Location of the Pupil-Iris Border in Slit-Lamp Images of the Cornea
Limit Cycle Oscillation Prediction for Aeroelastic Systems with Discrete Structural Non-Linearities
Force Appropriation for Flight Flutter Testing Using SMART Devices
Development of Smart Spars for Active Aeroelastic Structures
Experimental Investigation of an All-Movable Vertical Tail Model
AIAA-2004-1884 Experimental Validation of Wing Twist Control Using Adaptive Internal Structures
AIAA-2004-1883 Development of an Adaptive Stiffness All-Moving Vertical Tail
AIAA-2006-2131 On the Use of Adaptive Internal Structures to Optimise Wing Lift Distributions
AIAA-2006-2023 Application of Higher-Order Harmonic Balance to Non-Linear Aeroelastic Systems
Improved Implementation of the Harmonic Balance Method AIAA Paper 2007-2359 CD-ROM Number 7