;Contents: Some Doubts in Helicopter Aerodynamics; Investigation of Helicopter Longitudinal Control Response Based on ADS-33 Requirements; Design and Experiment of Lift Transfer in Scheme of High-Speed Helicopter; Prediction of Aerodynamic Interactions of Helicopter Fuselage on its Rotor; Aeroelastic Stability Analysis of Helicopter Rotor Blade with Swept Tips; Experimental Research on Adaptive Internal Model Control Simulation for Helicopter Cabin Noise; A Method for Designing Attitude Controller Based on Fuzzy Control; Ground Resonance Analysis of Helicopter with Magnetorheological Lag Damper; Unsteady Rotor Airload Prediction using a Comprehensive Aeroelastic Analysis; Theoretical Analysis of Rotational Noise in Hovering Rotors; Flight Dynamics Model and Stability Augment Design for a Small-Size Unmanned Helicopter; On-off Control for Ground Resonance of Helicopter using Inter-Connected Blade Magnetorheological Dampers; A Time-Domain Methodology for Identifying Model Parameters of Elastomeric Lag Dampers; Some Problems on Active Control of Structural Vibration for Helicopter; Influence of Downwash Flow on Launching Missile on Armed Helicopter Main Rotor; Experimental Study of Rotor Unsteady Aerodynamic Loads; Active Sliding Model Control of Vibration in a Class of Nonlinear Systems; Improvements of a Finite Volume Method for Euler Equations on Unstructured Meshes; Experimental Research of Jettison of Aircraft External Store in Low Speed Wind Tunnel; Aerodynamic Optimization Design of Micro Air Vehicle Propeller; Research of Multi-Restrict Airline Schedule Optimization Model and Method; Filament Winding Pattern Design for Composite Elbow; and Advances in Computational Fluid Dynamics of Helicopter Rotor.


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    Titel :

    Journal of Nanjing University of Aeronautics and Astronautics, Volume 35, Number 3, 2003


    Beteiligte:
    L. Dewang (Autor:in)

    Erscheinungsdatum :

    2003


    Format / Umfang :

    130 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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