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Table 1.

Parameters of the test components.

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Table 1 Expand

Fig 1.

Process of sandwich panel preparation.

(a) Laying of the lower layer of fiber cloth. (b) Laying of the core material. (c) Laying of the upper face sheet of fiber cloth. (d) Laying of the vacuum bag. (e) Resin infusion. (f) Cutting and shaping.

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Fig 1 Expand

Fig 2.

Specimens for the GFRP tests.

(a) Specimen size for the tensile tests of the face sheets and webs. (b) Specimen size for the longitudinal and transverse shearing tests of the webs.

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Fig 2 Expand

Table 2.

Results of face sheet tensile tests.

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Table 2 Expand

Fig 3.

Foam compression test.

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Fig 3 Expand

Fig 4.

Stress-strain curves from flat crush tests of the foam core material.

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Fig 5.

Test loading device.

(a) Uniform loading. (b) Concentrated loading.

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Fig 6.

Load-central point vertical displacement curve.

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Fig 6 Expand

Table 3.

Experimental results for specimens with different web heights.

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Table 3 Expand

Fig 7.

Photograph of the failure of specimen SX75-175.

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Fig 7 Expand

Fig 8.

Fracture failure of the upper face sheet.

(a) SX50-75. (b) SX75-75. (c) SX100-75. (d) SX75-125.

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Fig 8 Expand

Fig 9.

Load-deflection curves of the specimens.

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Fig 9 Expand

Fig 10.

Relationship between the specimen load and web density.

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Fig 10 Expand

Fig 11.

Relationship between the specimen load and web height.

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Fig 11 Expand

Table 4.

Test result comparison.

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Table 4 Expand

Fig 12.

Schematic diagram of an original sandwich panel and the corresponding simulated sandwich panel.

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Fig 12 Expand

Fig 13.

Mechanical model of the simulated sandwich panel.

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Fig 14.

Calculation of specimen deflections and comparison with the experimental values.

(a) SX75-75 deflection. (b) SX75-125 deflection. (c) SX75-175 deflection. (d) SX100-75 deflection. (e) SX50-75 deflection.

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Fig 14 Expand

Table 5.

Contrast in vertical deflections at the central point of the sandwich panels (uniformly distributed load q = 10.08kN/2).

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Table 5 Expand