中国机械工程Issue(3)：383-386,4.DOI:10.3969/j.issn.1004-132X.2016.03.018
航空发动机风扇叶片脱落仿真分析大规模并行计算方法研究
Study on Parallel Computing Methods for Aero Engine Fan Blade off Simulation Analyses
摘要
Abstract
To solve the numerical simulation problem of fan blade off in aero engine,the effects of parallel mode and grid domain decomposition strategy on computing efficiency and consistence were analyzed herein.An optimal strategy for domain decomposition and parallel mode configuration was proposed to satisfy the computation consistency requirements.The superiority of the strategy was ver-ified by a practical engineering case.关键词
航空发动机/风扇叶片脱落/并行计算/一致性Key words
aero engine/fan blade off/parallel computing/consistency分类
航空航天引用本文复制引用
侯亮,张晓云,王志强,柴象海..航空发动机风扇叶片脱落仿真分析大规模并行计算方法研究[J].中国机械工程,2016,(3):383-386,4.基金项目
国家自然科学基金资助项目(51205377) （51205377）
上海市自然科学基金资助项目(13ZR142230) （13ZR142230）
