Application of adaptive technology to static aeroelastic control of wing structures
THE INFLUENCE OF CONTROL SYSTEM DESIGN ON THE PERFORMANCE OF VIBRATORY GYROSCOPES
Free vibration of elastically supported thin cylinders including gyroscopic effects
Power Flow and Consumption in Piezoelectrically Actuated Structures
Enhanced Structural Control with Discretely Attached Induced Strain Actuators
Performance and Optimization of Induced Strain Actuated Structures Under External Loading
Enhancing Induced Strain Actuator Authority Through Discrete Attachment to Structural Elements
Design of Displacement-Amplified Induced-Strain Actuators for Maximum Energy Output
Impedance-based modelling of induced strain actuators bonded on ring structures (sv960764)
Modeling Considerations for In-Phase Actuation of Actuators Bonded to Shell Structures