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
Aeroelastic Flight Control for Subscale UAVs AIAA Paper 2007-1706 CD-ROM Number 7
Drag Minimisation Using Adaptive Aeroelastic Structures AIAA Paper 2007-1710 CD-ROM Number 7
Efficient Prediction of Aeroelastic Response Including Geometric Non-Linearities
Adaptive Aeroelastic Concept Applied to a Civil Jet Aircraft Model
SMorph - Smart Aircraft Morphing Technologies Project
Rapid Prediction of Worst Case Gust Loads Following Structural Modification
Design of Composite Structures to Improve the Aeroelastic Performance
Receptance Based Active Aeroelastic Control Using Multiple Control Surfaces