Dynamic Stability of a Rotor Blade Using Finite Element Analysis
Author:
Affiliation:
1. Stanford University, Stanford, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.51129
Reference16 articles.
1. Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in Hover
2. On the Nonlinear Deformation Geometry of Euler-Bernoulli Beams.
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3. New Method for Analyzing the Flutter Stability of Hingeless Blades with Advanced Geometric Configurations in Hovering;International Journal of Aerospace Engineering;2020-02-17
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