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Active interrogation of helicopter rotor faults using trailing-edge flaps
P. W. Stevens
,
E. C. Smith
Aerospace Engineering
Research output
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Conference article
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peer-review
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Dive into the research topics of 'Active interrogation of helicopter rotor faults using trailing-edge flaps'. Together they form a unique fingerprint.
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Keyphrases
Helicopter Rotor
100%
Trailing Edge Flap
100%
Active Interrogation
100%
Rotor System
50%
Health Monitoring
25%
Numerical Simulation
25%
Rotorcraft
25%
Minimum Size
25%
Stiffness
25%
Actuator
25%
Function-based
25%
Low Amplitude
25%
Centrifugal Force
25%
Discrete Frequency
25%
Aerodynamic Force
25%
Strain-based
25%
Noise Effects
25%
Improved Health
25%
Aerodynamic Damping
25%
Frequency Response Function
25%
Flap Deflection
25%
Engineering
Trailing Edge
100%
Flaps
100%
Helicopter Rotors
100%
Rotor System
50%
Health Monitoring
25%
Computer Simulation
25%
Rotorcraft
25%
Structural Damage
25%
Damage Detection
25%
Centrifugal Force
25%
Good Result
25%
Aerodynamic Force
25%
Aerodynamic Damping
25%
Detection Algorithm
25%
Frequency Response Function
25%