Helicopter vibration reduction using structural optimization with aeroelastic/multidisciplinary constraints - A survey
Author:
Affiliation:
1. University of California at Los Angeles, Los Angeles, California 90024
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45987
Reference58 articles.
1. Helicopter Vibrations: A Technological Perspective
2. Helicopter Blade Vibration and Flutter
3. Effect of Spanwise and Chordwise Mass Distribution on Rotor Blade Cyclic Stresses
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