Simulation of Helicopter Rotor-System Structural Damage, Blade Mistracking, Friction, and Freeplay
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
2. U.S. Naval Air Warfare Center, Bethesda, Maryland 20084
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2342
Reference12 articles.
1. The use of Math-Dynamic Models to Aid the Development of Integrated Health and Usage Monitoring Systems
2. Formulation of a Helicopter Rotor System Damage Detection Methodology
3. Analysis of the Response of a Multi-Rotor-Bearing System Containing a Transverse Crack in a Rotor
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