Helicopter Vibration Reduction Using Fixed-System Auxiliary Moments
Author:
Affiliation:
1. Pennsylvania State University, University Park, Pennsylvania 16802
2. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.575
Reference12 articles.
1. Helicopter Vibrations: A Technological Perspective
2. Helicopter vibration reduction using structural optimization with aeroelastic/multidisciplinary constraints - A survey
3. Vibration reduction in rotorcraft using active control - A comparison of various approaches
4. Flight Program on the NH‐3A Research Helicopter
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4. Helicopter rotor blade vibration reduction with optimizing the structural distribution of composite layers;Journal of Measurements in Engineering;2022-03-30
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