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Keyphrases
Active-passive
100%
Rotor Blade
100%
Hybrid Optimization
100%
Trailing Edge Flap
100%
Passive Hybrid
100%
Hybrid Design
100%
Active Flap
80%
Control Effort
60%
Vibration Reduction
40%
Structural Optimization
40%
Process Optimization
20%
Hybrid Method
20%
Control Input
20%
Physical Understanding
20%
Passive Approach
20%
Controller Design
20%
Off-design Condition
20%
Helicopter Rotor
20%
Design Procedure
20%
Flap Deflection
20%
Flight Range
20%
Aeroelastic Model
20%
Blade Configuration
20%
Effective Design
20%
Vibratory Loads
20%
Hybrid Approach
20%
Engineering
Trailing Edge
100%
Flaps
100%
Rotor Blade
100%
Aircraft Control
33%
Parametric Study
16%
Hybrid Method
16%
Control Input
16%
Design Method
16%
Objective Function
16%
Controller Design
16%
Helicopter Rotors
16%
Hybrid Approach
16%
Design Condition
16%
Vibration Reduction
16%
Retro-Fitting
16%
Design Procedure
16%
Hub Load
16%
Baseline Blade
16%
Vibratory Loads
16%
Optimal Control
16%