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...
Saved in:
| 主要作者: | |
|---|---|
| 格式: | Thesis |
| 语言: | English |
| 出版: |
2007
|
| 主题: | |
| 在线阅读: | http://psasir.upm.edu.my/id/eprint/5222/1/FK_2007_31.pdf |
| 标签: |
添加标签
没有标签, 成为第一个标记此记录!
|
成为第一个发表评论!