Dynamic Pressure Perturbation Method for Flutter Solution: The Mu-Omega Method
Development of New Generation Turbine Disk Superalloys in the HTM21 Project
Development of a GPS/INS Sensor Fusion Simulation Environment Using Flight Data
Design Optimization of Composite Laminated Plates with Sub-Layer Variable Method
AIAA-2006-1736 Aeroelastic Analysis of an Airfoil with a Hysteresis Non-Linearity
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