1 Introduction
The particle transport equation, which was first developed by Boltzmann for the kinetic theory of gases, is based on the conservation of the neutrons in a reactor system. The radiative transfer of stellar and planetary atmosphere and light scattering phenomenon are also related with the transport concept. Therefore, the description of the behavior of the neutrons in a reactor has a great importance for the first calculation and thus the construction and the operation of the reactor uneventfully. The number of fission neutrons is wanted to be constant in all types of reactors in order to obtain constant power and to control it safely. This situation of the reactor is defined as to be critical and the criticality of a fission system is one of the most important problems in neutron transport theory. Therefore, the critical size of a reactor can be said to be decided after the investigation of the criticality problem related with the system under consideration.
As well known, the transport equation is an integro-differential equation and thus it is not easy to solve it analytically. The discrete ordinates (SN) and polynomial expansion based techniques are accepted to be the most common and powerful ones among the methods developed for the solution of the transport equation [1-4]. In about all methods, either the derivative of the neutron angular flux or the neutron scattering function presented in the integral part of the transport equation are treated by some approximations to simplify the solution of the equation. In some instances, using an approximated scattering function in the transport equation can be sufficient depending on the scope of the problem under consideration. However, these approximations can take the problems and thus the solutions more or less away from the real situations. Since the scattering cross-sections vary with the scattering angle incredibly, various difficulties occur when the scattering function is represented in terms of any polynomials. Therefore, instead of using approximate expressions, if an exact scattering model is used in place of the scattering function, one could obtain more realistic results representing the system better [1,2].
Henyey and Greenstein [5] had first developed an exact scattering function called the Henyey-Greenstein (HG) formula to verify the existence of the diffuse interstellar radiation. However, they did not explain physically in their paper why they used such a function in the radiative transport equation. Later in the following studies such as biomedical applications, significant discrepancies have been reported about using the Henyey-Greenstein formula [5-7].
In this paper, an alternative scattering function (Anlı-Güngör, AG) which was applied successfully to the criticality problem in neutron transport theory using Legendre and the Chebyshev polynomials of first kind is preferred [9-11]. However, instead of using the first kind of Chebyshev polynomials, the second kind of Chebyshev polynomials approximation (UN method) is preferred to serve as an alternative solution method to the literature. This method has been successfully applied to the solutions of the problems of the transport equation in nearly a decade [13,15]. Therefore, this study can be thought of as the extension of the study previously carried out by Öztürk [11]. In the solution algorithm, the neutron angular flux is first expanded in terms of the Chebyshev polynomials of second kind then the AG phase function is inserted into the transport equation in place of the scattering function. At the end, applying the UN method to the resultant equation following the moment equations, a general expression for the criticality condition is obtained for one-speed neutrons. Then, the critical half-thicknesses of the slab are calculated using various scattering and collision parameters in the criticality condition. The numerical results are obtained with an increasing order of N = 1 to 9 and they are listed in Tables 1, 2, 3 and 4. Finally, a comparison table including the results obtained from the present method and the results obtained from the conventional PN method is given.
t | U1 | U3 | U5 | U7 | U9 |
---|---|---|---|---|---|
-1 | 6.35409 | 7.29973 | 7.27243 | 7.27499 | 7.27369 |
-4/5 | 6.50873 | 7.48101 | 7.45336 | 7.45608 | 7.45448 |
-3/4 | 6.54923 | 7.52819 | 7.50059 | 7.50333 | 7.50195 |
-2/3 | 6.61848 | 7.60864 | 7.58120 | 7.58398 | 7.58252 |
-1/2 | 6.76399 | 7.77692 | 7.75001 | 7.75283 | 7.75102 |
-3/10 | 6.95230 | 7.99354 | 7.96732 | 7.97020 | 7.96833 |
-1/4 | 7.00194 | 8.05049 | 8.02441 | 8.02729 | 8.02529 |
-1/5 | 7.05270 | 8.10865 | 8.08269 | 8.08560 | 8.08387 |
0 | 7.26764 | 8.35447 | 8.32866 | 8.33159 | 8.32957 |
1/5 | 7.50408 | 8.62419 | 8.59787 | 8.60083 | 8.59894 |
1/4 | 7.56698 | 8.69585 | 8.66929 | 8.67226 | 8.66762 |
3/10 | 7.63154 | 8.76937 | 8.74251 | 8.74549 | 8.74048 |
1/2 | 7.90785 | 9.08370 | 9.05518 | 9.05821 | 9.05398 |
2/3 | 8.16329 | 9.37393 | 9.34341 | 9.34647 | 9.34066 |
3/4 | 8.30095 | 9.53021 | 9.49849 | 9.50158 | 9.49957 |
4/5 | 8.38706 | 9.62794 | 9.59543 | 9.59858 | 9.59680 |
1 | 8.76137 | 10.05244 | 10.01637 | 10.01973 | 10.01662 |
t | U1 | U3 | U5 | U7 | U9 |
---|---|---|---|---|---|
-1 | 4.36099 | 4.98773 | 4.95863 | 4.96141 | 4.95998 |
-4/5 | 4.46439 | 5.11058 | 5.08128 | 5.08421 | 5.08269 |
-3/4 | 4.49144 | 5.14236 | 5.11315 | 5.11610 | 5.11456 |
-2/3 | 4.53769 | 5.19641 | 5.16742 | 5.17040 | 5.16882 |
-1/2 | 4.63477 | 5.30895 | 5.28061 | 5.28362 | 5.28200 |
-3/10 | 4.76024 | 5.45300 | 5.42548 | 5.42852 | 5.42682 |
-1/4 | 4.79329 | 5.49075 | 5.46339 | 5.46644 | 5.46471 |
-1/5 | 4.82706 | 5.52926 | 5.50204 | 5.50509 | 5.50338 |
0 | 4.96992 | 5.69153 | 5.66454 | 5.66761 | 5.66581 |
1/5 | 5.12677 | 5.86883 | 5.84138 | 5.84447 | 5.84261 |
1/4 | 5.16846 | 5.91583 | 5.88814 | 5.89123 | 5.88928 |
3/10 | 5.21121 | 5.96399 | 5.93601 | 5.93911 | 5.93711 |
1/2 | 5.39393 | 6.16940 | 6.13975 | 6.14288 | 6.14085 |
2/3 | 5.56249 | 6.35836 | 6.32668 | 6.32984 | 6.32764 |
3/4 | 5.65317 | 6.45983 | 6.42692 | 6.43011 | 6.42782 |
4/5 | 5.70985 | 6.52319 | 6.48948 | 6.49270 | 6.49033 |
1 | 5.95572 | 6.79755 | 6.76016 | 6.76360 | 6.76113 |
t | U1 | U3 | U5 | U7 | U9 |
---|---|---|---|---|---|
-1 | 1.08842 | 1.16747 | 1.13348 | 1.13843 | 1.13597 |
-4/5 | 1.11017 | 1.19975 | 1.16634 | 1.17137 | 1.16891 |
-3/4 | 1.11584 | 1.20746 | 1.17423 | 1.17924 | 1.17679 |
-2/3 | 1.12549 | 1.22006 | 1.18717 | 1.19217 | 1.18972 |
-1/2 | 1.14565 | 1.24468 | 1.21255 | 1.21748 | 1.21505 |
-3/10 | 1.17147 | 1.27373 | 1.24257 | 1.24737 | 1.24496 |
-1/4 | 1.17823 | 1.28099 | 1.25005 | 1.25481 | 1.25241 |
-1/5 | 1.18512 | 1.28827 | 1.25754 | 1.26226 | 1.25986 |
0 | 1.21406 | 1.31772 | 1.28759 | 1.29212 | 1.28974 |
1/5 | 1.24547 | 1.34808 | 1.31805 | 1.32237 | 1.31998 |
1/4 | 1.25376 | 1.35587 | 1.32576 | 1.33002 | 1.32763 |
3/10 | 1.26222 | 1.36374 | 1.33352 | 1.33772 | 1.33532 |
1/2 | 1.29809 | 1.39623 | 1.36508 | 1.36905 | 1.36662 |
2/3 | 1.33071 | 1.42471 | 1.39214 | 1.39596 | 1.39347 |
3/4 | 1.34808 | 1.43949 | 1.40596 | 1.40972 | 1.40719 |
4/5 | 1.35887 | 1.44855 | 1.41434 | 1.41809 | 1.41553 |
1 | 1.40513 | 1.48641 | 1.44860 | 1.45245 | 1.44965 |
t | U1 | U3 | U5 | U7 | U9 |
---|---|---|---|---|---|
-1 | 0.32188 | 0.30549 | 0.27813 | 0.27642 | 0.27071 |
-4/5 | 0.32719 | 0.31680 | 0.29045 | 0.28985 | 0.28463 |
-3/4 | 0.32856 | 0.31926 | 0.29298 | 0.29252 | 0.28734 |
-2/3 | 0.33090 | 0.32308 | 0.29684 | 0.29654 | 0.29142 |
-1/2 | 0.33574 | 0.32980 | 0.30350 | 0.30335 | 0.29832 |
-3/10 | 0.34190 | 0.33655 | 0.31016 | 0.30997 | 0.30503 |
-1/4 | 0.34350 | 0.33805 | 0.31165 | 0.31143 | 0.30651 |
-1/5 | 0.34512 | 0.33948 | 0.31308 | 0.31281 | 0.30792 |
0 | 0.35191 | 0.34465 | 0.31826 | 0.31771 | 0.31294 |
1/5 | 0.35917 | 0.34906 | 0.32266 | 0.32170 | 0.31705 |
1/4 | 0.36107 | 0.35007 | 0.32363 | 0.32255 | 0.31793 |
3/10 | 0.36301 | 0.35105 | 0.32456 | 0.32335 | 0.31175 |
1/2 | 0.37113 | 0.35465 | 0.32772 | 0.32591 | 0.32135 |
2/3 | 0.37841 | 0.35736 | 0.32960 | 0.32714 | 0.32249 |
3/4 | 0.38224 | 0.35866 | 0.33024 | 0.32738 | 0.32260 |
4/5 | 0.38461 | 0.35943 | 0.33052 | 0.32739 | 0.32249 |
1 | 0.39462 | 0.36258 | 0.33076 | 0.32612 | 0.32021 |
2 UN method with AG phase function
The stationary transport equation for one energy group neutrons in a source free medium can be written as,
where Ω′ and Ω are the unit vectors along the neutron velocity before and after a scattering collision, respectively.
Up to now, an appropriate scattering function representing the probabilities of the neutron interactions is found to be enough for the solutions of the problems in neutron transport theory because of its mathematical applicability. However, although using an approximate scattering function is usually accepted to be successful in many of the studies, the direct form of a scattering function like Henyey-Greenstein could be fascinating both in solution algorithm and in calculation of numerical results. On the other hand, the Henyey-Greenstein phase function is reported to be unsuccessful in some of the studies about radiative transfer [5-7]. Therefore, Anlı et al. constituted a new scattering kernel i.e., an AG phase function similar to Henyey-Greenstein formula and they first applied it to calculate the eigenvalue spectrum in the one-dimensional slab geometry transport equation [9,12]. In some recent studies, the AG phase function has been applied to diffusion equation and criticality problems in the transport theory using Legendre polynomials (PN method) and Chebyshev polynomials of first kinds (TN method) [10,11].
In this work, other than the previous studies about criticality calculations with defined scattering functions, the Chebyshev polynomials of second kind is preferred for use in the series expansion of the neutron angular flux. The AG phase function is used as the scattering function in the transport equation, and the critical half-thicknesses of the slab for one-speed neutrons are calculated for various values of the scattering parameters. Here, the detailed information about the PN method with the AG phase function does not needed to be given since it was mentioned in the previous work by the author [10,11].
The AG phase function, which is first used by Anlı et al. [9] in the determination of the eigenvalue spectrum, is then expressed as the scattering function,
where σS is any non-negative coefficient, t is the parameter representing all kinds of scattering (forward, backward and anisotropic, etc) and it is defined in the range of
The neutron angular flux is used as in Ref. [13],
When Eq. (2) is inserted on the right hand side of Eq. (1), the one-dimensional steady state transport equation can be written as,
with the free space boundary and symmetry conditions:
The slab is assumed to be homogeneous expanding from x = -a to x = a. The integrand on the right hand side of Eq. (5) over
Then, Eq. (5) can be rearranged using Eq. (7),
A dimensionless space variable, such that σTx/ν → x is defined in order to simplify the derivation of the equations and ν, is the eigenvalue.
In the application procedure of the method, first the neutron angular flux,
By following the steps mentioned above, a general expression for the UN moments of the angular flux could not be reached in this study. However, individual expressions for n = 0,1,2,…,9 are obtained and they are;
where Φ-1(x) = 0. A well-known solution [1],
is customarily used in Eqs. (11) in order to obtain analytic expressions of all An(ν)’s as follows,
where A-1(ν,t) = 0 and A0(ν,t) = 1. Eqs. (13) can also be written in a matrix form for an alternative solution algorithm,
where M(ν,t) is (N + 1) × (N + 1) coefficient matrix and A(ν,t) = [A0, A1,…,AN]T. It is possible to obtain non-trivial solutions for the discrete eigenvalues by equating the determinant of the coefficient matrix to zero, i.e. det[M(ν,t)] = 0.
As well known in the PN approximation, the contribution of the (N+1)th term to the neutron flux could be accepted as negligible. In addition, the Legendre and Chebyshev polynomials are the members of the Jacobi polynomials. Then by following the same procedure derived for the PN approximation, the discrete and continuumν eigenvalues can be obtained by setting AN+1(ν,t) = 0 for various values of c and t. A brief information about the profiles of the eigenvalues can be given as following: All roots of AN+1(ν) = 0 are identical with the roots of UN+1(ν) = 0 in the case of c = 0 and all values of t. When c = 1, one pair of the roots is
In other words, the same eigenvalues can be obtained using Eq. (14) by deriving a 2×2 matrix equation and then equating the determinant of the coefficient matrix to zero.
Therefore, the general solution of the flux moments for odd numbers of N can be written with so computed discrete eigenvalues νk for k = 1, …, N + 1,
where An(-ν,t) = (-1)n An(ν,t) and αk’s are the coefficients which can be determined from the physical boundary conditions of the system. The general solution Eq. (16) is constituted as the summation of all eigenvectors corresponding to each eigenvalues.
3 Boundary conditions and the critical system
The study of calculation of the eigenvalues of the problem representing the system under consideration can be said to be equivalent to find the critical size of that system. The values of the number of secondary neutrons per collision are very important to operate the reactor safely and decide whether it is critical or not. In a reactor, for each absorption collision the reactor cannot said to be critical when fewer neutrons are emitted than absorbed (c < 1). However, a reactor may be subcritical or critical for a slab of finite thickness with c > 1 [3].
The angular neutron flux is continuous across material region boundaries except for the direction μ = 0 in slab geometries. Any finite sum of the Legendre polynomials is continuous over the range -1 ⪯ μ ⪯ 1 and, therefore, continuous at μ = 0. Then, the PN approximation in slab geometries is a rather poor representation of the angular flux near material boundaries. Although the Mark and Marshak boundary conditions are the most commonly used ones for the criticality problems, the Marshak boundary condition which is based on the condition of zero incoming current at the vacuum boundary is somewhat more accurate than the Mark condition, at least for small N [3,16].
Because of the reasons mentioned above, for the criticality of the slab, the Marshak boundary condition for UN approximation of odd order can be written as,
In the application procedure of the boundary condition, first the neutron flux in Eq. (16) is replaced in Eq. (4) and then, the resulting equation is inserted into Eq. (17) with the parity relation of the Chebyshev polynomials of second kind Uk(-μ) = (-1)kUk(μ),
where In,k is,
and
Eq. (18) is referred to as the criticality condition and it can also be written in a matrix form,
where βk is the column vector comprising elements of
4 Numerical results
An application of the Chebyshev polynomials expansion (UN approximation) is done for the critical slab problem for one-speed neutrons in a uniform homogeneous medium. In the method, the Chebyshev polynomials of second kind are used in the angular part of the neutron flux as it has been successfully applied before [13,15]. Contrary to previous approximation scattering functions, in order to get closer to accurate solution of the transport equation, the AG phase function is used. Various values of c and t are used in Eq. (13) or (14) to compute the discrete eigenvalues by setting AN+1(ν) = 0. An analytic expression of the eigenvalues for U1 approximation is obtained and it is given in Eq. (15). Various orders of the UN approximation with the AG phase function are applied to Eq. (18) or (21) and the numerical results for the critical half-thickness of the slab are tabulated in Tables 1 through 4. A final table i.e. Table 5, has been needed to compare the results obtained from the present method with the ones already obtained from the conventional PN method in a previous study [11]. The Marshak boundary condition is used during the application of the criticality condition to the problem since it is accepted as to be more valid than the Mark for small N [3,16]. All calculations are carried out by means of the Maple software and the total macroscopic cross section is taken as to be its normalized value, σT = 1 cm-1.
t | c = 1.01 | c= 1.20 | c= 2.00 | |||
---|---|---|---|---|---|---|
P9 [11] | U9(present work) | P9 [11] | U9(present work) | P9 [11] | U9(present work) | |
-1 | 7.27723 | 7.27369 | 1.13840 | 1.13597 | 0.27052 | 0.27071 |
-4/5 | 7.45782 | 7.45448 | 1.17127 | 1.16891 | 0.28491 | 0.28463 |
-3/4 | 7.50499 | 7.50195 | 1.17906 | 1.17679 | 0.28775 | 0.28734 |
-2/3 | 7.58523 | 7.58252 | 1.19179 | 1.18972 | 0.29202 | 0.29142 |
-1/2 | 7.75318 | 7.75102 | 1.21664 | 1.21505 | 0.29922 | 0.29832 |
-3/10 | 7.96959 | 7.96833 | 1.24599 | 1.24496 | 0.30618 | 0.30503 |
-1/4 | 8.02650 | 8.02529 | 1.25333 | 1.25241 | 0.30769 | 0.30651 |
-1/5 | 8.08440 | 8.08387 | 1.26068 | 1.25986 | 0.30913 | 0.30792 |
0 | 8.33040 | 8.32957 | 1.29038 | 1.28974 | 0.31418 | 0.31294 |
1/5 | 8.60028 | 8.59894 | 1.32081 | 1.31998 | 0.31814 | 0.31705 |
1/4 | 8.67076 | 8.66762 | 1.32856 | 1.32763 | 0.31896 | 0.31793 |
3/10 | 8.74482 | 8.74048 | 1.33638 | 1.33532 | 0.31971 | 0.31175 |
1/2 | 9.05877 | 9.05398 | 1.36833 | 1.36662 | 0.32188 | 0.32135 |
2/3 | 9.34822 | 9.34066 | 1.39580 | 1.39347 | 0.32251 | 0.32249 |
3/4 | 9.50423 | 9.49957 | 1.40981 | 1.40719 | 0.32232 | 0.32260 |
4/5 | 9.60097 | 9.59680 | 1.41830 | 1.41553 | 0.32201 | 0.32249 |
1 | 10.02130 | 10.01662 | 1.45277 | 1.44965 | 0.31913 | 0.32021 |
In Tables 1, 2, 3, 4, the critical half-thicknesses of the slab are listed for c = 1.01, 1.02, 1.20, and 2.00 and t is selected with increasing order from -1 to 1. One can easily test that the t = 0 case corresponds to isotropic scattering [9,13,15]. In other words, by replacing the case of t = 0 in Eqs. (15-18) one would obtain the equations necessary for calculating the eigenvalues and the critical half-thicknesses using the UN method in slab geometry for isotropic scattering [13,15].
It can be seen from the tables that in many cases, the critical half-thickness of the slab increases while t is increasing and c is decreasing. It was reported that the critical thickness of the slab can behave non-monotonic when neutrons tend to propagate in the forward direction. This is observed as first an increasing trend and then a decreasing trend with increasing forward anisotropy parameter according to the choice of the c. This behavior of the critical thickness is referred to as non-monotonic and it is observed in this study for t approaching to 1 and c = 2, especially in the case of higher order approximations with N > 5. That means the same non-monotonic behavior of the critical thickness as reported before [17,18] appears when the neutrons scatter in the forward peaked directions. This circumstance can be followed in Tables 4 and 5 by examining the values with t > ¼. However, since the criticality calculations are important especially for c near to 1, this anomaly for the AG phase function can be thought as negligible. It can be seen from these tables that this non-monotonic behavior has occurred when c = 2.00 (away from 1) and higher order approximation is used (N = 9) which is pointed to as the advantage of the Marshak boundary condition against the Mark [3]. More discrepancies about the behavior of the critical thickness are reported as to be seen when using Henyey-Greenstein phase function [11].
5 Conclusion
In this paper, the critical thickness of one-speed neutrons in a finite homogeneous slab is studied using UN approximation which is applied successfully in preceding studies [13,15]. As a second important application of this study, the AG phase function is chosen as the scattering kernel of the transport equation. The critical half-thicknesses of the slab are calculated numerically using increasing orders of the UN approximation up to N = 9 for both positive and negative values of the parameter t. While the positive values of t represent the forward peaked scattering of the neutrons, the negative values of it represent the backward peaked scattering of the neutrons. These are physically possible situations presented in a reactor. When a neutron interacts with a particle having a mass approximately equal to the mass of the interacting neutron, such as a hydrogen nucleus in a moderator, this interaction has a probability to end with a forward scattering. In a similar way, when a neutron interacts with a particle having a mass of greater than the mass of the interacting neutron, such as an Oxygen nucleus in a moderator, a nucleus in reactor material, or a daughter nucleus emitted from a fission reaction, this interaction has a probability to end with a backward scattering [9]. Therefore, this study can be evaluated as the calculation of the critical half-thickness of the slab for forward and backward scattering since both the positive and negative values of t are taken in Tables 1, , 3, 4, 5.
In summary, one can easily assert from the derivation of the equations and the results already obtained here that the AG phase function is seen to be convenient for the solution of the problems in transport theory. Furthermore, the AG phase function with its easily applicable derivation can also be sufficient for other problems containing a phase function in particle or photon transport and in science and engineering.
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