Advances in Materials Science and Engineering / 2018 / Article / Tab 6

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.

Casem (g)Fmax (N)Favg (N)CFEEA (J)SEA (J/g)

A1-specimen22316145.70.463.060.14
A2-specimen20260117.10.452.460.12
A3-specimen203011300.432.730.14
A-average20.7292.31310.452.750.14
A-FEA19.83001200.402.80.14
G1-specimen23329.688.70.271.330.06
G2-specimen22360.8100.60.281.510.07
G3-specimen22351940.271.410.06
G-average22.3347.194.40.271.410.06
G-FEA15.5328900.271.380.09
H1-specimen16316.669.30.221.040.07
H2-specimen16282.2840.301.260.08
H3-specimen16301.980.70.271.210.08
H-average16300.2780.261.170.08
H-FEA11.3300770.261.10.10

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