Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime
Author:
Funder
Brazilian Research Agency
CNPq
Publisher
Elsevier BV
Subject
Civil and Structural Engineering,Ceramics and Composites
Reference17 articles.
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3. Aeroelastic tailoring of a plate wing with functionally graded materials;Dunning;J Fluids Struct,2014
4. Panel flutter: a review of the aeroelastic stability of plates and shells;Dowell;AIAA J,1970
5. Panel flutter suppression with an optimal controller based on the nonlinear model using piezoelectric materials;Moon;Compos Struct,2005
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