CLOSED-LOOP ACTIVE FLOW CONTROL OF THE WAKE OF A COMPRESSOR BLADE BY TRAILING-EDGE BLOWING

被引:0
|
作者
Kiesner, Matthias [1 ]
King, Rudibert [1 ]
机构
[1] Tech Univ Berlin, Chair Measurement & Control, D-10623 Berlin, Germany
关键词
Active Flow Control; Trailing-Edge Blowing; Robust Control; Stator Cascade; REDUCTION;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper presents a closed-loop active flow control strategy to reduce the velocity deficit of the wake of a compressor stator blade. The unsteady stator-rotor interaction, caused by the incoming stator wakes, generates fast changes of the rotor blade loading, affecting the stability and the performance of the overall compressor. Negative effects will be seen likewise when unsteady combustion concepts, such as a pulsed detonation, produce upstream disturbances. Furthermore, the periodic unsteady flow leads to additional undesired effects such as noise and blade vibrations. A controlled reliable manipulation of the stator wake is a way to handle these issues. Therefore, investigations on wake manipulation with trailing-edge blowing were carried out on a new low-speed cascade test rig. Detailed information about the wake profile is obtained by five-hole probe measurements in a plane downstream of the cascade for the natural and the actuated flow at a Reynolds number of 6x10(5). These measurements show a significant reduction of the wake velocity deficit for the investigated actuator geometry with an injection mass flow of less than 1% of the passage mass flow. Based on these results a position in the wake was chosen which is representative for the actuation impact on the velocity deficit. There, a hot-wire-probe measurement serves as the controlled variable. A family of linear dynamic black-box models was identified from experimental data to account for nonlinear and unmodelled effects. Static nonlinearitiy was compensated for by a Hammerstein model to reduce the model uncertainty and get a higher controller performance. To handle off-design conditions, a robust controller working in a range of Reynolds numbers from 5x10(5) to 7x10(5) was synthesized. The task of the controller is to rapidly regulate the controlled variable to a reference velocity by changing the blowing amplitude. The synthesized robust controller was successfully tested in closed-loop experiments with good results in reference tracking for pulse series up to 20 Hz. This translates into a much higher frequency when scaled to the dimension of a real machine.
引用
收藏
页数:12
相关论文
共 50 条
  • [21] Control of the flow in the near wake of an airfoil at full stall using fixed trailing-edge plates
    Ozkan, Gokturk M.
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 122
  • [22] Closed-loop active flow control systems: Actuators
    Seifert, A.
    Active Flow Control, 2007, 95 : 85 - 102
  • [23] Influence of trailing-edge flow control on airfoil performance
    Gai, SL
    Palfrey, R
    JOURNAL OF AIRCRAFT, 2003, 40 (02): : 332 - 337
  • [24] Aeroelastic control of wind turbine blade using trailing-edge flap
    Li, Nailu
    Balas, Mark
    WIND ENGINEERING, 2014, 38 (05) : 549 - 560
  • [25] Wake-aerofoil interaction noise control with trailing-edge serrations
    Liu, X.
    Zang, B.
    Azarpeyvand, M.
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2022, 130
  • [26] Trailing-edge flap flow control for dynamic stall
    Green, R. B.
    Gillies, E. A.
    Wang, Y.
    AERONAUTICAL JOURNAL, 2011, 115 (1170): : 493 - 503
  • [27] Influence of trailing-edge flow control on airfoil performance
    Gai, S.L., 1600, American Inst. Aeronautics and Astronautics Inc. (40):
  • [28] Vortex breakdown on pitching delta wing: Control by intermittent trailing-edge blowing
    Vorobieff, PV
    Rockwell, DO
    AIAA JOURNAL, 1998, 36 (04) : 585 - 589
  • [29] Numerical study on closed-loop control of transonic buffet suppression by trailing edge flap
    Gao, Chuanqiang
    Zhang, Weiwei
    Ye, Zhengyin
    COMPUTERS & FLUIDS, 2016, 132 : 32 - 45
  • [30] Iterative Learning Control for Trailing-Edge Flap Lift Enhancement with Pulsed Blowing
    Cai, Zhonglun
    Angland, David
    Zhang, Xin
    Chen, Peng
    AIAA JOURNAL, 2015, 53 (07) : 1969 - 1979