Research Article
The Bending Responses of Sandwich Panels with Aluminium Honeycomb Core and CFRP Skins Used in Electric Vehicle Body
Table 6
Different layer thicknesses for FEA and experimental results.
| Case | m (g) | Fmax (N) | Favg (N) | CFE | EA (J) | SEA (J/g) |
| A1-specimen | 22 | 316 | 145.7 | 0.46 | 3.06 | 0.14 | A2-specimen | 20 | 260 | 117.1 | 0.45 | 2.46 | 0.12 | A3-specimen | 20 | 301 | 130 | 0.43 | 2.73 | 0.14 | A-average | 20.7 | 292.3 | 131 | 0.45 | 2.75 | 0.14 | A-FEA | 19.8 | 300 | 120 | 0.40 | 2.8 | 0.14 | G1-specimen | 23 | 329.6 | 88.7 | 0.27 | 1.33 | 0.06 | G2-specimen | 22 | 360.8 | 100.6 | 0.28 | 1.51 | 0.07 | G3-specimen | 22 | 351 | 94 | 0.27 | 1.41 | 0.06 | G-average | 22.3 | 347.1 | 94.4 | 0.27 | 1.41 | 0.06 | G-FEA | 15.5 | 328 | 90 | 0.27 | 1.38 | 0.09 | H1-specimen | 16 | 316.6 | 69.3 | 0.22 | 1.04 | 0.07 | H2-specimen | 16 | 282.2 | 84 | 0.30 | 1.26 | 0.08 | H3-specimen | 16 | 301.9 | 80.7 | 0.27 | 1.21 | 0.08 | H-average | 16 | 300.2 | 78 | 0.26 | 1.17 | 0.08 | H-FEA | 11.3 | 300 | 77 | 0.26 | 1.1 | 0.10 |
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