Surface actuated variable-camber and variable-twist morphing wings using piezocomposites

Keyphrases

• Airfoil 100%
• Piezocomposite 100%
• Morphing Wing 100%
• Variable Camber 100%
• Twist Morphing 100%
• Variable Twist 100%
• Geometric Features 50%
• Substrate Material 50%
• Geometric Parameters 50%
• Fluid-structure Interaction 50%
• Piezoelectric Ceramics 50%
• Macro Fiber Composite 50%
• Bimorph 50%
• Aerodynamic Loads 50%
• Response Characterisation 50%
• Lift Coefficient 50%
• Composite Actuator 50%
• Variable Camber Airfoil 50%
• Host Material 50%
• Trailing Edge 50%
• Active Surface 50%
• Compliant Hinge 50%
• Static Aeroelastic 50%
• Coupled Treatment 50%
• Camber Line 50%
• Camber Morphing 50%
• Aeroelastic Response 50%
• Morphing Airfoil 50%
• Airfoil Shape 50%
• Single Substrate 50%
• Lift-to-drag Ratio 50%
• Fluid-structure Interaction Problems 50%
• Optimized Location 50%
• Smooth Deformation 50%
• Bimorph Actuator 50%
• Airfoil Surface 50%

Engineering

• Airfoil 100%
• Boundary Condition 75%
• Fluid-Structure Interaction 50%
• Realization 25%
• Structural Parameter 25%
• Geometric Feature 25%
• Substrate Material 25%
• Composite Fiber 25%
• Parametric Study 25%
• Trailing Edge 25%
• Piezoceramics 25%
• Aerodynamic Load 25%
• Lift Coefficient 25%
• Geometric Parameter 25%
• Active Surface 25%
• Airfoil Shape 25%
• Camber Morphing 25%
• Camber Line 25%
• Lift to Drag Ratio 25%
• Airfoil Surface 25%