Crack-Induced Effects on Aeroelasticity of an Unswept Composite Wing
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24060-0261
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.21689
Reference30 articles.
1. Divergence speed degradation of forward-swept wings with damaged composite skin
2. Aeroelastic Stability of the GA-ASI Predator Aircraft
3. Flutter analysis of thin cracked panels using the finite element method
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