Keyphrases
Bending Moment
100%
Trailing Edge Flap
100%
Composite Rotor Blade
100%
Rotor Blade
75%
Control Method
50%
Control Input
50%
Process Optimization
25%
Steady State
25%
Numerical Simulation
25%
Aerodynamics
25%
Helicopter
25%
Forward Flight
25%
Blade Structure
25%
Active Control
25%
Advance Rate
25%
Composite Rotor
25%
Flap Deflection
25%
Flap Control
25%
Active Flap
25%
Aeroelastic Model
25%
Hybrid Design
25%
Design Yield
25%
Rigid Blade
25%
Engineering
Trailing Edge
100%
Flaps
100%
Rotor Blade
100%
Active Load
100%
Load Control
100%
Bending Moment
66%
Hub Load
50%
Control Input
33%
Harmonics
16%
Rotors
16%
Computer Simulation
16%
Significant Change
16%
Optimal Control
16%
Objective Function
16%
Forward Flight
16%
Blade Element
16%
Active Control
16%