Aeroelastic Stability of Hingeless Rotor Blades in Hover Using Fully Intrinsic Equations
Author:
Affiliation:
1. Amirkabir University of Technology, 15875-4413 Tehran, Iran
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055079
Reference69 articles.
1. HodgesD. H. “Nonlinear Equations for the Dynamics of Pretwisted Beams Undergoing Small Strains and Large Rotations,” NASA Rept. TP-2470, 1985.
2. Aeroelastic stability of composite hingeless rotor blades in hover—Part I: Theory
3. Aeroelastic stability of hingeless rotor blade in hover using large deflection theory
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