TY - GEN
T1 - Additive multigrid with scaled correction for implicit compressible flow solvers
AU - Vangara, Syam
AU - Kashi, Aditya
AU - Nadarajah, Siva
N1 - Publisher Copyright:
© 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2019
Y1 - 2019
N2 - Application of additive multigrid with scaled correction for implicit solvers of the compressible Reynolds-averaged Navier-Stokes (RANS) equations is presented. Using multiplicative V-cycle multigrid to solve RANS equations in parallel typically results in poor parallel efficiency on the coarser grids. To alleviate these issues, additive multigrid can be used, since it exhibits better parallel efficiency. However, additive multigrid is typically observed to be slower than multiplicative multigrid and, in some cases it may not even converge. In this work, the convergence rate of additive multigrid is improved significantly through scaling the correction. Convergence of the approach compared to V-cycle is demonstrated for RANS equations on several external aerodynamics cases. In light of emerging massively parallel hardware for scientific computing, the applicability of the asynchronous fine-grain parallel smoothers to the proposed method is verified.
AB - Application of additive multigrid with scaled correction for implicit solvers of the compressible Reynolds-averaged Navier-Stokes (RANS) equations is presented. Using multiplicative V-cycle multigrid to solve RANS equations in parallel typically results in poor parallel efficiency on the coarser grids. To alleviate these issues, additive multigrid can be used, since it exhibits better parallel efficiency. However, additive multigrid is typically observed to be slower than multiplicative multigrid and, in some cases it may not even converge. In this work, the convergence rate of additive multigrid is improved significantly through scaling the correction. Convergence of the approach compared to V-cycle is demonstrated for RANS equations on several external aerodynamics cases. In light of emerging massively parallel hardware for scientific computing, the applicability of the asynchronous fine-grain parallel smoothers to the proposed method is verified.
UR - http://www.scopus.com/inward/record.url?scp=85099511944&partnerID=8YFLogxK
U2 - 10.2514/6.2019-3712
DO - 10.2514/6.2019-3712
M3 - Conference contribution
AN - SCOPUS:85099511944
SN - 9781624105890
T3 - AIAA Aviation 2019 Forum
SP - 1
EP - 8
BT - AIAA Aviation 2019 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aviation 2019 Forum
Y2 - 17 June 2019 through 21 June 2019
ER -