Page 102 - Thermal Hydraulics Aspects of Liquid Metal Cooled Nuclear Reactors
P. 102

76                    Thermal Hydraulics Aspects of Liquid Metal Cooled Nuclear Reactors

         each). The free surface of the water model is at atmospheric pressure. The facility is
         designated for a nominal water flow rate of 5.6 L/s. The maximum ΔT during the tests
         is 30°C. Based on these values, it is possible to simulate a Richardson number between
         0.01 and 1000 when performing physical water experiments (Fig. 3.1.13A). In natural
         convection, assuming a natural decay power of 5 MW in the real scale HLM reactor,
         the ratio of velocity between MYRRHA and MYRRHABELLE is estimated to a value
         of 3. The ratio of temperature is equal of 4, and the ratio of time scale is equal to 0.6.
            Fig. 3.1.12B shows a picture of the water model representing the upper plenum
         illuminated by a thin laser sheet. The heating elements used to simulate the heat source
         at the core level can be seen in the background, with the feeding electrical cables in
         zigzag leaving the model at the level of the free surface. The electrical cable is inside
         the Above Core Barrel (ACB). The different holes of the ACB can be identified in the
         figure. One copper heat exchanger is clearly visible in the frontal part of the picture.
         One the left side, we can distinguish partially the immersed pump.
            The Euler number is respected by measuring the overall pressure loss and by
         adding an obstruction at the level of the core to satisfy Euler similarity, taking into
         account the pressure losses of the heat exchangers and the core region. The flow
         through the bypass of the core can be controlled with a sliding gate.



         3.1.4.3 PIV measurements in MYRRHABELLE
         Fig. 3.1.14 shows a sketch of the PIV measurement section in MYRRHABELLE with
         the corresponding thermocouple positions. The thermocouple probes are positioned in
         each exits of the barrel cylinder and in the plenum, halfway between the barrel plate
         and the heat exchanger. A double pulse Nd:YAG laser is used to illuminate the desired
         test section from the top of the model while a double frame camera is used to record
         consecutive images of the PIV tracers.





              Richardson number as function of flow rate  Euler number as a function of bypass opening
             10                               190
                                 Q = 48 kW
                                              180
                                 Test 1
                                 Test 2       170                       Euler
           Richardson  1  0  1  2  3  4  5  6  7  8  9  Euler number  160
                                              150
                                              140
                                              130
                                              120
                                                 0     10   20    30   40
            0.1                                       Bypasss opening (%)
                     Total flow rate-liter/s
          (A)                               (B)
         Fig. 3.1.13 (A) Richardson number. (B) Core Euler number.
   97   98   99   100   101   102   103   104   105   106   107