Assessment of Beam and Shell Elements for Modeling Rotorcraft Blades
Author:
Affiliation:
1. U.S. Army Research Laboratory, Advanced Rotorcraft Technology, Inc., Sunnyvale, California 94085
2. U.S. Army Aeroflightdynamics Directorate (AMRDEC), Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032217
Reference15 articles.
1. Modeling rotorcraft dynamics with finite element multibody procedures
2. VABS: A New Concept for Composite Rotor Blade Cross-Sectional Modeling
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4. Anisotropic beam theory and applications
5. Time integrators for shells in multibody dynamics
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