Two-level parallel load balancing strategy for accelerating DSMC simulations in near-continuum gases

Author:

Xiao Chenxiang1ORCID,Zhang Chenchen2ORCID,Zhang Bin13,Xu Hui1,Liu Hong1

Affiliation:

1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, 800 Dong Chuan Road, Shanghai 200240, P. R. China

2. School of Mathematical Sciences, Peking University, Beijing 100871, P. R. China

3. Sichuan Research Institute, Shanghai Jiao Tong University, Chengdu 610213, P. R. China

Abstract

The Direct Simulation Monte Carlo (DSMC) algorithm is widely employed for simulating rarefied gas flows and is increasingly applied in near-continuum regimes for research and engineering purposes. However, its computational demands, notably load imbalance and extended simulation time, hinder widespread adoption. Addressing these challenges, this paper introduces the Two-Level parallel load balancing strategy. This novel approach combines thread-level and multi-process parallelism to enhance load balancing and reduce simulation time. Key features include a thread-level load-decoupling strategy implemented via OpenMP and a multi-process load balancing mechanism employing distributed memory via MPI. Building upon our previous [Formula: see text] [L. Li, W. Ren and B. Zhang, J. Aeronaut. Astronaut. Aviat. Ser. A 46, 88 (2014)] approach, the load balancing mechanism utilizes Stop At Risk (SAR) criteria for repartitioning with METIS. Additionally, a specialized data transmission mechanism utilizing MPI nonblocking communication minimizes global communication between processes. Validation and evaluation are performed using four hypersonic flow cases around a cylinder and sphere, demonstrating significant improvements. Notably, the proposed strategy achieves [Formula: see text] enhancement over the [Formula: see text] strategy under 512 CPU cores compared to 16 CPU cores, and reduces between-process communication time with [Formula: see text]. These advancements contribute to enhancing the effectiveness of the DSMC algorithm in near-continuum aerodynamic simulations.

Funder

Sichuan Science and Technology Program

Shanghai Academy of Spaceflight Technology

Publisher

World Scientific Pub Co Pte Ltd

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