Structural Optimization of an Aeroelastically Tailored Composite Wing

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Structural Optimization of an Aeroelastically Tailored Composite Wing

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...

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Bibliographic Details
Main Author:	Attaran, Abdolhamid
Format:	Thesis
Language:	English
Published:	2007
Online Access:	http://psasir.upm.edu.my/id/eprint/5222/ http://psasir.upm.edu.my/id/eprint/5222/1/FK_2007_31.pdf

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