期刊文献+

Feedback control of boundary layer Tollmien-Schlichting waves using a simple model-based controller

原文传递
导出
摘要 The attenuation of spatially evolving instability Tollmien-Schlichting(T-S)waves in the boundary layer of a flat plate with zero pressure gradients using an active feedback control scheme is theoretically and numerically investigated.The boundary layer is excited artificially by various perturbations to create a three-dimensional field of instability waves.Arrays of actuators and sensors are distributed locally at the wall surface and connected together via a feedback controller.The key elements of this feedback control are the determination of the dynamic model of the flat plate boundary layer between the actuators and the sensors,and the design of the model-based feedback controller.The dynamic model is established based on the linear stability calculation which simulates the three-dimensional input-output behaviour of the boundary layer.To simplify the control problem,an uncoupled control mode of the dynamic model is made to capture only those dynamics that have greatest influences on the input-output behaviour.A Proportional-Integral-Derivative(PID)controller,i.e.a lead-lag compensator,combining with a standard Smith predictor is designed based on the system stability criterion and the specifications using frequency-response methods.Good performance of the feedback control with the uncoupled control mode is demonstrated by the large reduction of the three-dimensional disturbances in the boundary layer.This simple feedback control is realistic and competitive in a practical implementation of T-S wave cancellation using a limited number of localised sensors and actuators.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2021年第3期25-38,共14页 中国航空学报(英文版)
基金 the support provided by the Open Fund of Key Laboratory of Aerodynamic Noise Control of China(No:1901ANCL20190105)。
  • 相关文献

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部