Abstract
The fundamental frequencies of laminated truncated conical shells with a given material system are maximized with respect to fiber orientations by using a sequential linear programming method with a simple move-limit strategy. The significant influences of shell thickness, shell length, shell radius ratio and cutout on the maximum fundamental frequencies and the associated optimal fiber orientations are demonstrated.
| Original language | English |
|---|---|
| Pages (from-to) | 265-275 |
| Number of pages | 11 |
| Journal | Composite Structures |
| Volume | 52 |
| Issue number | 3-4 |
| DOIs | |
| Publication status | Published - 2001 May |
All Science Journal Classification (ASJC) codes
- Ceramics and Composites
- Civil and Structural Engineering
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