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Control Engineering
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Engineering
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Noise
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Noise Control
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title: Noise Control Engineering Journal
Airfoil–Vortex Interaction Noise Control Mechanism Based on Active Flap Control
Blade-vortex interaction (BVI) noise is a significant source of rotor noise. In recent years, active flap control
...Additively Manufactured Sound-Absorbing Porous Structures for Airfoil Trailing-Edge Noise Control
Numerical Study of Flow and Noise Control Mechanism of Shape-Optimized Series Cylinder
The study addresses the critical issue of noise generation attributed to airflow around cylinders and its
...Passive Control of Vortex Shedding Noise of Circular Cylinders by Passive Air-Jet Blowing
Passive air-jet blowing is an effective yet simple technique to control flow-induced noise due to vortex shedding
...Experimental Study of Far-Field Aerodynamic Noise Characteristics of Serrated Slat
High-lift airfoil slat and passive control noise were studied experimentally. A serrated slat with different
...Toward a Low Noise Shock Tunnel Facility via Multiobjective Optimization of Hypersonic Nozzle
In this paper, a systematic approach is considered for the development of a low noise shock tunnel facility. For
...Parametric Effect of Blade Surface Blowing on the Reduction of Rotor Blade–Vortex Interaction Noise
Analyzing Interaction Noise from a Small Contra-Rotating Fan Enclosed with Lined and Unlined Casings
Robust Flight Control Design Using Sensor-Based Backstepping Control for Unmanned Aerial Vehicles
The sensor-based backstepping control law, which is not sensitive to model uncertainty, uses less model knowledge
...A Case for Feedback Control to Prevent Delay
Active Vibration Control of Time-Varying Structural Systems with a Logic FxLMS Algorithm
The filtered-x least mean square (FxLMS) algorithm has been widely used in active noise and vibration control of
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This paper presents the design and analysis of a robust neural adaptive backstepping control (RNABC) for an
...Adaptive Control of Shock Waves with a Passively Morphing Layer for Rotating Blades
Intelligent Vibration Isolation and Mitigation of a Platform by Using MR and VE Devices
Comparison of Numerical Differentiation Techniques for Aircraft Identification
External disturbance and measurement noise during flight tests inevitably degrade the identification of the
...Mini Quadrotor UAV: Design and Experiment
Twist Suppression Method of Tethered Towing for Spinning Space Debris
Improved LQG Method for Active Gust Load Alleviation