Aerodynamic and Thrust Force Modeling for a Propulsion Assisted Control Aircraft Test Bed
Aerodynamic and Thrust Force Modeling for a Propulsion Assisted Control Aircraft Test Bed
AIAA-2006-1736 Aeroelastic Analysis of an Airfoil with a Hysteresis Non-Linearity
Design Optimization of Composite Laminated Plates with Sub-Layer Variable Method
Development of a GPS/INS Sensor Fusion Simulation Environment Using Flight Data
Development of New Generation Turbine Disk Superalloys in the HTM21 Project
Dynamic Pressure Perturbation Method for Flutter Solution: The Mu-Omega Method
Generalized Mu-Omega Method with Complex Perturbation to Dynamic Pressure
High-gain high-speed low-noise single-avalanche-stage APDs
In Situ Measurement on the Pressure and Resin Flow in Hot Press Process of Composites
Nonlinear Aircraft Model Identification and Validation for a Fault-Tolerant Flight Control System