Research Article
Finite Element Modeling of Stress Behavior of FGM Nanoplates
Table 8
Maximum stresses at z = h/2 of fully simply supported FGM nanoplate subjected to uniformly distributed load, a/h = 10, and a/b = 1.
| | n | | 0 | 0.5 | 1.0 | 1.5 | 2.0 | 2.5 |
| | 0 | 48.298 | 49.056 | 49.814 | 50.593 | 51.350 | 52.106 | 0.5 | 57.740 | 58.645 | 59.550 | 60.456 | 61.361 | 62.267 | 2 | 67.767 | 68.828 | 69.890 | 70.951 | 72.013 | 73.074 | 10 | 85.703 | 87.042 | 88.381 | 89.720 | 91.059 | 92.398 |
| | 0 | 48.298 | 49.056 | 49.814 | 50.503 | 51.350 | 52.126 | 0.5 | 57.740 | 58.585 | 59.550 | 60.456 | 61.361 | 62.267 | 2 | 67.767 | 68.828 | 69.890 | 70.951 | 72.013 | 73.074 | 10 | 85.703 | 87.042 | 88.381 | 89.720 | 91.059 | 92.398 |
| | 0 | 25.456 | 27.260 | 34.260 | 41.260 | 48.259 | 55.259 | 0.5 | 30.401 | 32.564 | 40.926 | 49.287 | 57.649 | 66.010 | 2 | 35.696 | 38.228 | 48.403 | 57.859 | 67.675 | 77.490 | 10 | 45.185 | 48.368 | 60.787 | 73.207 | 85.626 | 98.045 |
| | 0 | 3.893 | 3.894 | 3.895 | 3.896 | 3.897 | 3.898 | 0.5 | 4.852 | 4.853 | 4.854 | 4.855 | 4.856 | 4.857 | 2 | 6.401 | 6.402 | 6.403 | 6.404 | 6.405 | 6.406 | 10 | 8.344 | 8.345 | 8.346 | 8.347 | 8.348 | 8.349 |
| | 0 | 3.893 | 3.894 | 3.895 | 3.896 | 3.897 | 3.898 | 0.5 | 4.852 | 4.853 | 4.854 | 4.855 | 4.856 | 4.857 | 2 | 6.401 | 6.402 | 6.403 | 6.404 | 6.405 | 6.406 | 10 | 8.344 | 8.345 | 8.346 | 8.347 | 8.348 | 8.349 |
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