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Model validation and controller design for vibration suppression of flexible rotor using AMB

โœ Scribed by Jeon, Soo ;Ahn, Hyeong-Joon ;Han, Dong-Chul


Publisher
Springer-Verlag
Year
2002
Tongue
Korean
Weight
784 KB
Volume
16
Category
Article
ISSN
1226-4865

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OPTIMUM DESIGN OF A HELICOPTER ROTOR FOR
โœ R. GANGULI ๐Ÿ“‚ Article ๐Ÿ“… 2002 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 604 KB

An aeroelastic analysis based on finite elements in space and time is used to model the helicopter rotor in forward flight. The rotor blade is represented as an elastic cantilever beam undergoing flap and lag bending, elastic torsion and axial deformations. The objective of the improved design is to