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D型体主被动结合流动控制研究
引用本文:杨志刚,韩业恺,李启良,单希壮.D型体主被动结合流动控制研究[J].同济大学学报(自然科学版),2020,48(4):566-574.
作者姓名:杨志刚  韩业恺  李启良  单希壮
作者单位:1.同济大学 上海地面交通工具风洞中心, 上海 201804;2.同济大学 上海市地面交通工具空气动力与热环境模拟重点实验室,上海 201804;3.北京民用飞机技术研究中心, 北京 102211
基金项目:上海市地面交通工具风洞专业技术服务平台项目(19DZ2290400);上海市地面交通工具空气动力与热环境模拟重点实验室项目(18DZ2273300)
摘    要:以简化准三维模型D型钝体为研究对象,通过数值仿真手段,利用零质量合成射流器理论进行了D型体主动流动控制和主被动结合的流体控制研究发现,在尾部分离点进行射流控制时,高频射流有助于钝体减阻,减阻效果可以达到1.78%。主被动结合的锯齿和射流加强了尾迹三维流动结构,破坏了准三维模型的展向流动结构,使得减阻效果较好。采用主被动结合控制的射流为低频和高频时减阻效果为20.86%和21.20%。

关 键 词:D型体  气动减阻  主动控制  合成射流
收稿时间:2019/5/14 0:00:00
修稿时间:2020/2/25 0:00:00

Flow Control of Active and Passive Combination of D-Shaped Bluff Body
YANG Zhigang,HAN Yekai,LI Qiliang,SHAN Xizhuang.Flow Control of Active and Passive Combination of D-Shaped Bluff Body[J].Journal of Tongji University(Natural Science),2020,48(4):566-574.
Authors:YANG Zhigang  HAN Yekai  LI Qiliang  SHAN Xizhuang
Affiliation:1.Shanghai Automotive Wind Tunnel Center, Tongji University, Shanghai 201804, China;2.Shanghai Key Laboratory of Vehicle Aerodynamics and Vehicle Thermal Management Systems, Tongji University,Shanghai 201804, China;3.Beijing Aeronautical Science and Technology Research Institute, Beijing 102211, China
Abstract:To explore the flow field of the vehicle and the strategies of drag reduction, this paper focuses mainly on numerical simulation of the flow structures of D-shaped bluff body. Based on the theory of zero mass synthetic jet, it studies the active flow control and the active-passive flow control of D-shaped bluff body. It is found that high frequency jet can reduce the drag of D-shaped bluff body, and the maximum drag reduction can reach 1.78%. The combination of active and passive splitter plates with tabs and synthetic jet strengthens the three-dimensional flow structure of wake, impedes the extended flow structure in the wake of quasi-three-dimensional model, and makes the drag reduction perform better. The drag reduction effect is 20.86% at low frequencies and 21.20% at high frequencies.
Keywords:D-shaped bluff body  drag reduction  active control  synthetic jet
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