scholarly journals Numerical Simulation of an Active Feedback Control of Sheet Flutter in a Narrow Passage

2007 ◽  
Vol 1 (3) ◽  
pp. 570-582 ◽  
Author(s):  
Masahiro WATANABE ◽  
Yutaka KOYAMA
Keyword(s):  
Numerical Simulation ◽  
Feedback Control ◽  
Active Feedback ◽  
Narrow Passage ◽  
Active Feedback Control

Active Feedback Control of Leakage-Flow-Induced Sheet Flutter by Injection and Suction of Fluid at Inlet or Outlet of Passage

2006 ◽  
Author(s):  
Masahiro Watanabe ◽  
Yutaka Koyama
Keyword(s):  
Feedback Control ◽  
Flow Velocity ◽  
The Self ◽  
Control Technique ◽  
Critical Flow ◽  
Leakage Flow ◽  
Critical Flow Velocity ◽  
Active Feedback ◽  
Narrow Passage ◽  
Active Feedback Control

This paper proposes and develops a new non-contact active feedback control of leakage-flow-induced sheet flutter in a narrow passage, by injection and suction of fluid at inlet or outlet of the passage. The strategy of this active control technique is that the active feedback, which is by the activation of the injection/suction of the fluid at the inlet or outlet of the passage, suppresses the original source of the self-exciting fluid force acting on the structure, i.e., cancels the self-excited feedback mechanism. In this paper, the effective suppression of the leakage-flow-induced sheet flutter by the active feedback control technique is demonstrated experimentally. A flexible sheet, as a controlled object, is subjected to fluid flow in a narrow passage. The leakage-flow-induced flutter occurs to the flexible sheet in the translational motion over the critical flow velocity. The leakage-flow-induced sheet flutter is actively controlled and suppressed by the activation of injection/suction of the fluid at the inlet or outlet of the passage. The critical flow velocity under the controlled condition is examined with varying the controller gain and phase-shift between the injection/suction of the fluid and the sensor (vibration displacement) signal of the flexible sheet. As a result, it is indicated experimentally that the active feedback control technique increases the critical flow velocity, and suppress the leakage-flow-induced sheet flutter effectively. Moreover, the control performance is examined experimentally, and stabilization mechanism by the active feedback control is discussed.

Feedback Control of Turbulence

1994 ◽  
Vol 47 (6S) ◽  
pp. S3-S13 ◽  
Author(s):  
Parviz Moin ◽  
Thomas Bewley
Keyword(s):  
Feedback Control ◽  
Turbulent Flows ◽  
Systems Approach ◽  
Stokes Equations ◽  
Navier Stokes ◽  
Small Scale ◽  
Flow Equations ◽  
Active Feedback ◽  
Active Feedback Control ◽  
Mathematical Techniques

A brief review of current approaches to active feedback control of the fluctuations arising in turbulent flows is presented, emphasizing the mathematical techniques involved. Active feedback control schemes are categorized and compared by examining the extent to which they are based on the governing flow equations. These schemes are broken down into the following categories: adaptive schemes, schemes based on heuristic physical arguments, schemes based on a dynamical systems approach, and schemes based on optimal control theory applied directly to the Navier-Stokes equations. Recent advances in methods of implementing small scale flow control ideas are also reviewed.

Nonlinear Control of Axisymmetric Swirling Flows in a Long Finite-Length Pipe

2015 ◽  
Vol 138 (2) ◽  
Author(s):  
Lei Xu ◽  
Zvi Rusak ◽  
Shixiao Wang ◽  
Steve Taylor
Keyword(s):  
Reynolds Number ◽  
Feedback Control ◽  
High Reynolds Number ◽  
Vortex Breakdown ◽  
Basin Of Attraction ◽  
Swirling Flows ◽  
Active Feedback ◽  
Active Feedback Control ◽  
High Reynolds ◽  
Control Methodology

Feedback stabilization of inviscid and high Reynolds number, axisymmetric, swirling flows in a long finite-length circular pipe using active variations of pipe geometry as a function of the evolving inlet radial velocity is studied. The complicated dynamics of the natural flow requires that any theoretical model that attempts to control vortex stability must include the essential nonlinear dynamics of the perturbation modes. In addition, the control methodology must establish a stable desired state with a wide basin of attraction. The present approach is built on a weakly nonlinear model problem for the analysis of perturbation dynamics on near-critical swirling flows in a slightly area-varying, long, circular pipe with unsteady changes of wall geometry. In the natural case with no control, flows with incoming swirl ratio above a critical level are unstable and rapidly evolve to either vortex breakdown states or accelerated flow states. Following an integration of the model equation, a perturbation kinetic-energy identity is derived, and an active feedback control methodology to suppress perturbations from a desired columnar state is proposed. The stabilization of both inviscid and high-Re flows is demonstrated for a wide range of swirl ratios above the critical swirl for vortex breakdown and for large-amplitude initial perturbations. The control gain for the fastest decay of perturbations is found to be a function of the swirl level. Large gain values are required at near-critical swirl ratios while lower gains provide a successful control at swirl levels away from critical. This feedback control technique cuts the feed-forward mechanism between the inlet radial velocity and the growth of perturbation's kinetic energy in the bulk and thereby enforces the decay of perturbations and eliminates the natural explosive evolution of the vortex breakdown process. The application of this proposed robust active feedback control method establishes a branch of columnar states with a wide basin of attraction for swirl ratios up to at least 50% above the critical swirl. This study provides guidelines for future flow control simulations and experiments. However, the present methodology is limited to the control of high-Reynolds number (nearly inviscid), axisymmetric, weakly nonparallel flows in long pipes.

Active Feedback Control Using Adaptive Filtering

2004 ◽  
Vol 10 (1) ◽  
pp. 25-38
Author(s):  
Fenglin Wang ◽  
Chris K Mechefske
Keyword(s):  
Feedback Control ◽  
Closed Loop ◽  
Noise Control ◽  
Active Noise Control ◽  
Experimental Studies ◽  
Loop Control ◽  
Active Noise ◽  
Active Feedback ◽  
Loop Control System ◽  
Active Feedback Control

In this paper we apply a filtered-X algorithm to an active feedback control structure and derive the transfer function of a closed-loop control system. Simulation studies are then carried out on the closed-loop property while varying the parameters (input frequency, delays in plant, amplitude and phase of modeling filter). Several properties of adaptive feedback control are revealed. Experimental studies on feedback active noise control of noise in a finite duct and a small enclosure are described, and outstanding active noise control effects are achieved. Experimental results of closed-loop frequency response are also provided.

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