Flutter and stall response of a helicopter blade with structural nonlinearity
Author:
Affiliation:
1. Duke University, Durham, North Carolina 27706
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46268
Reference11 articles.
1. Application of transient aerodynamics to the structural nonlinear flutter problem
2. Analysis of limit cycle flutter of an airfoil in incompressible flow
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