Research Article
Forced Vibration Analysis of Laminated Composite Shells Reinforced with Graphene Nanoplatelets Using Finite Element Method
Table 3
The first nondimensional fundamental frequencies with different meshes.
| Cases of GPL | UD-type | X-type | O-type | V-type | BC | SSSS | CCCC | SSSS | CCCC | SSSS | CCCC | SSSS | CCCC |
| SPH (spherical shell) | Mesh | 4 × 4 | 28.9466 | 45.7319 | 29.7675 | 44.5987 | 23.9914 | 39.9593 | 25.9421 | 41.9856 | 6 × 6 | 28.9305 | 45.6370 | 29.7532 | 44.5122 | 23.9789 | 39.8547 | 25.9291 | 41.8878 | 8 × 8 | 28.9279 | 45.6238 | 29.7508 | 44.4995 | 23.9769 | 39.8417 | 25.9270 | 41.8752 | 10 × 10 | 28.9273 | 45.6202 | 29.7502 | 44.4959 | 23.9763 | 39.8384 | 25.9291 | 41.8719 | 12 × 12 | 28.9270 | 45.6189 | 29.7500 | 44.4946 | 23.9761 | 39.8372 | 25.9264 | 41.8706 | 14 × 14 | 28.9269 | 45.6183 | 29.7499 | 44.4940 | 23.9760 | 39.8367 | 25.9262 | 41.8701 | [35] | 29.5920 | 44.0300 | 30.8370 | 43.2450 | 25.3060 | 39.4860 | 27.4230 | 40.5730 |
| CLY (cylindrical shell) | Mesh | 4 × 4 | 27.0804 | 43.7319 | 28.4903 | 41.3521 | 22.7309 | 38.5900 | 24.5928 | 40.6802 | 6 × 6 | 27.0659 | 43.6467 | 28.4761 | 41.2750 | 22.7179 | 38.4899 | 24.5792 | 40.5859 | 8 × 8 | 27.0635 | 43.6348 | 28.4737 | 41.2635 | 22.7158 | 38.4780 | 24.5770 | 40.5741 | 10 × 10 | 27.0629 | 43.6316 | 28.4731 | 41.2603 | 22.7152 | 38.4750 | 24.5764 | 40.5711 | 12 × 12 | 27.0627 | 43.6304 | 28.4729 | 41.2590 | 22.7150 | 38.4739 | 24.5762 | 40.5700 | 14 × 14 | 27.0626 | 43.6299 | 28.4728 | 41.2585 | 22.7149 | 38.4734 | 24.5761 | 40.5695 | [35] | 28.4430 | 42.4540 | 29.7630 | 41.7740 | 23.9830 | 37.9270 | 25.9830 | 39.0500 |
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