航空学报 > 2009, Vol. 30 Issue (7): 1219-1226

流体力学、飞行力学与发动机

二维翼型微吸吹气减阻控制新技术数值研究

段会申1,刘沛清1,何雨薇1,陈建中1,2   

  1. 1北京航空航天大学 航空科学与工程学院 2中国空气动力研究与发展中心
  • 收稿日期:2009-01-03 修回日期:2009-03-08 出版日期:2009-07-25 发布日期:2009-07-25
  • 通讯作者: 刘沛清

Numerical Investigation of Drag-reduction Control by Micro-suction-blowing on Airfoil

Duan Huishen1, Liu Peiqing1, He Yuwei1, Chen Jianzhong1,2   

  1. 1School of Aeronautic Science and Engineering, Beijing University of Aeronautics and  Astronautics 2China Aerodynamics Research and Development Center
  • Received:2009-01-03 Revised:2009-03-08 Online:2009-07-25 Published:2009-07-25
  • Contact: Liu Peiqing

摘要: 结合抽吸气转捩控制和微吹气湍流减阻控制的特点,探索了一种新的吸吹气减阻控制技术。使用Fluent求解器,并利用用户自定义函数(UDF)二次开发对其自带的Wilcox转捩模式进行了修正。在此基础上,数值研究了吸吹气控制对翼型阻力性能的影响。结果表明:在一定的吸气量范围内,吸气、吸吹气控制都能使翼型总阻力减小,且在同一雷诺数下,吸气控制能使翼型总阻力减小约3%,而吸吹气联合控制使翼型总阻力减小约16%。由此可见,吸吹气控制技术是一种行之有效的减阻控制技术。

关键词: 翼型, 层流流动, 转捩, 湍流减阻, 吸吹气控制

Abstract: Combining the characteristics of suction-transition control and micro-blowing turbulence-drag-reduction technology, a novel suction-blowingcontrol technique is put forward to reduce airfoil drag. By using the computational fluid dynamics (CFD) code of Fluent, the Wilcox transition mode is modified by a user-defined function (UDF) and incorporated into the CFD code. Based on the above modifications, the effect of suctionblowing control on the airfoil drag performance is numerically studied. The results show that when the suction flow rate are in a certain range, suction and suction-blowing control can both reduce the total drag of an airfoil. At the same Reynolds number, the leadingedge suction without blowing reduces the total drag below the airfoil by up to 3%, while the suction-blowing control results in a drag reduction by up to 16%. Therefore, the suction-blowing control technique is an effective way for drag reduction control.

Key words: airfoils, laminar flow, transition, turbulence-drag reduction, suction-blowing control

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