Optimal vibration control of adaptive aircraft wings carrying externally mounted stores and exposed to blast loading

Keyphrases

• Blast Loading 100%
• Aircraft Wing 100%
• Optimal Vibration Control 100%
• Wing Structure 100%
• Anisotropy 50%
• Sensing Capability 50%
• Host Structure 50%
• Transverse Shear 50%
• External Excitation 50%
• Quadratic Performance Index 50%
• Piezoelectric Actuator 50%
• Closed Cross-section 50%
• Vibration Control 50%
• Input Power 50%
• Piezoelectric Devices 50%
• Control Efficacy 50%
• Nonclassical Feature 50%
• External Store 50%

Engineering

• Vibration Control 100%
• Wings 100%
• Blast Loading 100%
• Sensing Capability 33%
• Piezoelectric Device 33%
• Constituent Material 33%
• Input Power 33%
• Closed Cross Section 33%
• Host Structure 33%
• Piezoelectric Actuator 33%

Material Science

• Aircraft 100%
• Anisotropy 50%
• Piezoelectricity 50%
• Performance Index 50%