Refined Structural Dynamics Model for Composite Rotor Blades
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1310
Reference32 articles.
1. Assessment of Composite Rotor Blade Modeling Techniques
2. VABS: A New Concept for Composite Rotor Blade Cross-Sectional Modeling
3. Nonclassical Behavior of Thin‐Walled Composite Beams with Closed Cross Sections
4. Formulation and Evaluation of an Analytical Model for Composite Box‐Beams
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