Examination of the flap-lag stability of rigid articulated rotor blades
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio
2. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44643
Reference20 articles.
1. Pitch‐Lag Instability of Helicopter Rotors
2. Recent Studies of the Pitch‐Lag Instabilities of Articulated Rotors
3. Aeroelastic Instability of Torsionally Rigid Helicopter Blades
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3. Bilinear formulation applied to the response and stability of helicopter rotor blade;AIAA Journal;1994-10
4. Comparison between imposed-periodicity and marching-in-time solutions of helicopter rotor blade steady-state response problem;33rd Structures, Structural Dynamics and Materials Conference;1992-04-13
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