TY - GEN
T1 - Bandwidth-Optimized Summation-by-Parts Operators for High-Resolution Turbulent Flow Simulations
AU - Coder, James G.
N1 - Publisher Copyright:
© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2023
Y1 - 2023
N2 - Three new, bandwidth-optimized, 4th-order-accurate finite-difference schemes are introduced with boundary closures that satisfy the summation-by-parts convention. These schemes include a conventional-form interior scheme with diagonal norm and two Padé-type schemes, one with a pentadiagonal norm and one with a tridiagonal norm. It is proven that tridiagonal Padé schemes are limited to 1st-order boundary closures for the commonly used structure of the implicit and explicit sides, whereas 3rd-order closure was achievable with a pentadiagonal norm. Modified wavenumber analyses are presented to show the spectral resolution of the various schemes, and various test cases are considered to evaluate their efficacy. After this evaluation, the optimized conventional scheme with diagonal boundary closure appeared to have the best combination of resolution, stability, and computational efficiency.
AB - Three new, bandwidth-optimized, 4th-order-accurate finite-difference schemes are introduced with boundary closures that satisfy the summation-by-parts convention. These schemes include a conventional-form interior scheme with diagonal norm and two Padé-type schemes, one with a pentadiagonal norm and one with a tridiagonal norm. It is proven that tridiagonal Padé schemes are limited to 1st-order boundary closures for the commonly used structure of the implicit and explicit sides, whereas 3rd-order closure was achievable with a pentadiagonal norm. Modified wavenumber analyses are presented to show the spectral resolution of the various schemes, and various test cases are considered to evaluate their efficacy. After this evaluation, the optimized conventional scheme with diagonal boundary closure appeared to have the best combination of resolution, stability, and computational efficiency.
UR - https://www.scopus.com/pages/publications/85199907966
UR - https://www.scopus.com/pages/publications/85199907966#tab=citedBy
U2 - 10.2514/6.2023-3862
DO - 10.2514/6.2023-3862
M3 - Conference contribution
AN - SCOPUS:85199907966
SN - 9781624107047
T3 - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
BT - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
Y2 - 12 June 2023 through 16 June 2023
ER -