# Core Flow Distribution from Coupled Supercritical Water Reactor Analysis

Authors: Po Hu; Paul P. H. Wilson
Journal: Science and Technology of Nuclear Installations
 (2014)

---

## Abstract

This paper introduces an extended code package PARCS/RELAP5 to analyze steady state of SCWR US reference design. An 8 × 8 quarter core model in PARCS and a reactor core model in RELAP5 are used to study the core flow distribution under various steady state conditions. The possibility of moderator flow reversal is found in some hot moderator channels. Different moderator flow orifice strategies, both uniform across the core and nonuniform based on the power distribution, are explored with the goal of preventing the reversal.


---

## Body

## 1. Introduction

The supercritical water reactor (SCWR) is a next generation nuclear reactor concept. It is essentially a light water reactor (LWR) operating at higher pressure and temperature with a direct cycle. Its higher thermal efficiency and considerable plant simplification have distinguished it from the current reactors. Oka and his team presented both a thermal and fast SCWR design [1, 2], and Buongiorno presented a thermal SCWR as the US reference design [3], and Kim et al. and Xu et al. presented various mixed spectrum (thermal/fast) SCWR designs [4, 5].In the US reference SCWR design, the majority of the coolant firstly flows downward as a dedicated moderator in separated water rods and then flows upward adjacent to the fuel pins as coolant. Because of the large change in water density through the pseudocritical point, heat transfer between the coolant and the moderator has an important impact in accurate SCWR reactor analysis. This paper uses an extended code package, which couples the core simulator PARCS to the thermal-hydraulics simulator RELAP5, to analyze both steady state and transient of SCWR design. An 8 × 8 quarter core model in PARCS and a reactor core model in RELAP5 [6] are used to study the core flow distribution under various steady state conditions.


## 2. Analysis Methodology

### 2.1. Extended Code Package

PARCS is a 3D core simulator using the nodal method to solve diffusion equation. It is able to analyze PWR and BWR designs in which water is used as both coolant and moderator in a single flow channel. In this work, PARCS was modified to accommodate thermal-hydraulic feedback to the nuclear cross-sections of the separated coolant and moderator channels in SCWR. In addition, changes have been made to the communication between PARCS and RELAP5 to accommodate these separate flows [7].To enable the feedback from separated moderator, a new subroutine is added to look up macroscopic/homogenized cross-section information based on three thermal hydraulic properties: fuel temperature, coolant density, and moderator density. The homogenized cross-section data is prepared by the lattice transport code HELIOS [8].Coupled PARCS and RELAP5 use lookup files to share information between corresponding computational units (nodes for PARCS, hydrodynamic volumes, and heat structures for RELAP5). In the original lookup file, the nodes in PARCS correspond to the hydrodynamic volumes representing the single fluid and the heat structures representing fuel, cladding, and other core structure components in two separate tables. After the modification, there are three tables in the lookup file: one representing the coolant hydrodynamic volumes, one representing the moderator channel hydrodynamic volumes, and one representing the heat structures.


### 2.2. Core Models

An 8×8 quarter core model is used in PARCS, as show in Figure 1, with water reflectors at lateral boundaries and reflective boundary condition at top and bottom of the core. The fuel arrangement shown in Figure 1 is used in all the following calculations. These particular burnups were chosen to give an indication of the effect of burnup; a real equilibrium core loading would have larger burnups for partially used fuel. After considerations for symmetry, the 37 fuel assemblies in the PARCS model are coupled to 21 unique flow paths in the RELAP5 model. Both the PARCS and RELAP5 models have 12 axial nodes through the core. Flow paths in downcomer, moderator upper plenum, core, and lower plenum are modeled in RELAP5. A schematic of the flow path is shown in Figure 2; a moderator channel and a coolant channel represent one assembly in the core. In addition to being in contact with the fuel heat structure, the coolant channel is thermally coupled to the moderator channel through another heat structure representing the moderator channel wall. The majority of the inlet flow (90%) to the core flows up to the moderator upper plenum and then flows downward through moderator channels. Next, all the moderator flow mixes with the downcomer flow and finally flows upwards through coolant channels and the coolant upper plenum and to the outlet of vessel. The design parameters are shown in Table 1.Table 1
SCWR nominal design parameters (Buongiorno et al., 2003 [3]).
Fuel pin
Core
Fuel material
UO2
Thermal power
3575 MW
Fissile enrichment
5%
Number of fuel assemblies
148
Fuel radius
0.436 cm
Active height
4.27 m
Cladding material
Stainless steel
Effective diameter
3.93 m
Cladding thickness
0.063 cm
Volumetric power density
69 MW/m3
Fuel pitch
1.12 cm
Average linear heat rate
19.2 kW/m
P/D
1.12
Fuel assembly
Thermal-hydraulic parameters
Number of fuel rods
300
System pressure
25 MPa
Number of water rods
36
Coolant flow rate
1843 kg/s
Number of control rods
16
Moderator bypass,β
10% (184 kg/s)
Assembly pitch
28.6 cm
Inlet temperature
280°C
Water rod width
3.36 cm
Outlet temperature
500°C
Water rod wall thickness
0.04 cm
Thermal efficiency
44.80%Figure 1
Fuel assembly and quarter core assembly arrangement.Figure 2
Flow pattern in RELAP5.Previous research [9] showed that the heat transfer between the coolant and moderator channels could reduce the axial power peak by changing the equivalent moderator density, which represents combined moderation from moderator and coolant. These results were generated with a thermal hydraulic model inside PARCS assuming a fixed flow distribution in both moderator and coolant channels. This paper studies flow distributions in steady state using coupled PARCS/RELAP5. The possibility of moderator flow reversal is found in some hot moderator channels. Different moderator flow orifice strategies, both uniform across the core and nonuniform based on the power distribution, are explored with the goal of preventing the reversal.


## 2.1. Extended Code Package

PARCS is a 3D core simulator using the nodal method to solve diffusion equation. It is able to analyze PWR and BWR designs in which water is used as both coolant and moderator in a single flow channel. In this work, PARCS was modified to accommodate thermal-hydraulic feedback to the nuclear cross-sections of the separated coolant and moderator channels in SCWR. In addition, changes have been made to the communication between PARCS and RELAP5 to accommodate these separate flows [7].To enable the feedback from separated moderator, a new subroutine is added to look up macroscopic/homogenized cross-section information based on three thermal hydraulic properties: fuel temperature, coolant density, and moderator density. The homogenized cross-section data is prepared by the lattice transport code HELIOS [8].Coupled PARCS and RELAP5 use lookup files to share information between corresponding computational units (nodes for PARCS, hydrodynamic volumes, and heat structures for RELAP5). In the original lookup file, the nodes in PARCS correspond to the hydrodynamic volumes representing the single fluid and the heat structures representing fuel, cladding, and other core structure components in two separate tables. After the modification, there are three tables in the lookup file: one representing the coolant hydrodynamic volumes, one representing the moderator channel hydrodynamic volumes, and one representing the heat structures.


## 2.2. Core Models

An 8×8 quarter core model is used in PARCS, as show in Figure 1, with water reflectors at lateral boundaries and reflective boundary condition at top and bottom of the core. The fuel arrangement shown in Figure 1 is used in all the following calculations. These particular burnups were chosen to give an indication of the effect of burnup; a real equilibrium core loading would have larger burnups for partially used fuel. After considerations for symmetry, the 37 fuel assemblies in the PARCS model are coupled to 21 unique flow paths in the RELAP5 model. Both the PARCS and RELAP5 models have 12 axial nodes through the core. Flow paths in downcomer, moderator upper plenum, core, and lower plenum are modeled in RELAP5. A schematic of the flow path is shown in Figure 2; a moderator channel and a coolant channel represent one assembly in the core. In addition to being in contact with the fuel heat structure, the coolant channel is thermally coupled to the moderator channel through another heat structure representing the moderator channel wall. The majority of the inlet flow (90%) to the core flows up to the moderator upper plenum and then flows downward through moderator channels. Next, all the moderator flow mixes with the downcomer flow and finally flows upwards through coolant channels and the coolant upper plenum and to the outlet of vessel. The design parameters are shown in Table 1.Table 1
SCWR nominal design parameters (Buongiorno et al., 2003 [3]).
Fuel pin
Core
Fuel material
UO2
Thermal power
3575 MW
Fissile enrichment
5%
Number of fuel assemblies
148
Fuel radius
0.436 cm
Active height
4.27 m
Cladding material
Stainless steel
Effective diameter
3.93 m
Cladding thickness
0.063 cm
Volumetric power density
69 MW/m3
Fuel pitch
1.12 cm
Average linear heat rate
19.2 kW/m
P/D
1.12
Fuel assembly
Thermal-hydraulic parameters
Number of fuel rods
300
System pressure
25 MPa
Number of water rods
36
Coolant flow rate
1843 kg/s
Number of control rods
16
Moderator bypass,β
10% (184 kg/s)
Assembly pitch
28.6 cm
Inlet temperature
280°C
Water rod width
3.36 cm
Outlet temperature
500°C
Water rod wall thickness
0.04 cm
Thermal efficiency
44.80%Figure 1
Fuel assembly and quarter core assembly arrangement.Figure 2
Flow pattern in RELAP5.Previous research [9] showed that the heat transfer between the coolant and moderator channels could reduce the axial power peak by changing the equivalent moderator density, which represents combined moderation from moderator and coolant. These results were generated with a thermal hydraulic model inside PARCS assuming a fixed flow distribution in both moderator and coolant channels. This paper studies flow distributions in steady state using coupled PARCS/RELAP5. The possibility of moderator flow reversal is found in some hot moderator channels. Different moderator flow orifice strategies, both uniform across the core and nonuniform based on the power distribution, are explored with the goal of preventing the reversal.


## 3. Reference Case

The reference model uses a uniform orifice size for each moderator flow channel, with a ratio of the orifice area to the moderator area of 0.20. This results in flow reversal in some moderator channels as shown in Table2. Negative flow rates indicate a downward flow, as intended. These results show that two assemblies have reverse flow.Table 2
Moderator flow rate and assembly power in the reference case.
Flow rate (kg/s)
−15.6
−13.6
−15.2
−13.7
−15.7
−15.5
−17.1
Power (MW)
25.2
27.7
25.7
27.3
24.8
25.3
18.2
Flow rate (kg/s)
−13.6
−7.5
−13.1
3.6
−13.6
−13.7
−17.2
Power (MW)
27.7
26.8
27.8
24.8
27.4
27.4
16.1
Flow rate (kg/s)
−15.2
−13.1
−14.8
−12.9
−11.4
−16.5
Power (MW)
25.7
27.8
26.3
27.9
28.3
22.5
Flow rate (kg/s)
−13.7
3.6
−12.9
−10.4
−15.6
−17.2
Power (MW)
27.3
24.8
27.91
28.2
25.0
16.6
Flow rate (kg/s)
−15.7
−13.6
−11.4
−15.6
−17.1
Power (MW)
24.8
27.4
28.3
25.0
17.9
Flow rate (kg/s)
−15.5
−13.7
−16.5
−17.2
Power (MW)
25.3
27.4
22.5
16.6
Flow rate (kg/s)
−17.1
−17.2
Power (MW)
18.2
16.1


### 3.1. Pressure Balance in Moderator Channel

Due to buoyancy, the flow rate in hot moderator channels is lower than the flow rate in colder moderator channels. In most of moderator channels, a stable downward flow occurs as designated. In the highest power channels, due to the large density change through the pseudocritical point, the buoyancy effect is so large that the stable flow can be changed to flow upwards. This can result in a stable core flow distribution in which the flow in few moderator channels is upward while the flow in the rest of moderator channels is downward.A reactor core designed with downward moderator flow may not behave well when the flow reverses; as unexpected, reversed channels will have power peak at the bottom for both moderator and coolant that are flowing upwards and their densities are decreasing accordingly, and these peaks may be difficult to deal with during the depletion considering the control rods withdrawing from the top of the core, and the flow reversal may vanish over the cycle. Therefore, it is important to study the circumstances under which this reversal occurs. Furthermore, there are at least two ways to manage/prevent the moderator flow reversal. A thermal-hydraulics approach based on flow orifices in the moderator channels is discussed here. A neutronics approach based on using control rods, burnable absorbers, and axial fuel enrichment variance to change the power distribution will be studied in the future [10].As shown in Figure2, moderator enters the channel from the moderator upper plenum, flows downwards in the channel, and then exits to the lower plenum. The pressure balance through the moderator channel is dominated by three terms: the elevation pressure loss (gain in this case) and the entrance/exit pressure losses. The pressure balance can be written as follows:
(1)
∫
in
out
ρ
g
d
l
-
1
2
A


mod
⁡
2
K
m
˙
2
ρ
o
=
Δ
P
,
where Δ
P represents the pressure difference of upper and lower plenum for an individual channel. In RELAP5, the abrupt orifice friction lost coefficient is defined as [11]
(2)
K
=
(
A


mod
⁡
A
c
-
1
)
2
,
where A
c is the physical minimum flow area. It is defined as
(3)
A
c
=
0.62
A
o
+
0.38
A
o
4
A


mod
⁡
3
,
where A
o is cross-section of orifice and A


mod
⁡ is cross-section of moderator channel.Since the hot channel has a lower water density than the normal channel, the elevation pressure loss is lower. To balance (1), the flow rate in the hot channel has to decrease. However, by reducing the orifice size A
o, the increased loss coefficient K ((2) and (3)) suggests that a smaller change in mass flow rate is needed and the reversal can be prevented. While the neutronics may mitigate the effect because of the lower moderation due to lower density in the hot channel, a coupled analysis will be helpful to investigate the possibility of this reversal.In the following section, the results from three uniform orifice size cases are displayed followed by the results from one case with varied orifices corresponding to different assembly powers.


## 3.1. Pressure Balance in Moderator Channel

Due to buoyancy, the flow rate in hot moderator channels is lower than the flow rate in colder moderator channels. In most of moderator channels, a stable downward flow occurs as designated. In the highest power channels, due to the large density change through the pseudocritical point, the buoyancy effect is so large that the stable flow can be changed to flow upwards. This can result in a stable core flow distribution in which the flow in few moderator channels is upward while the flow in the rest of moderator channels is downward.A reactor core designed with downward moderator flow may not behave well when the flow reverses; as unexpected, reversed channels will have power peak at the bottom for both moderator and coolant that are flowing upwards and their densities are decreasing accordingly, and these peaks may be difficult to deal with during the depletion considering the control rods withdrawing from the top of the core, and the flow reversal may vanish over the cycle. Therefore, it is important to study the circumstances under which this reversal occurs. Furthermore, there are at least two ways to manage/prevent the moderator flow reversal. A thermal-hydraulics approach based on flow orifices in the moderator channels is discussed here. A neutronics approach based on using control rods, burnable absorbers, and axial fuel enrichment variance to change the power distribution will be studied in the future [10].As shown in Figure2, moderator enters the channel from the moderator upper plenum, flows downwards in the channel, and then exits to the lower plenum. The pressure balance through the moderator channel is dominated by three terms: the elevation pressure loss (gain in this case) and the entrance/exit pressure losses. The pressure balance can be written as follows:
(1)
∫
in
out
ρ
g
d
l
-
1
2
A


mod
⁡
2
K
m
˙
2
ρ
o
=
Δ
P
,
where Δ
P represents the pressure difference of upper and lower plenum for an individual channel. In RELAP5, the abrupt orifice friction lost coefficient is defined as [11]
(2)
K
=
(
A


mod
⁡
A
c
-
1
)
2
,
where A
c is the physical minimum flow area. It is defined as
(3)
A
c
=
0.62
A
o
+
0.38
A
o
4
A


mod
⁡
3
,
where A
o is cross-section of orifice and A


mod
⁡ is cross-section of moderator channel.Since the hot channel has a lower water density than the normal channel, the elevation pressure loss is lower. To balance (1), the flow rate in the hot channel has to decrease. However, by reducing the orifice size A
o, the increased loss coefficient K ((2) and (3)) suggests that a smaller change in mass flow rate is needed and the reversal can be prevented. While the neutronics may mitigate the effect because of the lower moderation due to lower density in the hot channel, a coupled analysis will be helpful to investigate the possibility of this reversal.In the following section, the results from three uniform orifice size cases are displayed followed by the results from one case with varied orifices corresponding to different assembly powers.


## 4. Results

### 4.1. Uniform Orifice Case

The results in Figures3 and 4 are generated at the beginning of cycle for three different uniform orifice sizes, indicated by the ratio of their area to the moderator channel area, r. The fuel arrangement is shown in Figure 1. There are no control rods or burnable absorbers used in this problem.Figure 3
Moderator flow rate, equivalent density, and normalized assembly power (reference value 24.59 MW) in different orifice area ratior
=
A
o
/
A


mod
⁡.Figure 4
Power, fuel temperature, moderator and coolant temperature, and equivalent density profiles in three assemblies for three orifice cases.Figure3 shows moderator flow rate, equivalent density, and total assembly power in each assembly of the quarter core. The equivalent density is defined as
(4)
ρ
eq
=
∑
i
=
1
12
(
ρ
cool
,
i
V
cool
,
i
+
ρ

mod
⁡


,
i
V

mod
⁡


,
i
)
∑
i
=
1
12
(
V
cool
,
i
+
V

mod
⁡


,
i
)
,
where the summation is over the 12 axial nodes, i. The results for r
=
0.20 are repeated here for comparison purposes and show the reversed flow in the moderator channels of two assemblies. As the area ratio is reduced to r
=
0.18, the flow reversal is avoided and downward flow occurs in all assemblies. The assembly power for those assemblies increases because the average equivalent density increases, improving the overall moderation. With further reduction in the orifice area, to r
=
0.15, even more of the moderator flow is distributed to the assemblies that previously showed reverse moderator flow. Although the equivalent density is still much lower than the other assemblies, these assemblies are now the highest power assemblies in the core.Figure4 shows the axial variations in the assembly power, coolant and moderator temperatures, and equivalent density for an assembly that experiences flow reversal (2D) and for an assembly that does not (2C). In the reference case, the power distribution is shifted towards the bottom of the core since the flow reversal reduces the moderation in the top of the core. Although the nonreversed assemblies do not experience any local reduction in the moderation (equivalent density), their power distribution is shifted down somewhat. The largest local power density in the core is found in the reversed channel even though it is not the highest power assembly in the reference case. By contrast, in the cases with flow reversal suppressed, r
=
0.18 and r
=
0.15, the axial power distribution is similar in all assemblies, including the highest power assemblies in which flow reversal occurred with r
=
0.20. One apparent benefit to the downward shifted power distribution is a reduction in cladding/fuel temperatures since the maximum power occurs at a location with lower coolant temperatures. However, the strong axial variation in power for the reversed channel could present other problems. In particular, as a result of nonuniform burnup, the flow reversal may vanish over the cycle as the axial power distribution in these channels responds.Based on the results of Figures3 and 4, it is possible to prevent the reversal by using uniform orifice area ratio, r
<
0.18, though from consideration of safety margin a lower value is preferred.


### 4.2. Nonuniform Orifice Case

In traditional PWR design, orifices are used to manage the distribution of coolant flow based on the power distribution. Following this example, this study developed an orifice pattern in which larger orifice sizes are applied to hot channels to deliver more flow and lower moderator temperatures to prevent reversal. This approach leads to larger orifice flow area ratios and lower overall pressure drops. The following results show comparison between a varied orifice case and a uniform orifice case without reversal(
r
=
0.15
).The variation of area ratior is chosen based on the expectation of higher assembly power for the most reactive (fresh) assemblies.Table 3 shows the r value of each assembly. The results of the varied r case are similar to those of r
=
0.15 case, although they show a slightly higher degree of power peaking among assemblies. Figure 5 shows the moderator flow rate, equivalent density, and assembly power across the quarter core of the two cases and Figure 6 compares the power and temperature profiles in corresponding channels. These results demonstrate that varied orifice sizes can prevent reversal with a larger orifice size that is required for the uniform orifice size solution.Table 3
Orifice arrangement.
0.2
0.2
0.2
0.2
0.2
0.2
0.2
0.2
0.25
0.2
0.25
0.2
0.225
0.2
0.2
0.2
0.2
0.2
0.225
0.2
0.2
0.25
0.2
0.225
0.2
0.2
0.2
0.2
0.225
0.2
0.2
0.2
0.225
0.2
0.2
0.2
0.2Figure 5
Moderator flow rate, equivalent density, and normalized assembly power (reference value 24.59 MW) in variedr case and r
=
0.15 case.Figure 6
Power, fuel temperature and moderator, and coolant temperature in hot channel in variedr case and r
=
0.15 case.


## 4.1. Uniform Orifice Case

The results in Figures3 and 4 are generated at the beginning of cycle for three different uniform orifice sizes, indicated by the ratio of their area to the moderator channel area, r. The fuel arrangement is shown in Figure 1. There are no control rods or burnable absorbers used in this problem.Figure 3
Moderator flow rate, equivalent density, and normalized assembly power (reference value 24.59 MW) in different orifice area ratior
=
A
o
/
A


mod
⁡.Figure 4
Power, fuel temperature, moderator and coolant temperature, and equivalent density profiles in three assemblies for three orifice cases.Figure3 shows moderator flow rate, equivalent density, and total assembly power in each assembly of the quarter core. The equivalent density is defined as
(4)
ρ
eq
=
∑
i
=
1
12
(
ρ
cool
,
i
V
cool
,
i
+
ρ

mod
⁡


,
i
V

mod
⁡


,
i
)
∑
i
=
1
12
(
V
cool
,
i
+
V

mod
⁡


,
i
)
,
where the summation is over the 12 axial nodes, i. The results for r
=
0.20 are repeated here for comparison purposes and show the reversed flow in the moderator channels of two assemblies. As the area ratio is reduced to r
=
0.18, the flow reversal is avoided and downward flow occurs in all assemblies. The assembly power for those assemblies increases because the average equivalent density increases, improving the overall moderation. With further reduction in the orifice area, to r
=
0.15, even more of the moderator flow is distributed to the assemblies that previously showed reverse moderator flow. Although the equivalent density is still much lower than the other assemblies, these assemblies are now the highest power assemblies in the core.Figure4 shows the axial variations in the assembly power, coolant and moderator temperatures, and equivalent density for an assembly that experiences flow reversal (2D) and for an assembly that does not (2C). In the reference case, the power distribution is shifted towards the bottom of the core since the flow reversal reduces the moderation in the top of the core. Although the nonreversed assemblies do not experience any local reduction in the moderation (equivalent density), their power distribution is shifted down somewhat. The largest local power density in the core is found in the reversed channel even though it is not the highest power assembly in the reference case. By contrast, in the cases with flow reversal suppressed, r
=
0.18 and r
=
0.15, the axial power distribution is similar in all assemblies, including the highest power assemblies in which flow reversal occurred with r
=
0.20. One apparent benefit to the downward shifted power distribution is a reduction in cladding/fuel temperatures since the maximum power occurs at a location with lower coolant temperatures. However, the strong axial variation in power for the reversed channel could present other problems. In particular, as a result of nonuniform burnup, the flow reversal may vanish over the cycle as the axial power distribution in these channels responds.Based on the results of Figures3 and 4, it is possible to prevent the reversal by using uniform orifice area ratio, r
<
0.18, though from consideration of safety margin a lower value is preferred.


## 4.2. Nonuniform Orifice Case

In traditional PWR design, orifices are used to manage the distribution of coolant flow based on the power distribution. Following this example, this study developed an orifice pattern in which larger orifice sizes are applied to hot channels to deliver more flow and lower moderator temperatures to prevent reversal. This approach leads to larger orifice flow area ratios and lower overall pressure drops. The following results show comparison between a varied orifice case and a uniform orifice case without reversal(
r
=
0.15
).The variation of area ratior is chosen based on the expectation of higher assembly power for the most reactive (fresh) assemblies.Table 3 shows the r value of each assembly. The results of the varied r case are similar to those of r
=
0.15 case, although they show a slightly higher degree of power peaking among assemblies. Figure 5 shows the moderator flow rate, equivalent density, and assembly power across the quarter core of the two cases and Figure 6 compares the power and temperature profiles in corresponding channels. These results demonstrate that varied orifice sizes can prevent reversal with a larger orifice size that is required for the uniform orifice size solution.Table 3
Orifice arrangement.
0.2
0.2
0.2
0.2
0.2
0.2
0.2
0.2
0.25
0.2
0.25
0.2
0.225
0.2
0.2
0.2
0.2
0.2
0.225
0.2
0.2
0.25
0.2
0.225
0.2
0.2
0.2
0.2
0.225
0.2
0.2
0.2
0.225
0.2
0.2
0.2
0.2Figure 5
Moderator flow rate, equivalent density, and normalized assembly power (reference value 24.59 MW) in variedr case and r
=
0.15 case.Figure 6
Power, fuel temperature and moderator, and coolant temperature in hot channel in variedr case and r
=
0.15 case.


## 5. Discussion

In the current US reference design, changing the orifice size can prevent flow reversal and manage axial power peaking at steady state condition. However, the assembly power peaking is large and may lead to detrimental hot spot effects. And furthermore, the reversal during depletion can be moderated by using control rods, burnable absorbers, and varying the fuel enrichment in the further analysis.Noticing that the density change across the supercritical point has a tendency to reverse the moderator flow, as in Oka’s original design, the water rods are insulated from the hot coolant of the fuel, which is surrounded by almost stagnant water which has an insulation cover around, to provide adequate moderation; the same kind of reversal should be avoided in such design. However, these insulated water rods are replaced with the similar water rods with US reference SCWR in his later designs [1, 10]. While in mixed spectrum reactor design, which separates the higher density/higher moderation water and lower density/moderation water to thermal and fast zones, this kind of reversal can be mitigated, though the reversal due to other effects still appeared during the accidents [5, 12].


## 6. Conclusion

A coupled code package, PARCS and RELAP5, is introduced to study the SCWR reactor core. Flow reversal in downward flowing moderator channels is found using the coupled codes. The reason of the reversal is the buoyancy and density change across the supercritical point. Using both uniform and nonuniform orifices in moderator channels to prevent the reversal is studied. Results showed that, with uniform orifices, orifice-moderator area ratio less than 0.18 is needed; with nonuniform orifice, higher area ratio can prevent the reversal.



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*Source: 178129-2014-05-15.xml*