Improved Understanding of Aerodynamic Damping Through the Hilbert Transform
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of Notre Dame, Notre Dame, Indiana 46556
2. Rotor Dynamics and Aeromechanics, Bell Helicopter Textron, Fort Worth, Texas 76053
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052630
Reference32 articles.
1. FungY. C., An Introduction to the Theory of Aeroelasticity, Dover, New York, 2008, pp. 320–326.
2. Blade Stall—Half Fact, Half Fiction
3. Limit cycle torsional motion of helicopter blades due to stall
4. Incipient torsional stall flutter aerodynamic experiments on three-dimensional wings
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