;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.


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    Titel :

    Journal of Nanjing University of Aeronautics and Astronautics, Volume 37, Number 2, April 2005


    Beteiligte:
    L. Dewang (Autor:in)

    Erscheinungsdatum :

    2005


    Format / Umfang :

    144 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch