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         Table 2 shows the details of boundary conditions for these calculations. The fan is installed to exhaust
         the heated air, and the temperatures on the deck and the side-hull surfaces are assumed to be 65' and
         42'  Celsius degree, respectively. These conditions are obtained from the rules to consider when a ship
         operates in tropical oceans. For the turbulent flow on the solid surfaces, wall function is used.

                                          TABLE 2
                         THE DESCRIPTION OF BOUNDARY CONDITIONS(SEE FIGURE 2)
                    Surface           Name                  Details
                      s1              Fan        Q+60  m3Min,
                      s2             Reefer      No-slip, Heat 5.23KW
                      s3            Side Hull    No-slip, T=42OC
                      s4              Deck       No-slip, T=65OC
                      s5              Air-In     No-slip, T=35'C
                     Others           Wall       No-Slip, T=35'C


         3  CALCULATEDRESULTS
         In order to understand the flow pattern inside the hold with a relatively low computational cost, the
         flow between a duct and a container column is simulated as shown in Figure. 3, like approaches for
         cascade foils. The capacity of a fan at the end of a duct is assumed to be half of the original fan, i.e.
         480 m3NlN. On the both surfaces in the lateral direction, symmetric boundary conditions is applied

         3.1 Cascade Approach for a Duct and u Contabter Column
         Figure 4 shows the flow and temperature distributions on the longitudinally cut-surfaces as determined
         in Figure 3. The calculated results around upper, middle, lower parts of the duct are plotted separately.
         The major drawbacks of the flow and temperature in the original system are summarized as follows:

          The suction flow does not reach the surface of reefer containers to generate the heat. As the result,
         the heated flow does not move into the duct.
          At the end of duct, the relatively cool air is inhaled.

                                          TABLE 3
                          THE SIZE OF THE ORIGINAL AND MODIFIED DUCT SYSTEM


                        Duct             Origid            Modified
                                     (1 2 Duct Column)   (6 Duct Column)
                 I  Width  XThickness  1   0.8m  X  0.6m   I   1.25m  X  1.Om  I
                     Hole Width           0.4m              1.2m
                     Hole Height          0.3m              0.3m

         From the results, we find that it is necessary to make the velocity at the hole increased and only heated
         air inhaled. However, the increase of fan capacity requires additional costs. Hence, the duct system is
         modified in following ways:
          To make the duct short, not to inhale the relatively cool air
          To adjust the hole size to make the suction flow velocity increase.
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