Compact Finite Difference based Framework for Large Scale Simulations of Compressible Turbulent Flows
ORAL
Abstract
This work develops a computational framework modernizing the utilization of compact finite difference methods on large scale high performance computing platforms for simulations of compressible turbulent flows. The framework has two major components — a parallel algorithm to solve the cyclic banded system, and a unified discretization approach for compressible Navier-Stokes equations. The linear solver considers the operations on distributed and shared memory hierarchies assuming a flexible grid partition strategy without all-to-all communication nor iterations. The discretization approach allows all conservative variables to be stored at collocated grid points while fluxes to be assembled at staggered grid points. Computational robustness is gained by implicit dealiasing in nonlinear flux assembly as well as enhanced spectral resolution from staggereing and model based subgrid dissipation. The framework has been demonstrated to scale up to 24576 GPUs, and maintains robust performance on cartesian and curvilinear mesh without the need for numerical filtering.
*This work is supported by the National Science Foundation, grant number OAC-2103509. The investigation used resources of the Oak Ridge Leadership Computing Facility at the Oak Ridge National Laboratory. The research code development used resources from the Extreme Science and Engineering Discovery Environment.
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Publication:Song, H., Ghate, A. S., Matsuno, K. V., West, J. R., Subramaniam, A., Brown, L. J., & Lele, S. K. (2022). Robust high-resolution simulations of compressible turbulent flows without filtering. In AIAA AVIATION 2022 Forum (p. 4122).
Song, H., Matsuno, K. V., West, J. R., Subramaniam, A., Ghate, A. S., & Lele, S. K. (2022). Scalable Parallel Linear Solver for Compact Banded Systems on Heterogeneous Architectures. Journal of Computational Physics, 111443.
Presenters
Hang Song
Stanford University
Authors
Hang Song
Stanford University
Aditya S Ghate
Stanford Univ
Akshay Subramaniam
Stanford Univ
Kristen V Matsuno
Stanford University
Jacob R West
Department of Mechanical Engineering, Stanford University, CA, USA