Page 301 - Fundamentals of The Finite Element Method for Heat and Fluid Flow
P. 301

SOME EXAMPLES OF FLUID FLOW AND HEAT TRANSFER PROBLEMS
                              8
                                                   Row
                                                Re
                                                                                        Row
                                                                                    Re
                                               100 - Central
                                               100 - Lateral    8                   100 - Central  293
                                                                                    100 - Lateral
                              6                200 - Central    6                   200 - Central
                                               200 - Lateral                        200 - Lateral
                                               300 - Central                        300 - Central
                             Nu  4             300 - Lateral   Nu  4                300 - Lateral
                              2                                 2
                              0                                 0
                                  1st  2nd   3rd  4th  5th           1st  2nd  3rd  4th  5th
                                           Column                            Column
                                        (a) q = 0°, inline                (b) q = 10°, inline
                                               8
                                               6

                                                   Re
                                              Nu  4  100 - Central
                                                      Row
                                                   100 - Lateral
                                                   200 - Central
                                               2   200 - Lateral
                                                   300 - Central
                                                   300 - Lateral
                                               0
                                                    1st  2nd  3rd  4th  5th
                                                            Column
                                                         (c) q = 20°, inline
                        Figure 9.35 Forced convection heat transfer from spherical heat sources mounted on the
                        wall. Average Nusselt number distribution for in-line arrangement at different inclination
                        angles and Reynolds numbers


                        of Re. This information about the influence of the angle of attack can be very useful in this
                        type of application, in which the central part of the electronic device tends to be the hottest.
                           The average Nusselt number variation for different Reynolds numbers and flow angles
                        for the staggered arrangement of the solder balls is shown in Figure 9.36. In these figures,
                        the x-axis represents the column numbers of the ball clusters. For all legend details, refer
                        to Figure 9.34. The symbols used for the ‘central’ and the ‘lower’ rows are identical, as
                        the balls from these rows do not fall onto the same column. For example, the ‘central’ row
                        balls fall onto the columns with odd numbers but the ‘lower’ rows fall onto the columns
                        with even numbers.
                           As for the in-line arrangement, the average Nusselt number obtained is smaller for the
                        balls at the centre of the cluster. The front column, as expected, gives the highest heat
                        transfer rate. As the angle of attack of the incoming flow is increased, the participation
                        of the balls within the cluster increases, thus influencing the heat transfer. However, the
                        Nusselt numbers calculated are much smaller than that of the in-line arrangement for the
                        same Reynolds number and angle of attack.
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