Optimization of Composite Wing Structures for Maximum Flutter Speed
Author:
Affiliation:
1. Cranfield University
2. Beijing University of Aeronautics and Astronautics
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2132
Reference22 articles.
1. of Forward Swept Composite Wings Divergence
2. Aeroelastic divergence of swept-forward composite wings including warping restraint effect
3. L.Librescu & J.Simovich, General Formulation for the Aeroelastic Divergence of Composite Swept-Forward WingStructures, JournalofAircraft, Vol25, No. 4,1988,pp364-371
4. L.Librescu and S.Thangjitham, Analytical Study on Static Aeroelastic Behavior of Swept-Forward Composite WingStructures, JournalofAircraft, Vol28, No. 2,1991,pp151-157
5. Aeroelastic flutter and divergence of stiffness coupled, graphite/epoxy cantilevered plates
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