1 Introduction
The conventional method of evaluating effective resonance cross-section is based on the equivalence theory, which turns the effect from moderator in heterogeneous models into the escape cross-section. Under equivalence theory, the background cross-section for heterogeneous models can be divided into two parts, one from the homogeneous medium, and another from the escape cross-section. Stamm’ler’s method [1, 2], which is an equivalence theory method built on Carlvik’s two-term rational approximation, is originally derived for the case of infinite lattice geometry, making use of first-flight collision probability and transmission probability. Another equivalent theory method, the Dancoff method, applies the Dancoff factor directly to the escape cross-section of an isolated fuel rod surrounded with infinite moderator. It is derived by using either Wigner’s one-term rational approximation or by taking the limit of infinite absorption. The Dancoff method is easier to apply in general as it involves only the calculation of Dancoff factor, while the Stamm’ler method is difficult to apply to cases of non-lattice geometry, though it is more accurate than the Dancoff method.
Sugimura Yamamoto [3] developed the neutron current method to calculate in a easy way the Dancoff factor for irregular assembly geometry, which requires only a fixed source transport calculation with "black” fuel rods.
In this paper we propose to rewrite the Stamm’ler equations so that the Dancoff factor appears there explicitly. The neutron current method can then be used to calculate the Dancoff factor for irregular assembly geometry and to apply it to the Stamm’ler equations. The method of characteristics [4] is applied to the fixed source transport calculation in the limit of black fuel rods.
When the multi-group cross-section library is generated, the resonance cross-section does not include the interference effect between different kinds of absorbers. In reality there are always multiple resonance nuclides, especially with burn-up of the fuel, the presence of the additional resonances will exaggerate the spectral flux dips and change the results in calculation. In common practice, the background cross-section iteration method [5, 6] is often used to correct the interference effects. But the iteration method is crude and not very effective.
In more recent methods of lattice calculation, the resonance interference effect among different resonance absorbers can be taken into account by resonance interference factors (RIFs) [7, 8], which are calculated and tabulated before evaluating the effective cross-section, and used as correction multipliers to the effective cross-section.
In the presented paper, a simplified evaluation of resonance interference factor table is done. For a typical reactor design, 238U dominants the number density of the resonance absorbers. So the interference effect between any two resonance absorbers other than 238U can be ignored for simplicity. The RIFs between 238U and another resonance nuclide are tabulated for different background cross-sections and different number density ratios.
The theoretical considerations are discussed in detail in Sect. 2, and verified in Sect. 3 for problems of infinite lattice geometry and single assembly geometry, with two or multiple resonance absorbers. The results for the case of infinite lattice geometry with only two resonance absorbers, for the case with multiple resonance absorbers, and for the case of single assembly geometry, are given.
2 Theory
The neutron slowing-down equation, the Stamm’ler method, and theYamamoto’s neutron current method are briefly reviewed and summarized in Sect. 2.1–2.3. In Sect. 2.4, we discusses how to apply Yamamoto’s Dancoff factor calculation to Stamm’ler method of resonance integral calculation. The simplified RIF table is discussed in Sect. 2.5. Finally Sect. 2.6 describes the overall calculation procedure for implementing the improvement.
2.1 Neutron slowing-down equation
For an isolated fuel rod, the neutron slowing-down equation is:
where, α=[(a -1)/(a+1)] 2, a is mass number of the nuclide; ∑t,f(E) is total cross-section in fuel region; ∑s,f(E) and ∑s,m(E) are scattering cross-section in fuel and moderator region, respectively; ϕf(E) and ϕm(E) are flux in fuel and moderator region, respectively; Pff(E) is first-flight collision probability in the fuel region; Pm0(E) is first-flight escape probability in the moderator region; Vf is volume of fuel region and Vm is volume of moderator region.
In moderator region, assuming that the 1/E spectrum is suitable and ∑s,f(E) is constant in the integral, the second term on the right part in Eq. (1) can be simplified. And assuming that the absorption cross-section in moderator is negligible, then total cross-section is equal to the scattering cross-section. Substituting the reciprocity relationship of Eq. (2) into Eq. (1) and using some approximation, the neutron spectrum can be solved as Eq. (3).
where λ is the Goldstein-Cohen factor, with λ =1, λ =0 and 0<λ <1 being the narrow, wide and intermediate resonance approximation, respectively.
If the Pff(E) in isolated fuel rod is replaced with the first-flight collision probability in a lattice model, PFF(E), the neutron spectrum in the lattice model can be written as:
2.2 Stamm’ler’s method for evaluating the effective cross-section
In an infinite lattice system, according to Stamm’ler’s method, the PFF(E) and Pff(E) can be correlated as:
where,
The expression of Pff in Carlvik’s two-term rational approximation is as follows:
Substituting Eq. (6) into Eq. (5), we have the expression of PFF with two-term rational approximation:
where, α1,2 = (5A+6) (A2 +36A +36)/[2(A+1)], β1=[(4A +6)/(A+1) - α1]/(α2 - α1), and β2= 1 -β1.
Substituting Eq. (7) into Eq. (4), and assuming that (1 -λ)s,F is far smaller than t,F, we have:
Equation (9) defines effective cross-section of a single resonance nuclide in group g. Substitute Eq. (8) into Eq. (9) and assumeing λ rs,f(E) is far smaller than α,f(E), too, the effective cross-section can be defined by Eq. (10):
where, RIn,x = βnFx(bn), bn = λσp.f +αnσe,
In Eq. (10), Δu is usually adjusted to unity by the library. The resonance integral Fx(bn) will be determined by the interpolation in the resonance integral table which will be supplied by the nuclear data library. Therefore, to evaluate the effective cross-section, parameter A in Stamm’ler’s method is calculated in advance. In the original Stamm’ler derivation, A is a characteristic constant for a given infinite lattice problem and is evaluated by using collision probability method. Instead of using the collision probability method to calculate A, we will relate A to Dancoff factor and then use Yamamoto’s neutron current method to calculate the Dancoff factor in a simple way, which is valid even for the non-lattice assembly geometry.
2.3 The neutron current method for calculating Dancoff factor
According to Eq. (4), the total reaction rate can be written as:
Taking the black-limit of very large total cross-section, the limit of Eq. (11) can be expressed as:
In the black-limit Wigner’s one-term rational approximation to PFF is valid:
Substituting Eq. (12) into Eq. (13), we have:
If the total cross-section is large enough, the total reaction rate is very close to Eq. (14). So when the total reaction rate in the resonance region is obtained by Yamamoto’s fixed source transport calculation in the limit of large total cross-section, the Dancoff factor can be calculated by:
In using the Dancoff method for effective resonance cross-section calculation, the Dancoff factor from Eq. (15) is applied directly to the equivalent escape cross-section of an isolated rod to calculate the background cross-section for resonance integral table lookup. Instead, we propose to apply the Dancoff factor from Eq. (15) to the Stamm’ler method equations.
2.4 Application of Dancoff factor to Stamm’ler method
An alternative equivalent definition of Dancoff factor is given as [2, 3]:
Also note that the first flight collision probability satisfies the following relation:
Substituting Eqs. (5) and (17) into Eq. (16), the relationship between the Dancoff factor and the parameter A in Stamm’ler method is obtained:
Therefore the neutron current method can be used to calculate D and thus obtain A without having to use the collision probabilities in Eq. (5). Furthermore the neutron current method is applicable to the general non-lattice assembly geometry. Once A is known, the two-term coefficients in Eq. (7) can be calculated. The Stamm’ler method can then be used without any change to calculate the effective cross-section by Eq. (10).
2.5 Simplification of the resonance interference factor table
Traditionally the background cross-section iteration method is used for the resonance interference correction, but the iteration method is not yet effective. A method using simplified resonance interference factor (RIF) table is given below.
In a typical LWR core, the number density of 238U is usually much larger than that of other resonance nuclides. The spectrum in the resonance region is dominated by resonance absorption from 238U. To simplify the resonance interference treatment, only the interference effects between 238U and other resonance nuclides are considered. To correct the resonance overlap (interference) effects, the resonance interference factors (RIFs) prepared with Eq. (19) are used.
where,
Corresponding to the overlap effects from 238U to other resonance nuclides, the interference effects from other resonance nuclides to 238U at the same number density ratio (Ni/N238) are calculated by Eq. (20):
Taking 238U as an example, the whole process of evaluating a resonance interference factor is described below.
For
The number density of 238U will be set to unity for convenience. To get different background cross-sections, we just need to adjust the number density of Hydrogen.
For
where, b,238 and
When the effective cross-sections with and without the interference effect is obtained, RIF from resonance nuclide i to 238U is calculated by Eq. (20). For a typical lattice, the flux spectrum varies with the background cross-section, caused by different number densities of 238U or different shielding conditions. So, a series of calculations with different background cross-sections and different number density ratios are carried out.
For resonance nuclides other than 238U, the effective cross-section for a specific resonance nuclide without the resonance interference correction is calculated by interpolating the nuclear data library, before interpolating the RIFs table to obtain RIF. Finally the RIF is multiplied to the uncorrected effective cross-section as:
where,
For 238U, the resonance interference effects from other resonance nuclides to 238U are counted into the correction as:
where
2.6 Calculation procedure
The calculation procedures for implementing the improvement are described as follows.
i) Prepare table of RIFs as described in Sect. 2.5.
ii) Perform fixed source transport calculation for each resonance group. The macroscopic total cross-section in resonance region is set to 100000 (or any number that is large enough), and set to λp for regions without resonance nuclide. The neutron source is set to λp for all regions. The transport equation, Eq. (25), is solved with the MOC (Method of Characteristics):
where ∑t,g=105 in resonance region, and t,g= λp,g in non-resonance region. With the solution for the fixed source transport solution, the total reaction rate for each resonance region is calculated.
iii) Dancoff factor for each resonance region in each resonance group is calculated through Eq. (15). And parameter A is calculated through Eq. (18).
iv) In resonance regions and for resonance nuclides, calculate the effective cross-section through Eq. (10).
v) For resonance nuclide other than 238U the effective cross-section is corrected by Eq. (23). For 238U, the effective cross-section is corrected by Eq. (24).
3 Verification results
Numerical verifications were carried out for cases in lattice geometry, cases with two absorbers in the resonance region, and cases with multiple absorbers in the resonance region. To assess the effect coming separately from the Dancoff factor or the RIF, two calculations were performed for each case problem. As shown in Table 1,
Methods | Stamm’ler’s method | Improved use of Dancoff factors | Treatment of resonance interference | |
---|---|---|---|---|
Iteration | RIFs | |||
A | √ | √ | ||
B | √ | √ | ||
C | √ | √ |
Method A used the background cross-section iteration for resonance interference and Method B used the RIF table for resonance interference. Both methods used improved Dancoff factor in Stamm’ler equations. Method C used the traditional Stamm’ler’s method with the background cross-section iteration for resonance interference as a contrast. Together with verification for the case of non-lattice single assembly geometry, all calculations used the 69-groups WIMS-D format micro library. For all the cases, continuous energy Monte Carlo calculation [10] was taken as the reference solution. Both the 69-group micro nuclear data library and the continuous energy nuclear data library were used in all calculations and verifications were developed from the basic library: ENDF/B-VII.0. Errors of eigenvalue in the verification results are all expressed in pcm, defined as (x- reference)× 105, where x is given by the tested method.
3.1 Infinite lattice cases
An infinite lattice of hexagonal fuel cells, as shown in Fig. 1, was used in the lattice calculation. Each side of the hexagonal cell is 7.83 mm. In the cell, the fuel rod is of 7.862-mm diameter, the clad made of Zr-Nat is 0.649 mm thick, and the moderator is light water at 300 K in both resonance and non-resonance regions.
-201602/1001-8042-27-02-010/alternativeImage/1001-8042-27-02-010-F001.jpg)
3.1.1 Infinite lattice case with two resonance absorbers
Let the fuel rod contain only UO2, with 235U enrichment of 0.8%–3.6% in steps of 0.2%. Figure 2 shows errors of the eigenvalue as function of the 235U enrichment. One sees that Method A differs little from Method C. This indicates that our goal to find an alternative way to use Stamm’ler equations without possibility calculation is achieved. As Methods A and C have almost the same result, the following discussions will focus on Methods A and B.
-201602/1001-8042-27-02-010/alternativeImage/1001-8042-27-02-010-F002.jpg)
There is a significant improvement in eigenvalue for Method B over Method A. This shows that the RIF table works much better than the background cross-section iteration in capturing resonance interference. The error of using Method B is around 100 pcm, which is quite acceptable in practice.
The verification results of 1.8% enrichment, as a typical case named as Case-A for the convenience of discussion, are given in Table 2. Table 3 shows the nuclide composition in Case-A. The reference eigenvalue at 1.8% enrichment is 1.22667± 0.00009 and the errors to the reference eigenvalue are -290 and -115 pcm (Fig. 2), for Methods A and B, respectively. From the microscopic cross-section for absorption and neutron production by each resonance nuclide (Table 2), one sees that the interference effect is mostly on 235U, not on 238U, as the Method B results are almost the same as the Method A results for 238U. This is expected because of the large 238U number density versus the much smaller number density of 235U.
Energy groups | Absorption of 235U | Neutron production of 235U | Absorption of 238U | ||||||
---|---|---|---|---|---|---|---|---|---|
∑a | δ (%)b | ∑a | δ (%)b | ∑a | δ (%)b | ||||
Method A | Method B | Method A | Method B | Method A | Method B | ||||
15 | 4.4904 | 0.02 | 0.02 | 7.9300 | 0.05 | 0.04 | 0.69442 | -0.19 | -0.17 |
16 | 5.6824 | -0.12 | -0.10 | 10.420 | -0.12 | -0.09 | 0.73277 | -0.81 | -0.78 |
17 | 6.9880 | -0.23 | -0.17 | 12.586 | -0.22 | -0.22 | 0.94726 | -1.65 | -1.60 |
18 | 9.5619 | -0.04 | 0.17 | 14.984 | -0.34 | 0.11 | 0.87767 | -1.62 | -1.56 |
19 | 12.184 | -0.69 | -0.11 | 19.408 | -1.07 | -0.08 | 1.1712 | -1.75 | -1.71 |
20 | 16.946 | -0.2 | 0.25 | 28.906 | -0.13 | 0.43 | 1.3449 | -2.29 | -2.26 |
21 | 27.897 | -0.36 | -1.07 | 45.743 | -1.06 | -0.76 | 1.5361 | -0.03 | 0.05 |
22 | 34.768 | -0.37 | -0.18 | 53.527 | -0.12 | -0.51 | 2.4168 | 0.06 | 0.08 |
23 | 58.251 | -2.36 | 0.55 | 99.149 | -2.75 | 0.58 | 2.1192 | -0.71 | 0.12 |
24 | 69.201 | -3.37 | -0.01 | 102.82 | -2.80 | -0.05 | 4.6044 | 2.25 | 2.27 |
25 | 74.991 | 6.58 | -1.15 | 114.81 | 2.23 | -0.56 | 6.2095 | 0.40 | 0.36 |
26 | 74.892 | -1.03 | -0.73 | 88.854 | -0.75 | -0.53 | 0.47409 | -0.54 | -0.27 |
27 | 67.381 | -1.04 | -1.46 | 98.015 | -8.06 | 0.25 | 7.8266 | 0.79 | 0.42 |
Materials | Fuel rod | Clad | Moderator | |||
---|---|---|---|---|---|---|
235U | 238U | 16O | Zr-Nat | H | 16O | |
Number density (1024/cm3) | 4.21236E-04 | 2.26905E-02 | 4.62234E-02 | 3.89087E-02 | 4.42326E-02 | 2.21163E-02 |
3.1.2 Infinite lattice case with multiple resonance absorbers
As the fuel burns, different resonance nuclides build up. A fresh UO2 fuel with 3.1% enrichment of 235U is taken as an example to verify the proposed method at different burnup steps. Figure 3 shows the error in eigenvalue versus burnup of 10–40 GW d/t using Method A or Method B to model the case. It can be seen that the RIF table captures the interference effect much better than the background cross-section iteration method, and the Method B results are quite acceptable.
-201602/1001-8042-27-02-010/alternativeImage/1001-8042-27-02-010-F003.jpg)
The verification results is given in Tables 4 and 5 for 30 GW d/t burnup, as a particular case named as Case-B for the convenience of discussion. Table 4 shows the material and number density of nuclides, and Table 5 shows the effective cross-sections for major absorbers (235U, 238U and 238Pu). Again, Method B gives better performance than Method A in most cases for all nuclides except for 238U. 238U is almost not affected by resonance interference due to its very large number density. Therefore the 238U effective cross-section is not sensitive to using Method A or Method B. These results are consistent with those in Sec. 3.1.1.
Materials | Fuel rod | Clad | Moderator | ||||||||
---|---|---|---|---|---|---|---|---|---|---|---|
235U | 236U | 238U | 239Pu | 240Pu | 241Pu | 242Pu | 16O | Zr-Nat | H | 16O | |
Na | 2.115d-2 | 8.449d-3 | 2.166 | 1.505d-2 | 4.441d-3 | 2.833d-3 | 7.811d-4 | 4.581 | 3.891 | 4.423 | 2.212 |
Energy groups | Absorption of 235U | Neutron production of 235U | Absorption of 236U | ||||||
---|---|---|---|---|---|---|---|---|---|
∑a | δ (%)b | ∑a | δ (%)b | ∑a | δ (%)b | ||||
Method A | Method B | Method A | Method B | Method A | Method B | ||||
15 | 4.4903 | 0.04 | 0.03 | 7.9297 | 0.06 | 0.05 | 1.0488 | -1.51 | -1.53 |
16 | 5.6829 | -0.11 | -0.09 | 10.421 | -0.12 | -0.09 | 1.2468 | -1.65 | -1.66 |
17 | 6.9896 | -0.22 | -0.16 | 12.588 | -0.21 | -0.21 | 1.5081 | -1.75 | -1.77 |
18 | 9.5685 | -0.07 | 0.13 | 14.996 | -0.37 | 0.06 | 1.9279 | -2.88 | -2.39 |
19 | 12.188 | -0.65 | -0.08 | 19.419 | -1.06 | -0.07 | 2.7944 | -2.97 | -1.95 |
20 | 16.959 | -0.13 | 0.30 | 28.924 | -0.06 | 0.49 | 5.0874 | -4.49 | -2.60 |
21 | 27.983 | -0.28 | -1.03 | 45.859 | -0.97 | -0.71 | 6.0751 | -5.57 | -9.20 |
22 | 34.903 | -0.30 | -0.17 | 53.623 | 0.05 | -0.39 | 17.340 | -7.43 | -3.49 |
23 | 59.000 | -2.68 | 0.11 | 100.37 | -3.04 | 0.15 | 17.684 | -11. 6 | -5.61 |
24 | 70.387 | -3.19 | 0.06 | 104.40 | -2.49 | 0.16 | 38.844 | -14.2 | -5.53 |
25 | 77.462 | 5.97 | -1.77 | 118.40 | 1.62 | -1.22 | 0.0511 | -2.98 | -1.28 |
26 | 78.153 | -2.13 | -1.86 | 91.932 | -1.95 | -1.77 | 0.1365 | -1.10 | -1.46 |
27 | 70.004 | -1.65 | -1.81 | 103.76 | -10.13 | -1.64 | 208.25 | -4.97 | -2.09 |
Energy groups | Absorption of 239Pu | Neutron production of 239Pu | Absorption of 238U | ||||||
∑ | δ (%) | ∑ | δ (%) | ∑ | δ (%) | ||||
Method A | Method B | Method A | Method B | Method A | Method B | ||||
15 | 3.6384 | -0.01 | -0.02 | 6.1712 | -0.04 | -0.04 | 69.268 | -0.23 | -0.20 |
16 | 4.5680 | 0.08 | 0.04 | 7.1936 | 0.11 | 0.08 | 0.7303 | -0.87 | -0.83 |
17 | 6.1122 | -0.18 | 0.11 | 9.8722 | 0.14 | 0.41 | 0.9418 | -1.70 | -1.61 |
18 | 7.2395 | -0.01 | -0.46 | 10.503 | 0.55 | -0.56 | 0.8698 | -1.61 | -1.53 |
19 | 10.240 | 3.16 | -0.51 | 17.738 | 3.53 | -0.59 | 1.1610 | -1.82 | -1.68 |
20 | 14.618 | -2.45 | 0.34 | 24.590 | -1.91 | 0.66 | 1.3305 | -2.41 | -2.19 |
21 | 29.322 | -1.82 | -3.08 | 44.010 | -1.14 | -1.64 | 1.5170 | -0.02 | 0.06 |
22 | 49.759 | -1.95 | -1.14 | 85.083 | -2.36 | -1.34 | 2.3971 | -0.26 | 0.18 |
23 | 100.02 | 4.41 | -2.72 | 177.93 | 5.57 | -2.95 | 2.0807 | 0.10 | 1.15 |
24 | 37.159 | -9.15 | 0.90 | 29.986 | -8.77 | 0.31 | 4.5449 | 2.19 | 2.71 |
25 | 79.071 | -8.77 | -0.89 | 122.97 | -8.99 | -1.21 | 6.1062 | 0.60 | 0.76 |
26 | 217.05 | -1.83 | -1.56 | 396.23 | -2.03 | -1.83 | 0.4759 | -0.94 | -0.10 |
27 | 54.238 | -14.30 | -2.16 | 89.712 | -13.35 | -2.55 | 7.8411 | -0.11 | 0.95 |
4 The single assembly case
A hexagonal single assembly case is tested to verify the proposed method for non-lattice geometry. Figure 4(a) shows the whole assembly and the sector of one twelfth of the assembly with reflective boundary condition. The arrangement of the cells in the selected sector is shown on the right part of Fig. 4(a). The cell types are shown in Fig. 4(b). Type T cell is the guide tube cell filled with moderator and clad tube. Type F cell is the fuel cell filled with the fuel rod, clad tube and moderator. As this is a rough assembly model, Types T and F cells share the same clad tube size and structure shown in Fig. 1. All fuel rods contain UO2 of 1.8% enrichment.
-201602/1001-8042-27-02-010/alternativeImage/1001-8042-27-02-010-F004.jpg)
This single assembly problem was solved using Method B and the results were compared to those of continuous energy Monte Carlo calculation for both eigenvalue and pin power distribution. The eigenvalue value is 1.24894± 0.00009 and the error is -161 pcm, and the pin power distribution error is 1% (Fig. 5). It should be noted that for this non-lattice problem, the Dancoff factor calculated with the neutron current method is position dependent, different for every fuel pin.
-201602/1001-8042-27-02-010/alternativeImage/1001-8042-27-02-010-F005.jpg)
5 Conclusion
Incorporating the Dancoff factor into the Stamm’ler equations and evaluating the Dancoff factor by the neutron current method provides a convenient method to calculate the effective resonant cross-section. Not only it is easier to do the calculation but the validity is also generalized to non-lattice geometry. To correct for the resonance interference effect, a simplified RIF table can be used adequately. Test problems using the proposed method have shown very good results for both the lattice geometry case and the non-lattice geometry case. The use of RIF table is much better than the conventional background cross-section iteration method for resonance interference correction.
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