radiative heat transfer between two surfaces or between
                          a surface and its surroundings is not linearly dependent on the temperature difference and
                          is expressed instead as
                                                            4
                                                                4
                                                   q    SF(T   T )   (W)                      (20)
                                                            1   2
                          where F includes the effects of surface properties and geometry and   is the Stefan–Boltzman
                                                      4
                                                   2
                          constant,     5.67   10  8  W/m  K . For modest temperature differences, this equation can
                          be linearized to the form
                                                   q   hS(T   T )    (W)                      (21)
                                                        r
                                                           1
                                                                2
                          where h is the effective ‘‘radiation’’ heat-transfer coefficient
                                r
                                                     2
                                                          2
                                                                           2
                                             h    F(T   T )(T   T )   (W/m  K)                (22a)
                                                     1
                                              r
                                                                 2
                                                             1
                                                          2
                          and, for small 
T   T   T , h is approximately equal to
                                           1    2  r
                                                h   4 F(TT ) 3/2   (W/m  K)                  (22b)
                                                                       2
                                                          1
                                                           2
                                                 r
                          It is of interest to note that for temperature differences of the order of 10 K, the radiative
                          heat-transfer coefficient, h , for an ideal (or ‘‘black’’) surface in an absorbing environment
                                              r
                          is approximately equal to the heat-transfer coefficient in natural convection of air.
                             Noting the form of Eq. (21), the radiation thermal resistance, analogous to the convective
                          resistance, is seen to equal
                                                           1
                                                     R          (K/W)                         (23)
                                                       r
                                                          hS
                                                           r
           1.5  Chip Module Thermal Resistances
                          Thermal Resistance Network
                          The expression of the governing heat-transfer relations in the form of thermal resistances
                          greatly simplifies the first-order thermal analysis of electronic systems. Following the estab-
                          lished rules for resistance networks, thermal resistances that occur sequentially along a ther-
                          mal path can be simply summed to establish the overall thermal resistance for that path. In
                          similar fashion, the reciprocal of the effective overall resistance of several parallel heat-
                          transfer paths can be found by summing the reciprocals of the individual resistances. In
                          refining the thermal design of an electronic system, prime attention should be devoted to
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