93F006 Supply Chains: The Challenge of Managing Variety and Complexity
2007-01-1504 Real Time Control of Restraint Systems in Frontal Crashes
Adaptive Aeroelastic Concept Applied to a Civil Jet Aircraft Model
Adaptive Gust Alleviation for a Tilt-Rotor UAV Operating in Turbulent Airwakes
Addressing gaps in the availability of travel behaviour data
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
A Sense and Avoid System for Unmanned Aircraft in Formation Flight (AIAA 2014-0967)
Consumer response to sustainable planning and transport policy initiatives
Data-Driven Simulation-Updates of Tiltrotor Aircraft
Delivering Multimedia Content to Automobiles Using Wireless LANs
Densification and Urban Compaction: Reinforcing the Drive for Sustainability
Design of Composite Structures to Improve the Aeroelastic Performance
Development and Application of New Low Rhodium Three-Way Catalyst Technology
Development of a Dual-Frequency GNSS Receiver for Scientific Applications
Development of Smart Spars for Active Aeroelastic Structures
Drag Minimisation Using Adaptive Aeroelastic Structures AIAA Paper 2007-1710 CD-ROM Number 7
Effectiveness of Real Time Control for Active Restraint Systems in Frontal Crashes
Efficient Prediction of Aeroelastic Response Including Geometric Non-Linearities
Experimental Investigation of an All-Movable Vertical Tail Model
Flight Testing an Iced Business Jet for Flight Simulation Model Validation AIAA Paper
Force Appropriation for Flight Flutter Testing Using SMART Devices
Frequency-Domain Method for Automated Simulation Updates based on Flight Data
Improved Implementation of the Harmonic Balance Method AIAA Paper 2007-2359 CD-ROM Number 7
Integrated Methods to Model and Update Rotorcraft Simulations with Experimental Data
Investigation of Flight Loads Prediction using Multi-Body Simulation