Well-aligned CuO nanowires detached from Cu foil by a simple contact printing method
Virtual Network Embedding With Adaptive Modulation in Flexi-Grid Networks
Vibration control for active seat suspension system based on projective chaos synchronisation
Upgrade Desiqn of the Yuchai F-6113 HD-DI Diesel Engine
Upconversion phenomenon in Tm^3^+-doped tellurite glass [5061-32]
Ultrafast time-resolved optical multichannel analyzer [2321-53]
Two Approaches to Improve FPGA Performance for the Stereo Camera of the Chang'E-1 Satellite
The Practice of Parking Management in Adelaide
Theory and Technology for Standard WiMAX Over Fiber in High Speed Train Systems (Invited Paper)
Theory and Technology for Standard WiMAX Over Fiber in High Speed Train Systems
The influence of flight altitude on supersonic drag reduction with laser energy depositions
THE CONVERSATION ANALYSIS OF AVIATION ENGLISH FROM SYSTEMIC FUNCTIONAL LINGUISTICS PERSPECTIVES
Study on ISAR Imaging of Stepped-Frequency Chirp Signal
Study on Control Strategy of Ignition Advanced Angle of Electronic Control Motorcycle Engine
Strong motion observations and recordings from the great Wenchuan Earthquake
Spun-Related Effects on Optical Properties of Spun Silica Optical Fibers
Spectroscopic properties of Er^3^+-doped glasses for amplifiers [4990-28]
Simulation Study for Anti-lock Braking System of a Light Bus
Rotation-invariant photorefractive correlator [2849-33]
Research on Safety Lane Change Model of Driver Assistant System on Highway
Research of Vehicle Scheduling Problem and Algorithm Based on Emergency Needs
Quantized H ∞ fault-tolerant control for networked control systems
Q-switching of 10W fiber coupled diode laser pumped Nd:YAG
Propagation Characteristics of Anisotropic a-Axis Hollow Lithium Niobate Nanowire
Preliminary Study on Configuration of Triple-Wall Shield with Oblique Middle Wall
Preliminary Analysis on Effect of Sleeper Pitch on Rail Corrugation at a Curved Track
Preliminary Analysis on Effect of Sleeper Pitch on Rail Corrugation at a Curved Track
Precise Determination of the Reachable Domain for a Spacecraft With a Single Impulse (AAS 14-371)