西华大学学报（自然科学版）2018，Vol.37Issue(1)：62-67,6.DOI:10.3969/j.issn.1673-159X.2018.01.010
快背式MIRA模型射流主动控制气动减阻研究
Active Flow Control of Fast-back MIRA Model to Reduce Aerodynamic Drag with Steady Jet
田思 1侯园章 2吴敏 1朱玲 1李春林 1杨彦君1
作者信息
- 1. 奇瑞上海技术中心,上海200120
- 2. 中国汽车工程研究院股份有限公司,重庆401120
- 折叠
摘要
Abstract
In this paper,the CFD simulation software STAR-CCM + is used to simulate the wake field of the MI RA model.The flow mode of the tail flow field was controlled by the active control drag reduction technique with steady jet.The method of jet reduction and the SST k-w turbulence model were adopted to simulate the tail flow field of the fast-back MIRA model.The position of the tail was studied.The best reduction case was obtained and the variation of the tail vortex was anlyzed.It is found that the pressure of the model can be changed by controlling the separation vortex of the tail of the model in order to reduce the pressure resistance of the model and realize the purpose of drag reduction.关键词
外流场/CFD/主动控制/射流/尾流结构/气动减阻Key words
outflow field/CFD/active control/jet flow/wake structure/aerodynamic drag reduction分类
交通工程引用本文复制引用
田思,侯园章,吴敏,朱玲,李春林,杨彦君..快背式MIRA模型射流主动控制气动减阻研究[J].西华大学学报（自然科学版）,2018,37(1):62-67,6.
