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
Flight Testing an Iced Business Jet for Flight Simulation Model Validation AIAA Paper
Development and Application of New Low Rhodium Three-Way Catalyst Technology
2007-01-1504 Real Time Control of Restraint Systems in Frontal Crashes
Real Time Control of Restraint Systems in Frontal Crashes
Adaptive Gust Alleviation for a Tilt-Rotor UAV Operating in Turbulent Airwakes
Optimisation of Composite Sensorcraft Structures for Gust Alleviation
Optimization of a Scaled Sensorcraft Model with Passive Gust Alleviation
Scaling for a Static Nonlinear Response of a Joined-Wing Aircraft
Data-Driven Simulation-Updates of Tiltrotor Aircraft
On-Line Identification of Ship Airwake Disturbances on Rotorcraft