Investigation of Particle Trajectory in Solid Rocket Motor
Track Occupied Identification Method Based on Switch Curve Information
Thermal Stresses In Piezoelectric Materials: A Boundary Integral Formulation
Large eddy simulation of flow transition in a supersonic flat-plate boundary layer
Large Eddy Simulation of Flow Transition in a Supersonic Flat-Plate Boundary Layer
Spectral Properties of High-Power Distributed Bragg Reflector Lasers
Scaling up the Accuracy of k-Nearest-Neighbour Classifiers: A Naive-Bayes Hybrid
AIAA-2007-1186 PRANDTL/SCHMIDT NUMBER EFFECT ON TEMPERATURE DISTRIBUTION IN A MODEL COMBUSTOR
Architecture of a multiprocessor system for Hartmann-Shack wavefront sensor [1920-28]
Sensitivity Improved SPR Biosensor Based on the MoS2/Graphene–Aluminum Hybrid Structure
Small space target detection based on feature stability algorithm [8196-23]
Accounting for combustion mode switch dynamics and fuel penalties in drive cycle fuel economy
Impact of Power Grid Strength and PLL Parameters on Stability of Grid-Connected DFIG Wind Farm
Research and Application of Meta-Learning Based ITMS System
Space Atomic Oxygen Erosion Effects on Epoxy and Silicone Adhesives Used in LEO Spacecraft
Blind Density-Peak-Based Modulation Format Identification for Elastic Optical Networks
Measurements in a Combustor Operated on Alternative Liquid Fuels
In-Flight Aerodynamic and Mass Properties Identification Design for Mars Aerobraking (AAS 13-407)
LES for Interaction of Wingtip Vortex and Wakes AIAA Paper
Optimal Trajectory Design for Aerobraking (AAS 13-332)
Human Detection and Tracking within Hostile Aquatic Environments
Transonic Flow Field Around the CF-18 Wing at Angle of Attack 4.5^o
Ethanol detection in flex-fuel direct injection engines using in-cylinder pressure measurements
Aeroelastic Analysis of Composite Wing with Control Surface
Study of effect of different methanol and gasoline ratio on engine comprehensive performance
Effects of Particle Size on Microstructure of the Matrix Alloy in Aluminium Matrix Composites
Numerical Simulations of Laminar-Turbulent Transition In Supersonic Boundary Layer
Head Modeling Using Color Unequal Phase Stepping Method