Active vibration control of aircraft wings modeled as thin-walled composite beams using piezoelectric actuation

Keyphrases

• Aircraft Wing 100%
• Thin-walled Composite Beams 100%
• Active Vibration Control 100%
• Piezoelectric Actuation 100%
• Boundary Moment 66%
• Stiffness 33%
• Control Method 33%
• Transverse Shear Deformation 33%
• Diamond-like 33%
• Beam Model 33%
• Closed-loop 33%
• Velocity Feedback Control 33%
• Piezoelectric Layer 33%
• Bending Shear 33%
• Angle Orientation 33%
• Feedback Control 33%
• Piezoelectric Actuator 33%
• Warping Restraint 33%
• Non-classical Effects 33%
• Transverse Shear 33%
• Ply Angle 33%
• Material Anisotropy 33%
• Coupled Motion 33%
• Fundamental Frequency 33%
• Adaptive Materials 33%
• Dynamical Characteristics 33%
• Vibrational Behavior 33%
• Host Structure 33%
• Proportional Feedback Control 33%
• Lateral Bending 33%
• Active Feedback Control 33%
• Adaptive Change 33%
• Elastic Coupling 33%

Engineering

• Actuation 100%
• Piezoelectric 100%
• Wings 100%
• Thin-Walled Composite Beam 100%
• Active Vibration Control 100%
• Feedback Control 100%
• Cross Section 33%
• Shear Deformation 33%
• Beam Model 33%
• Closed Loop 33%
• Diamond 33%
• Ply Angle 33%
• Material Anisotropy 33%
• Fundamental Frequency 33%
• Directionality 33%
• Control Procedure 33%
• Span Beam 33%
• Host Structure 33%
• Piezoelectric Actuator 33%