Optimal design of laminated composite stiffened panels of symmetric and balanced layup with different number of T-shape stiffeners is investigated and presented. The stiffened panels are simply supported and subjected to uniform biaxial compressive load. In the optimization for the maximum buckling
✦ LIBER ✦
Buckling of composite panels: A criterion for optimum stiffener design
✍ Scribed by P. Weißgraeber; C. Mittelstedt; W. Becker
- Book ID
- 113471336
- Publisher
- Elsevier Science
- Year
- 2012
- Tongue
- English
- Weight
- 524 KB
- Volume
- 16
- Category
- Article
- ISSN
- 1270-9638
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