Limit Cycle Oscillation Prediction for Aeroelastic Systems with Discrete Structural Non-Linearities
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
Optimisation of Composite Sensorcraft Structures for Gust Alleviation
Adaptive Aeroelastic Concept Applied to a Civil Jet Aircraft Model
SMorph - Smart Aircraft Morphing Technologies Project
Design of Composite Structures to Improve the Aeroelastic Performance