Adjoint-based Shape and Kinematics Optimization of Flapping Wing Propulsive Efficiency
A Feasibility Study of the Use of Axisymmetric Thrust Vectoring for Enhanced In-Flight Simulation
AIAA 2006-1309 Azimuthal Vorticity Dynamics and Vortex Breakdown Above a Delta Wing
AIAA-2006-6084 A New Off-Axis Laser Beamrider Missile Guidance Algorithm
An Object-Oriented Mission Control System Development: Report on Scos-II
An Object-Oriented Mission Control System Development: Report on SCOS-II
Appearance-Based Structure from Motion Using Linear Classes of 3-D Models
A Quasi-3-D Theory for Impedance Eduction in Uniform Grazing Flow AIAA Paper 2005-2848
A Special Oil Recovery Tug: The SORT 33 - A New Tug with a Mission
Brillouin Properties of a Novel Strontium Aluminosilicate Glass Optical Fiber (Invited Paper)
Can railway station design reduce the risk of a terrorist attack or the impact of an incident?
Comparison of RVR System Estimates and Human Observations Under Category IIIb Conditions
Comparison of Simulator Platform and Flight Tasks on Adverse Rotorcraft Pilot Coupling Prediction
Cost Reduction Through Application of Fieldbus Technology to Space Mission Operation and Control
Design for Assembly - A Strategy for Right First Time Design
Detecting Pedestrians Using Patterns of Motion and Appearance
Development of a Low-Emission, Dedicated Ethanol-Fuel Vehicle with Cold-Start Distillation System
Dynamics of the Vortex Core During Pitching of a High-Sweep Delta Wing AIAA Paper
ESA Software Engineering Standards and ISO 9001: Theory and Practice
ESA Software Engineering Standards and ISO 9001: Theory and Practice
EVALUATION OF A SLUNG LOAD CONTROL SYSTEM FOR PILOTED OFFSHORE WINCHING OPERATIONS
EVALUATION OF A SLUNG LOAD CONTROL SYSTEM FOR PILOTED OFFSHORE WINCHING OPERATIONS
Evaluation of Simulator Cueing Fidelity for Rotorcraft Certification by Simulation
Evaluation of Simulator Cueing Fidelity for Rotorcraft Certification by Simulation
Fatigue and Damage Tolerance Design of Large Airbus Wing Structures
Fiber optic pressure/skin friction gage for supersonic flow applications
Fiber Optic Pressure/Skin Friction Gage for Supersonic Flow Applications
Flight Test of Scaled MTEs for VTOL Certification Using an Ultralight Coaxial Helicopter
Flight Test of Scaled MTEs for VTOL Certification Using an Ultralight Coaxial Helicopter
Fuzzy Control of a Tensegrity based Morphing UAV Wing