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Carbon Epoxy Composite - DOAJ

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Last Updated: 03 September 2022

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Oblique Low-Velocity Impact Response and Damage Behavior of Carbon-Epoxy Composite Laminates

The delamination damage to upper layers is increasing as a result of the increase of the impact angle, and the impact on the top interface has increased by 132. 1% from 0 to 60 percent, with a rise in the impact from 0 to 60. While delamination damage to lower layers is mainly determined by normal loads, weakening with the increasing impact angle overall, and the impact area of the lowest interface decreases by 36. 6% from 000b0 to 60 percent of 60.

Source link: https://doi.org/10.3390/ma15155256

* Please keep in mind that all text is summarized by machine, we do not bear any responsibility, and you should always check original source before taking any actions

* Please keep in mind that all text is summarized by machine, we do not bear any responsibility, and you should always check original source before taking any actions