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Low-Rank Methods for Radiation Transport Calculations

thesis
posted on 2024-03-25, 02:19 authored by Zhuogang Peng
<p>This dissertation seeks to reduce the computational cost in radiation transport calculations using dynamical low-rank approximation (DLR) methods, a complexity reduction technique to approximate a tensor or a matrix with a reduced rank. A DLR approximation method is developed for the time-dependent radiation transport equation in 1-D and 2-D Cartesian geometries. A low-rank system that evolves on a low-rank manifold via an operator-splitting approach is constructed using a finite volume (FV) method in space and a spherical harmonics (P<i><sub>N</sub></i>) basis in angle. Numerical results demonstrate that the low-rank solution requires less memory than solving the full-rank equations with the same accuracy. Furthermore, the low-rank algorithm can obtain much better results at a moderate extra cost by refining the discretization while keeping the rank fixed. </p><p>The DLR method does not preserve the number of particles, which limits its practicability. This conservation issue is addressed by solving a low-order equation with closure terms coupled to a low-rank approximation with the high-order solution. The high-order solution approximates the closure term well, and the low-order solution corrects the low-rank evolution's conservation bias. The so-called high-order / low-order (HOLO) algorithm is demonstrated that overcomes the conservation difficulty while the computational efficiency and accuracy are preserved. </p><p>The low-rank scheme is extended for the time-dependent radiation transport equation in 2-D and 3-D Cartesian geometries with discrete ordinates (S<i><sub>N</sub></i>) discretization in angle. The reduced system that evolves on a low-rank manifold is constructed via an “unconventional” basis update & Galerkin integrator to avoid a substep that is backward in time, which could be unstable for dissipative problems. The resulting system preserves the information on angular direction by applying separate low-rank decompositions in each octant where angular intensity has the same sign as the direction cosines. Then, transport sweeps and source iteration can efficiently solve this low-rank-SN system. The numerical results in 2-D and 3-D Cartesian geometries demonstrate that the low-rank solution requires less memory and computational time than solving the full-rank equations using transport sweeps without losing accuracy.</p>

History

Date Modified

2023-04-18

Additional Groups

  • Aerospace and Mechanical Engineering

Alternate Identifier

1376356933

Defense Date

2023-01-11

CIP Code

  • 14.1901

Research Director(s)

Ryan G. McClarren

Committee Members

Karel Matous Matthew Zahr Meng Wang

Degree

  • Doctor of Philosophy

Degree Level

  • Doctoral Dissertation

OCLC Number

1376356933

Program Name

  • Aerospace and Mechanical Engineering

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