Aeroelastic analysis of multibladed hingeless rotors in hover
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Taejon 305-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12990
Reference25 articles.
1. Rotary-wing aeroelasticity with application to VTOL vehicles
2. Rotor Blade Wake Flutter—A Comparison of Theory and Experiment
3. Experimentally Determined Flutter from Two‐ and Three‐Bladed Model Bearingless Rotors in Hover
4. Stability of Hingeless Rotors in Hover Using Three‐Dimensional Unsteady Aerodynamics
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2. Unsteady Aerodynamic Stabilization of the Dynamics of Hingeless Rotor Blades in Hover;AIAA Journal;2018-03
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