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
A FORM OF AERODYNAMIC ADMITTANCE FOR USE IN BRIDGE AEROELASTIC ANALYSIS
โ Scribed by R.H. SCANLAN; N.P. JONES
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 132 KB
- Volume
- 13
- Category
- Article
- ISSN
- 0889-9746
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