Research Article
Finite Element Simulation of the Vibration Provided by Sandwich Rigid Panel with a Resilient Material In Between under Heavyweight Impact
Table 6
Measured and simulated maximum acceleration under resilient materials.
| Tested panel | Test 1 (g) | Test 2 (g) | Test 3 (g) | Test 4 (g) | Test 5 (g) | Average (g) | Simulation (g) |
| No resilient | 26.11 | 26.47 | 26.38 | 25.65 | 26.17 | 26.16 | 28.15 (7.6%) | With NBR 18 | 7.57 | 7.75 | 7.59 | 7.48 | 7.39 | 7.56 | 8.78 (16.1%) | With EVA 25 | 10.33 | 10.07 | 9.41 | 8.73 | 10.28 | 9.76 | 10.43 (6.9%) | With EVA 35 | 10.41 | 9.20 | 11.93 | 9.74 | 13.25 | 10.93 | 12.81 (17.2%) | With EVA 55 | 17.28 | 16.85 | 14.64 | 17.84 | 16.04 | 16.53 | 14.86 (−10.1%) |
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