Page 236 - Thermal Hydraulics Aspects of Liquid Metal Cooled Nuclear Reactors
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Subchannel analysis for LMR                                       207


                                       cos 4θÞ
                                          ð
               HTC N ¼ 1                                                  (5.61)
                                         1:82            0:23
                                   P         0:24  λ clad
                         1+ 42:7 c    1     Pr
                                   D             λ coolant
           The coefficient c is 1.0 for interior subchannels and equal to 0.712 for edge and corner
           subchannels. For hexagonal rod bundles, the following correlation is given:

                                         ð
                                      cos 6θÞ
               HTC N ¼ 1                                                  (5.62)
                                  P        0:24  λ clad
                                       2:66            0:23
                         1 + 613:1   1    Pr
                                  D            λ coolant
           Here, HTC N stands for the ratio of the local HTC to the averaged HTC, that is,  HTC θðÞ .
                                                                           HTC
           According to Eqs. (5.61) and (5.62), the nonuniformity is stronger in case the Prandtl
           number of the coolant is larger, that is, the nonuniformity plays more important role in
           lead-cooled fast reactors (LFRs) than in SFRs.
              Fig. 5.14 shows the temperature distribution on fuel pin surface in a fuel assembly
           of the Ph  enix reactor. For this analysis, the Multichannel Analyzer for steady states
           and Transients in Rod Arrays (MATRA) code is applied, and one-twelfth of one fuel
           assembly is taken into consideration. Fig. 5.14A presents the division and numbering
           system of subchannels and fuel rods. The SCTH code gives the average coolant tem-
           perature 574°C at the fuel assembly exit. The temperature distribution obtained with
           Eq. (5.62) is also shown in Fig. 5.14 and indicated with “3-D model.” It is seen that the
           difference in temperature is about 4°C and relatively low, so that in the SFR design
           analysis, this nonuniformity is often neglected. However, it has to be pointed out that
           the nonuniformity in LFR could be several times larger than that in SFRs.

























           Fig. 5.14 Subchannel analysis of a Ph  enix fuel assembly. (A) Division of subchannels.
           (B) Temperature distribution.
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