Nonlinear analysis and enhancement of wing-based piezoaeroelastic energy harvesters

Engineering

• Nonlinear Analysis 100%
• Load Resistance 100%
• Aerodynamic Load 100%
• Harvester 100%
• Piezoelectric 50%
• Degree of Freedom 50%
• Fourth Order 50%
• Corrector 50%
• Lattice Method 50%
• Energy Harvesting 50%
• Aspect Ratio 50%
• Electrical Load 50%
• Pitch Motion 50%
• Aerodynamic Effect 50%
• Couplings 50%
• Vortex 50%
• Transducer 50%

Keyphrases

• Piezoaeroelastic 100%
• Torsion Spring 50%
• Low Aspect Ratio 25%
• Electrical Load 25%
• Coupling Scheme 25%
• Aeroelastic Vibration 25%
• Torsional Eccentricity 25%
• Elastic Axis 25%
• Aerodynamic Effect 25%
• Pitching Motion 25%
• Unsteady Aerodynamic Loads 25%
• Incident Flow 25%