Geometrically nonlinear free vibrations of symmetric rectangular honeycomb sandwich panels with simply supported boundaries at the four edges are investigated using the homotopy analysis method (HAM). The honeycomb core of hexagonal cells is modeled as a thick layer of orthotropic material whose par
โฆ LIBER โฆ
Free flexural vibration analysis of symmetric honeycomb panels
โ Scribed by S.D. Yu; W.L. Cleghorn
- Publisher
- Elsevier Science
- Year
- 2005
- Tongue
- English
- Weight
- 396 KB
- Volume
- 284
- Category
- Article
- ISSN
- 0022-460X
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