Active vibration control applications for adaptive aircraft wings modelled as thin-walled composite beams

Keyphrases

• Aircraft Wing 100%
• Control Applications 100%
• Thin-walled Composite Beams 100%
• Active Vibration Control 100%
• Boundary Moment 66%
• Stiffness 33%
• Transverse Shear Deformation 33%
• Slenderness Ratio 33%
• Beam Model 33%
• Optimal Control 33%
• Closed-loop 33%
• Velocity Feedback Control 33%
• Bending Shear 33%
• Feedback Control 33%
• Warping Restraint 33%
• Non-classical Effects 33%
• Transverse Shear 33%
• Material Anisotropy 33%
• Fundamental Frequency 33%
• Piezoelectric Ceramics 33%
• Adaptive Materials 33%
• Dynamical Characteristics 33%
• Vibrational Behavior 33%
• Host Structure 33%
• Lateral Bending 33%
• Adaptive Change 33%
• Elastic Coupling 33%
• Shear-coupled Motion 33%
• Proportional Feedback 33%
• Thin-walled Beam Theory 33%
• Kite 33%

Engineering

• Wings 100%
• Thin-Walled Composite Beam 100%
• Active Vibration Control 100%
• Feedback Control 66%
• Cross Section 33%
• Piezoelectric 33%
• Shear Deformation 33%
• Beam Model 33%
• Closed Loop 33%
• Material Anisotropy 33%
• Fundamental Frequency 33%
• Directionality 33%
• Span Beam 33%
• Host Structure 33%
• Aspect Ratio 33%
• Optimal Control 33%