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

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

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...

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Bibliographic Details
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/350/ http://eprints.utm.my/350/1/AAttaran2006_StructuralOptimizationofanAeroelasticallyTailored.pdf

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