Formulation of the aeroelastic stability and response problem of coupled rotor/support systems
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, Calif.
2. California, University, Los Angeles, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1979-732
Reference26 articles.
1. Recent Developments in Rotary-wing Aeroelasticity
2. 4eone,P. F. "Mechanical Stability of a Two-Bladed Cantilever Helicopter Rotor," Journal of the Aeronautical S.ciences, July 1956.
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Multi-flexible-body dynamic analysis of horizontal-axis wind turbines;20th 2001 ASME Wind Energy Symposium;2001-01-11
2. Coupled Rotor/Tower Aeroelastic Analysis of Large Horizontal Axis Wind Turbines;AIAA Journal;1980-09
3. Aeroelastic stability and response of horizontal axis wind turbine blades;AIAA Journal;1979-12
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