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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| Format: | Thesis |
| Language: | English |
| Published: |
2007
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| Online Access: | http://psasir.upm.edu.my/id/eprint/5222/1/FK_2007_31.pdf |