Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wing
Author:
Affiliation:
1. Technion—Israel Institute of Technology, Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45238
Reference17 articles.
1. Aeroelastic Tailoring of Forward Swept Composite Wings
2. Wind Tunnel Demonstration of Aeroelastic Tailoring Applied to Forward Swept Wings
3. Aeroelastic flutter and divergence of stiffness coupled, graphite/epoxy cantilevered plates
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