Aeroelastic Stability Enhancement and Vibration Suppression in a Composite Helicopter Rotor
Author:
Affiliation:
1. Indian Institute of Science, Bangalore 560 012, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.5652
Reference37 articles.
1. Rotary Wing Aeroelasticity-A Historical Perspective
2. Review of State of Art of Smart Structures and Integrated Systems
3. Aeroelastic optimization of a helicopter rotor with composite coupling
4. Structural Optimization for Vibratory Loads Reduction of Composite Helicopter Rotor Blades with Advanced Geometry Tips
5. A Coupled Rotor/Wing Optimization Procedure for High Speed Tilt-Rotor Aircraft
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