Flutter characteristics of laminated composite wings
Author:
Affiliation:
1. City University, London EC IV OHB, England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.47078
Reference9 articles.
1. AEROELASTIC TAILORING OF ADVANCED COMPOSITE LIFTING SURFACES IN PRELIMINARY DESIGN
2. Vibration tailoring of advanced composite lifting surfaces
3. Control of aeroelastic instabilities through stiffness cross-coupling
4. Free vibration of composite beams - An exact method using symbolic computation
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3. Multi-objective optimization of a composite wing subject to strength and aeroelastic constraints;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2011-10-21
4. Optimal design of an aeroelastic wing structure with seamless control surfaces;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2009-08-01
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