Aeroelastic optimization of a helicopter rotor with composite coupling
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46882
Reference20 articles.
1. Aeroelastic Stability Analysis of a Composite Rotor Blade
2. Aeroelastic Response, Loads, and Stability of a Composite Rotor in Forward Flight
3. Air and Ground Resonance of Helicopters with Elastically Tailored Composite Rotor Blades
4. Helicopter vibration reduction using structural optimization with aeroelastic/multidisciplinary constraints - A survey
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