Aeroelastic Analysis of a Hingeless Rotor Blade in Forward Flight
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Taejon 305-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1038
Reference40 articles.
1. Rotary-wing aeroelasticity with application to VTOL vehicles
2. Review of composite rotor blade modeling
3. Nonclassical Behavior of Thin‐Walled Composite Beams with Closed Cross Sections
4. Thin-walled composite beams under bending, torsional, and extensional loads
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3. Aeroelastic Analysis of a Hingeless Rotor Using a Dynamic Wake Model;Journal of Aircraft;2011-09
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