;Partial Contents: Generalized Dynamic Wake Model Applied to Helicopter Pitching and Rolling Maneuver; Active Damping with Adaptive Feedback Control in Time Domain for Dynamical Systems with Light Dan; Contact Process and Friction Analysis of Linear Ultrasonic Motor; Penalty Function Method Applied to Numerical Aerodynamic Optimization; Simulation of Hypersonic Non Equilibrium Flow Using Hybrid Grids; Unstructured Grid Generation Algorithm and Its Numerical Simulations; Grid Generation Method Using Prescribed Mesh Modules; Analysis of Boundary Layer Stability for Non-Parallic Flow with Pressure Gradient; Longitudinal Flight Control and Guidance Law Design for Trans-aerosphere Vehicle; Calculation of Three-Dimensional Rotational Effect on Blade Aerodynamic Characteristics; Direct Control of Aeroengine Thrust Based on Correlation Analysis and Neural Networks; Numerical Simulations of Energy Absorption Capability of Composite Components.
Journal of Nanjing University of Aeronautics and Astronautics, Volume 37, Number 2, April 2005
2005
144 pages
Report
Keine Angabe
Englisch