Mechanical response and damage evolution of CFRP laminates under coupled thermal-impact loading

This study investigates the mechanical properties and dynamic damage characteristics of CFRP laminates under coupled thermal and impact loads. Through thermal environment simulation, impact loading, and multidimensional data acquisition, experimental data on velocity, acceleration, stress-strain, and energy absorption were obtained. The results show that the heat-impact coupling effect significantly degrades the material’s mechanical performance. This study provides a research foundation for enhancing the structural performance of CFRP under thermal shock, and lays a scientific basis for its engineering application under complex service conditions.

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Publication Details

Journal
Vibroengineering PROCEDIA
Published
2026-04-22
DOI
https://doi.org/10.21595/vp.2026.26060
Primary Topic
Mechanical Behavior of Composites
Type
article
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article

Mechanical response and damage evolution of CFRP laminates under coupled thermal-impact loading

Fengfeng Wang, Jinyu Zhou, Lei Li
Vibroengineering PROCEDIA
Mechanical Behavior of Composites
article

Mechanical response and damage evolution of CFRP laminates under coupled thermal-impact loading

Fengfeng Wang, Jinyu Zhou, Lei Li
article en

Abstract

This study investigates the mechanical properties and dynamic damage characteristics of CFRP laminates under coupled thermal and impact loads. Through thermal environment simulation, impact loading, and multidimensional data acquisition, experimental data on velocity, acceleration, stress-strain, and energy absorption were obtained. The results show that the heat-impact coupling effect significantly degrades the material’s mechanical performance. This study provides a research foundation for enhancing the structural performance of CFRP under thermal shock, and lays a scientific basis for its engineering application under complex service conditions.

Vibroengineering PROCEDIAVol. 61
Openalex Percentile: Top 9%
Mechanical Behavior of Composites
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