Investigating the Aeroelastic Behaviors of Rotor Blades with Nonlinear Energy Sinks

Author:

Ebrahimzade Nima1,Dardel Morteza1,Shafaghat Rouzbeh1

Affiliation:

1. Babol Noshirvani University of Technology, 47148-71167 Babol, Iran

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference36 articles.

1. HouboltJ. C.BrooksG. W. “Differential Equations of Motion for Combined Flap-Wise Bending, Chordwise Bending and Torsion of Twisted Nonuniform Rotor Blade,” NACA TR-1346, 1958.

2. ArcidiaconoP. J. “Prediction of Rotor Instability at High Forward Speeds. Vol. 1, Steady Flight Differential Equations of Motion for a Flexible Helicopter Blade with Chordwise Mass Unbalance,” USAAVLABS TR 68-188, Vol. 1, U.S. Army Aviation Materiel Lab. Feb. 1969.

3. HodgesD. H.OrmistonR. A. “Nonlinear Equations for Bending of Rotating Beams with Application to Linear Flap–lag Stability of Hinge-Less Rotors,” NASA TM X-2770, 1973.

4. HodgesD. H.DowellE. H. “Nonlinear Equations of Motion for the Elastic Bending and Torsion of Twisted Nonuniform Rotor Blades,” NASA TN D-7818, 1974.

5. HodgesD. H.OrmistonR. A. “Stability of Elastic Bending and Torsion of Uniform Cantilever Rotor Blades in Hover with Variable Structural Coupling,” NASA TN D-8192, 1976.

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