Parametric study of helicopter blade for active twist control incorporating macro fiber composite actuator

Keyphrases

• Helicopter Blade 100%
• Spar 100%
• Active Twist 100%
• Macro Fiber Composite Actuator 100%
• Design Parameters 66%
• Active Method 66%
• Helicopter Rotor Blade 66%
• Fluid Flow 33%
• Rotor 33%
• Reinforced Foam 33%
• Response Surface Methodology 33%
• Airfoil 33%
• Negative Effects 33%
• Parameter Optimization 33%
• Helicopter 33%
• Flow Structure 33%
• Piezo 33%
• Chord Length 33%
• Speed Limit 33%
• Physical Structure 33%
• Capacity Constraints 33%
• Vibration Reduction 33%
• Noise Reduction 33%
• Aerodynamic Loads 33%
• 3D Model 33%
• Load Capacity 33%
• Analogy-making 33%
• Health Monitoring 33%
• Shape Control 33%
• Piezoelectric Effect 33%
• Glass Fiber Reinforced Polymer 33%
• Thermal Strain 33%
• Foam Core 33%
• Interaction Techniques 33%
• Noise Generation 33%
• Forward Speed 33%
• Passive Method 33%
• Two-way Fluid-structure Interaction 33%
• Web Thickness 33%
• Twisted Blade 33%
• Unsteady Aerodynamics 33%
• Higher Harmonic Control 33%
• Aerodynamic Environment 33%
• Circular Fitting 33%
• Individual Blade Control 33%
• Skin Thickness 33%
• Trailing Edge Flap 33%
• Control Monitoring 33%
• Macro Fiber Composite 33%
• Bimorph 33%
• Active Control of Structural Response 33%
• NACA 23012 33%
• Applied Vibration 33%
• Blade Twist 33%
• Strain-induced 33%
• Vibration Suppression 33%
• Torsion Angle 33%
• Load Noise 33%
• Polymeric Core 33%
• Unidirectional Fiberglass 33%
• Vibratory Loads 33%

Engineering

• Parametric Study 100%
• Helicopter Blade 100%
• Composite Fiber 100%
• Active Twist 100%
• Helicopter Rotors 50%
• Rotor Blade 50%
• Design Parameter 50%
• Similarities 25%
• Fluid Flow 25%
• Illustrates 25%
• Health Monitoring 25%
• Rotors 25%
• Airfoil 25%
• Negative Effect 25%
• Flaps 25%
• Fluid-Structure Interaction 25%
• Flow Structure 25%
• Response Surface Methodology 25%
• Structural Response 25%
• Active Control 25%
• Chord Length 25%
• Capacity Limitation 25%
• Aerodynamic Load 25%
• Physical Structure 25%
• Load Capacity 25%
• Piezoelectric Effect 25%
• Thermal Strain 25%
• Foam Core 25%
• Trailing Edge 25%
• Vibratory Loads 25%
• Forward Speed 25%
• Speed Limitation 25%
• Reinforced Plastic 25%
• Harmonics 25%