Flutter Prediction for Composite Wings Using Parametric Studies
Author:
Affiliation:
1. City University, London EC1V OHB, England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.170
Reference11 articles.
1. Vibration tailoring of advanced composite lifting surfaces
2. AEROELASTIC TAILORING OF ADVANCED COMPOSITE LIFTING SURFACES IN PRELIMINARY DESIGN
3. Vibration and flutter of advanced composite lifting surfaces
4. Flutter characteristics of laminated composite wings
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5. A dynamic stiffness element for free vibration analysis of composite beams and its application to aircraft wings;Computers & Structures;2008-03
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