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
β¦ LIBER β¦
Influence of post-buckling behaviour on optimum design of stiffened panels
β Scribed by Viggo Tvergaard
- Publisher
- Elsevier Science
- Year
- 1973
- Tongue
- English
- Weight
- 892 KB
- Volume
- 9
- Category
- Article
- ISSN
- 0020-7683
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