0-3 nanocomposites for optoelectronics and nonlinear optics (Invited Paper) [2321-04]
1.3-m separate confinement lasers [2321-98]
1.5T High Thermal Efficiency Modular Engine Platform
3-D Reconstruction of Shaded Objects from Multiple Images Under Unknown Illumination
8 x 8, 0.88-m wavelength of LED matrix module [2321-40]
18:54 WIPD1-3 Evanescent Wave Gas Sensing Using Microstructure Fibre
2001-01-3266 Polytopic Dynamics and Control for Variable Suspension System
2003-01-0327 Failure Mechanisms of Sandwich Specimens With Epoxy Foam Cores Under Bending Conditions
2005-01-1596 Dead Pedal and the Perception of Performance of a Continuously Variable Transmission
2007-01-1647 Effects of Braking on Suspension Loads in Potholes
2008-01-0352 Alternative Airbag Evaluation Methodology through Cold Gas Inflation System
A computer-aided simulation approach for mechanisms with time-varying topology
Active interferometers for shape and deformation measurements (Invited Paper) [2321-47]
Active Noise Control Method Considering Auditory Characteristics
Advanced Energy Management Strategies for Range Extended Electric Vehicle
Advanced Solid Lubricant Technology Improve Engine Performance
Advanced Solid Lubricant Technology Improve Engine Performance
Aerodynamic Numerical Simulation for EMU Passing Each Other in Tunnel
Aerodynamics on Flapping Rotary Wing in Low Reynolds Number
A Fast Finite Element Analysis of Millimeter Wave Waveguide Filters
A high-fidelity co-simulation platform for motion and control research for vehicle platooning
A Holistic Solution to the Bi-Link-Failure-Free RWA Problem for 2-D-Torus-Based WDM LANs
A Holistic Solution to the Bi-Link-Failure-Free RWA Problem for 2-D-Torus-Based WDM LANs
AIAA-2001-1566 Shape Estimation of Deforming Structures
AIAA 2006-0730 Advancement of a Collaboration Pursuing Method (CPM)
AIAA-2006-1713 Collaboration Pursuing Method Using Latin Hypercube Sampling
AIAA-2007-1238 EXPERIMENTAL RESEARCH ON SUPERSONIC COMBUSTION IN RESISTANCE HEATED FACILITY
AIAA-2007-1355 INVESTIGATION OF HYDROCARBON-FUEL IGNITION AND COMBUSTION IN SCRAMJET COMBUSTOR
Aircraft recognition in infrared image using wavelet moment invariants