218/2011

Spis treści:

1. Implementation of Flight Tests in Order to Develop new Flight Techniques for Takeoffs and Landing in a Limited Space for Helicopter W-3A SOKÓŁ
   Chołożyński E.
2. Study of the Influence of Helicopter’s External Components on the Aerodynamic Characteristics
   Dziubiński A., Grzegorczyk K.
3. CFD Analysis of External Armour Influence on a Helicopter Aerodynamic Characteristics
   Dziubiński A., Grzegorczyk K., Żółtak J.
4. Excitation of a Localized Nonlinear Normal Mode of a Bladed Disc Assembly Lump Mass Nonlinear Model
   Georgiades F., Warmiński J.
5. Mode Shapes Variation of a Composite Beam with Piezoelectric Patches
   Latalski J., Georgiades F., Warminski J.
6. Vibration and Damage Detections of Composite Beams with Defects
   Monoach E., Mitura A., Samborski S., Warmiński J.
7. Rotor Blade Segment with Piezoactuated Trailing-Edge Flap for Dynamic Pressure Measurements
   Miller M.
8. The Numerical Analysis of Properties of the Trailing-Edge Flap on the ILH412M-S Rotor Blade Airfoil
   Miller M., Stalewski W.
9. Vibration Testing of a Helicopter Main Rotor Composite Blade
   Parafiniak M., Skalski P.
10. Possibilities of Improvement of Directional Control Effectiveness of Light Gyroplane at High-Angle-Of-Attack Flight Conditions
    Stalewski W., Sznajder J.
11. Effectiveness of an Inverted-V-Shaped Control Surfaces of a Gyroplane at Low Speed and High Angles of Attack
    Sznajder J.