Structural Optimization of an Aeroelastically Tailored Composite Flat Plate Made of Woven Fiberglass/Epoxy

• Main Authors: Attaran, A., Majid, D. L., Basri, S., Mohd. Rafie, A. S.
• Format: Conference or Workshop Item
• Language: English
• Published: 2006
• Subjects: TL Motor vehicles. Aeronautics. Astronautics
• Online Access: http://eprints.utm.my/id/eprint/350/1/AAttaran2006_StructuralOptimizationofanAeroelasticallyTailored.pdf; http://eprints.utm.my/id/eprint/350/

Effects of aspect ratio, sweep angle, and stacking sequence of laminated composites were studied to find the optimized configuration of an aeroelastically tailored composite wing idealized as a flat plate in terms of flutter speed. The aeroelastic analysis has been carried out in frequency-domain. T...