Forward Flight Stability Characteristics for Composite Hingeless Rotors with Transverse Shear Deformation
Author:
Affiliation:
1. Chonbuk National University, Chonju 561-756, Republic of Korea
2. Seoul National University, Seoul 151-742, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1875
Reference32 articles.
1. Review of composite rotor blade modeling
2. VABS: A New Concept for Composite Rotor Blade Cross-Sectional Modeling
3. Formulation and Evaluation of an Analytical Model for Composite Box‐Beams
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1. Effect of Uncertainty on Hub Vibration Response of Composite Helicopter Rotor Blades;Journal of Aircraft;2010-01
2. Single-crystal-material-based induced-shear actuation for vibration reduction of helicopters with composite rotor system;Smart Materials and Structures;2008-10-07
3. Wind Energy Literature Survey No. 4;Wind Energy;2003
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