Journal of Bionic Engineering ›› 2020, Vol. 17 ›› Issue (2): 303-314.doi: 10.1007/s42235-020-0024-5

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Synthetic Jet Control on the Propulsion Behavior of a Foil in Plunge-pitch Motion

Yadong Li1, Guoqing Zhou1, Jie Wu2,3*   

  1. 1. Liaoning General Aviation Academy, Shenyang Aerospace University, Shenyang 110136, China
    2. College of Aerospace Engineering, Shenyang Aerospace University, Shenyang 110136, China
    3. State Key Laboratory of Mechanics and Control of Mechanical Structures, 
    Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • 收稿日期:2019-11-08 修回日期:2020-01-06 接受日期:2020-01-09 出版日期:2020-03-10 发布日期:2020-03-27
  • 通讯作者: Jie Wu E-mail:wuj@nuaa.edu.cn
  • 作者简介:Yadong Li1, Guoqing Zhou1, Jie Wu2,3*

Synthetic Jet Control on the Propulsion Behavior of a Foil in Plunge-pitch Motion

Yadong Li1, Guoqing Zhou1, Jie Wu2,3*   

  1. 1. Liaoning General Aviation Academy, Shenyang Aerospace University, Shenyang 110136, China
    2. College of Aerospace Engineering, Shenyang Aerospace University, Shenyang 110136, China
    3. State Key Laboratory of Mechanics and Control of Mechanical Structures, 
    Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • Received:2019-11-08 Revised:2020-01-06 Accepted:2020-01-09 Online:2020-03-10 Published:2020-03-27
  • Contact: Jie Wu E-mail:wuj@nuaa.edu.cn
  • About author:Yadong Li1, Guoqing Zhou1, Jie Wu2,3*

摘要: The Synthetic Jet (SJ) control on the propulsion behavior of a foil in plunge-pitch motion is examined in this work by numerical simulations. An elliptic foil with ratio of 8 performs the plunge and pitch motions synchronously. A pair of SJs with the same frequency and strength is integrated into the upper and lower surfaces of the foil. As a result, the local flow field around the foil could be obviously modified by the SJs. At the Reynolds number of 200, the effects of the inclined angle between the jet direction and the chord line, the phase angle between the SJs and the flapping motion as well as the location of SJ on the propulsion performance are systematically investigated. Compared with the pure plunging and pitching foil, it is indicated that the enhancement of mean thrust and propulsive efficiency can be obtained by the SJs with suitable working parameters. Based on the numerical analysis, it is found that the jet flow on the foil surfaces, which changes the local pressure distribution to increase the pressure difference between upper and lower surfaces, can benefit the propulsion behavior of the flapping foil.

关键词: propulsion behavior, plunge-pitch motion, elliptic foil, synthetic jet

Abstract: The Synthetic Jet (SJ) control on the propulsion behavior of a foil in plunge-pitch motion is examined in this work by numerical simulations. An elliptic foil with ratio of 8 performs the plunge and pitch motions synchronously. A pair of SJs with the same frequency and strength is integrated into the upper and lower surfaces of the foil. As a result, the local flow field around the foil could be obviously modified by the SJs. At the Reynolds number of 200, the effects of the inclined angle between the jet direction and the chord line, the phase angle between the SJs and the flapping motion as well as the location of SJ on the propulsion performance are systematically investigated. Compared with the pure plunging and pitching foil, it is indicated that the enhancement of mean thrust and propulsive efficiency can be obtained by the SJs with suitable working parameters. Based on the numerical analysis, it is found that the jet flow on the foil surfaces, which changes the local pressure distribution to increase the pressure difference between upper and lower surfaces, can benefit the propulsion behavior of the flapping foil.

Key words: propulsion behavior, plunge-pitch motion, elliptic foil, synthetic jet