Thin-walled composite beams under bending, torsional, and extensional loads
Author:
Affiliation:
1. University of Maryland, College Park, Maryland
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.25331
Reference15 articles.
1. Aeroelastic Stability Analysis of a Composite Rotor Blade
2. Aeroelastic Stability Analysis of a Composite Bearingless Rotor Blade
3. Finite-Element Model for Composite Beams with Arbitrary Cross-Sectional Warping
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