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Technical Papers

Direct Comparison of High-Order/Low-Order Transient Methods on the 2D-LRA Benchmark Problem

ORCID Icon, &
Pages 409-432 | Received 19 Jul 2021, Accepted 07 Sep 2021, Published online: 21 Dec 2021

Figures & data

Fig. 1. 2D-LRA geometry.Citation11

Fig. 1. 2D-LRA geometry.Citation11

Fig. 2. Example power evolution during the 2D-LRA transient on a 1 cm mesh.

Fig. 2. Example power evolution during the 2D-LRA transient on a 1 cm mesh.

Fig. 3. Assembly power densities normalized to 1 W/cm3 at steady state, error with respect to results by Smith.Citation12

Fig. 3. Assembly power densities normalized to 1 W/cm3 at steady state, error with respect to results by Smith.Citation12

TABLE I Sensitivity of the Transient Results on Time Step Size: Comparison with a Fine-Time Solution

Fig. 4. Time stepping scheme for transient HOLO methods.

Fig. 4. Time stepping scheme for transient HOLO methods.

Fig. 5. Example reactivity evolution during the 2D-LRA transient on a 1 cm mesh.

Fig. 5. Example reactivity evolution during the 2D-LRA transient on a 1 cm mesh.

Fig. 6. Summary of HOLO methods and their relationships.

Fig. 6. Summary of HOLO methods and their relationships.

Fig. 7. Power profile shows that the fixed shape method is inadequate.

Fig. 7. Power profile shows that the fixed shape method is inadequate.

Fig. 8. Zoom-in to the first peak.

Fig. 8. Zoom-in to the first peak.

Fig. 9. Values of k-balance over time.

Fig. 9. Values of k-balance over time.

Fig. 10. Prompt frequencies as calculated by the omega method (in units of inverse seconds).

Fig. 10. Prompt frequencies as calculated by the omega method (in units of inverse seconds).

Fig. 11. Precursor frequencies for each delayed neutron group in the first cell of the geometry as calculated by the omega method (in units of inverse seconds).

Fig. 11. Precursor frequencies for each delayed neutron group in the first cell of the geometry as calculated by the omega method (in units of inverse seconds).

Fig. 12. Spatial distribution of delayed frequencies for precursor group 2 at different points in time, as calculated by the omega method (in units of inverse seconds).

Fig. 12. Spatial distribution of delayed frequencies for precursor group 2 at different points in time, as calculated by the omega method (in units of inverse seconds).

TABLE II Sensitivity of the Adiabatic Method to Outer Time Step Size

TABLE III Sensitivity of the Omega Method to Outer Time Step Size

Fig. 13. Normalized assembly power densities at the peak for adiabatic versus omega. In green and red are errors that are lower and higher for omega method, respectively.

Fig. 13. Normalized assembly power densities at the peak for adiabatic versus omega. In green and red are errors that are lower and higher for omega method, respectively.

Fig. 14. Assembly temperatures at the end of transient for adiabatic versus omega. In green and red are errors that are lower and higher for omega method, respectively.

Fig. 14. Assembly temperatures at the end of transient for adiabatic versus omega. In green and red are errors that are lower and higher for omega method, respectively.

TABLE IV Alpha Eigenvalue Results, Obtained with 0.1 s Outer Time Steps

Fig. 15. Power profile, zoomed-in.

Fig. 15. Power profile, zoomed-in.

Fig. 16. Absolute error with respect to reference, in time, zoomed to the second peak.

Fig. 16. Absolute error with respect to reference, in time, zoomed to the second peak.

Fig. 17. Values of k-balance over time.

Fig. 17. Values of k-balance over time.

Fig. 18. Normalized assembly power densities at the peak for modified versus hybrid alpha. In green and red are errors that are lower or higher for hybrid, respectively.

Fig. 18. Normalized assembly power densities at the peak for modified versus hybrid alpha. In green and red are errors that are lower or higher for hybrid, respectively.

Fig. 19. Assembly temperatures at the end of transient for modified versus hybrid alpha. In green and red are errors that are lower or higher for hybrid, respectively.

Fig. 19. Assembly temperatures at the end of transient for modified versus hybrid alpha. In green and red are errors that are lower or higher for hybrid, respectively.

TABLE V Sensitivity of the Coarse Time Integration Method to Outer Time Step Size

TABLE VI Sensitivity of the Stripped-Down Coarse Time Integration Method to Outer Time Step Size

TABLE VII Time-Differencing Results, Obtained with 0.01 s Outer Time Steps

Fig. 20. Comparing prompt frequencies in the FTM to the amplitude derivative term in the IQS method.

Fig. 20. Comparing prompt frequencies in the FTM to the amplitude derivative term in the IQS method.

Fig. 21. Zoomed-in power profile.

Fig. 21. Zoomed-in power profile.

Fig. 22. Normalized assembly power densities at the peak for the IQS method versus the FTM. In green and red are errors that are lower and higher for FTM, respectively.

Fig. 22. Normalized assembly power densities at the peak for the IQS method versus the FTM. In green and red are errors that are lower and higher for FTM, respectively.

Fig. 23. Assembly temperatures at the end of transient for the IQS method versus the FTM. In green and red are errors that are lower and higher for FTM, respectively.

Fig. 23. Assembly temperatures at the end of transient for the IQS method versus the FTM. In green and red are errors that are lower and higher for FTM, respectively.

TABLE VIII Impact of Frequencies on Peak Power RMS Error

Fig. A.1. 2D-LRA geometry.Citation11

Fig. A.1. 2D-LRA geometry.Citation11