Adaptive Aeroelastic Concept Applied to a Civil Jet Aircraft Model
Aeroelastic Flight Control for Subscale UAVs AIAA Paper 2007-1706 CD-ROM Number 7
AIAA-2004-1883 Development of an Adaptive Stiffness All-Moving Vertical Tail
AIAA-2004-1884 Experimental Validation of Wing Twist Control Using Adaptive Internal Structures
AIAA-2006-2023 Application of Higher-Order Harmonic Balance to Non-Linear Aeroelastic Systems
AIAA-2006-2131 On the Use of Adaptive Internal Structures to Optimise Wing Lift Distributions