Experimental Study on Dynamic Characteristics Improvement of Helicopter Hingeless Rotor System

Author:

Kim Deog-Kwan,Lee In,Song Keun-Woong,Joo Gene

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference13 articles.

1. ReichertE. W. “Long Term Experience with a Hingeless/Composite Rotor,” AGARD CP-233, 1977, pp. 11-1–11-6.

2. SchindlerE. P. “Impacts of Rotor Hub Design Criteria on the Operational Capabilities of Rotorcraft,” AGARD CP-423, 1987, pp. 15-1–15-9.

3. JohnsonW. “Recent Development in the Dynamics of Advanced Rotor System (II),” AGARD LS-139, 1985, pp. 4-1–4-5

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

5. RosenA.FriedmannP. P. “Nonlinear Elastic Equations of Equilibrium for Elastic Helicopter or Wind Turbine Blades Undergoing Moderate Deformation,” NASA CR-159478, 1978.

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