Aeromechanics and Aeroelastic Stability of Coaxial Rotors
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109-2140
Funder
FXB Center for Rotary and Fixed Wing Air Vehicle Design at University of Michigan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036291
Reference27 articles.
1. Investigation of Maximum Blade Loading Capability of Lift-Offset Rotors
2. Aeromechanics of Rigid Coaxial Rotor Models for Wind-Tunnel Testing
3. Hingeless Rotor Aeroelastic Stability Analysis with Refined Aerodynamic Modeling
4. Rotary-Wing Aeroelasticity: Current Status and Future Trends
5. Coupled Flap‐Lag‐Torsional Dynamics of Hingeless Rotor Blades in Forward Flight
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