Physics-Based Hydraulic Damper Model for Rotor Structural Loads
Author:
Affiliation:
1. U.S. Army Research Laboratory, Aberdeen Proving Ground, Maryland 21005
2. Rensselaer Polytechnic Institute, Troy, New York 12180
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033735
Reference7 articles.
1. Formulation, Validation, and Application of a Finite Element Model for Elastomeric Lag Dampers
2. Characterization and Modeling of the Low Strain Amplitude and Frequency Dependent Behavior of Elastomeric Damper Materials
3. Application of a Refined Time Domain Elastomeric Damper Model to Helicopter Rotor Aeroelastic Response and Stability
4. HowlettJ. J. “UH-60A Black Hawk Engineering Simulation Program: Volume 1—Mathematical Model,” Ames Research Center, NASA CR-166309, Dec. 1981.
5. Ellis Horwood Series in Engineering Science Series;McCloy D.,1980
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