显式动力学子模型法在航空发动机整机瞬态冲击并行计算中的应用
柴象海1,2,*(
),胡寿丰1,2,张执南3,侯亮1,2
),胡寿丰1,2,张执南3,侯亮1,2
Application of Explicit Dynamic Sub-Model Method in Parallel Calculation of Aero-Engine Transient Impact
CHAI Xianghai1,2,*(),HU Shoufeng1,2,ZHANG Zhinan3,HOU Liang1,2
),HU Shoufeng1,2,ZHANG Zhinan3,HOU Liang1,2
图6. 子模型选取及边界定义
Fig.6. Sub-model selection and boundary definition
