Aeroelastic flutter and divergence of stiffness coupled, graphite/epoxy, cantilevered plates
Author:
Affiliation:
1. USAF, Flight Dynamics Laboratory, Wright-PattersonAFB, OH
2. MIT, Cambridge, MA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-722
Reference18 articles.
1. Aeroelastic Tailoring of Forward Swept Composite Wings
2. Wind Tunnel Demonstration of Aeroelastic Tailoring Applied to Forward Swept Wings
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