High temperature dynamic compression mechanical behavior of 3D woven carbon/carbon composites

This study investigates the dynamic compressive mechanical properties of three-dimensional woven carbon/carbon composites under both room temperature(25 ℃) quasi-static and from 25 ℃ to 900 ℃ dynamic compression conditions using both a materials testing machine and a split Hopkinson press bar device equipped for simultaneous high-temperature loading. The experimental results reveal that the strength of the composites is influenced by three key factors: fiber orientation, strain rate, and temperature. Specifically, under consistent strain rates and temperatures, the composites exhibit higher strength in the Z-direction compared to the XY-direction. As the strain rate escalates, the strengths of the composites in both the XY-direction and Z-direction increase, indicating a positive correlation with the strain rate. Upon heating from room temperature to 900 ℃, the strengths of both XY-direction and Z-direction composites initially rise, peaking at 600 ℃, and then gradually decline. Under both static and dynamic loading conditions, XY-direction composites undergo shear failure, albeit with a smaller shear fracture angle in the dynamic case compared to the quasi-static scenario. An increase in the strain rate results in a transition in the fracture mode of Z-direction composites, shifting from shear failure to a combination of matrix crushing and partial fiber fracture.

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Publication Details

Journal
SHILAP Revista de lepidopterología
Published
2025-05-01
DOI
https://doi.org/10.11868/j.issn.1001-4381.2023.000723
Primary Topic
Mechanical Behavior of Composites
Type
article
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article

High temperature dynamic compression mechanical behavior of 3D woven carbon/carbon composites

SHILAP Revista de lepidopterología
Mechanical Behavior of Composites
article

High temperature dynamic compression mechanical behavior of 3D woven carbon/carbon composites

article en

Abstract

This study investigates the dynamic compressive mechanical properties of three-dimensional woven carbon/carbon composites under both room temperature(25 ℃) quasi-static and from 25 ℃ to 900 ℃ dynamic compression conditions using both a materials testing machine and a split Hopkinson press bar device equipped for simultaneous high-temperature loading. The experimental results reveal that the strength of the composites is influenced by three key factors: fiber orientation, strain rate, and temperature. Specifically, under consistent strain rates and temperatures, the composites exhibit higher strength in the Z-direction compared to the XY-direction. As the strain rate escalates, the strengths of the composites in both the XY-direction and Z-direction increase, indicating a positive correlation with the strain rate. Upon heating from room temperature to 900 ℃, the strengths of both XY-direction and Z-direction composites initially rise, peaking at 600 ℃, and then gradually decline. Under both static and dynamic loading conditions, XY-direction composites undergo shear failure, albeit with a smaller shear fracture angle in the dynamic case compared to the quasi-static scenario. An increase in the strain rate results in a transition in the fracture mode of Z-direction composites, shifting from shear failure to a combination of matrix crushing and partial fiber fracture.

SHILAP Revista de lepidopterología
China Academy of Engineering Physics (CN)
Openalex Percentile: Top 54%
Mechanical Behavior of Composites
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