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Author:

Guo, Y.-E. (Guo, Y.-E..) | Shang, D.-G. (Shang, D.-G..) | Zuo, L.-X. (Zuo, L.-X..) | Qu, L.-F. (Qu, L.-F..) | Chen, C.-L. (Chen, C.-L..)

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EI Scopus SCIE

Abstract:

In this paper, a fatigue-creep damage model that can take into account the interaction of fatigue and creep damage is proposed under high temperature cyclic loading. In the proposed model, the effect of temperature on creep damage, the variation of creep damage under different high temperature cyclic loading conditions, and fatigue-creep interaction damage are considered. In addition, in order to accurately describe the creep behavior of unidirectional laminates with different orientations, the damage mechanism of unidirectional laminates was also analyzed. The creep and fatigue test results at different temperatures showed that the proposed creep rupture time model and the fatigue-creep damage model considering the damage mechanisms can successfully predict the creep and fatigue lives of unidirectional laminates at high temperature, and the prediction results are in good agreement with the experimental data. © 2024

Keyword:

Composite laminates Elevated temperature Creep damage Fatigue damage Fatigue life prediction

Author Community:

  • [ 1 ] [Guo Y.-E.]Faculty of Materials and Manufacturing, Beijing University of Technology, Beijing, 100124, China
  • [ 2 ] [Guo Y.-E.]Laboratory of Theoretical and Computational Nanoscience, CAS Center for Excellence in Nanoscience, National Center for Nanoscience and Technology, Chinese Academy of Sciences, Beijing, 100190, China
  • [ 3 ] [Shang D.-G.]Faculty of Materials and Manufacturing, Beijing University of Technology, Beijing, 100124, China
  • [ 4 ] [Zuo L.-X.]Shenyang Aircraft Design & Research Institute, The Aviation Industry Corporation of China, Ltd., Shenyang, China
  • [ 5 ] [Qu L.-F.]Shenyang Aircraft Design & Research Institute, The Aviation Industry Corporation of China, Ltd., Shenyang, China
  • [ 6 ] [Chen C.-L.]Faculty of Materials and Manufacturing, Beijing University of Technology, Beijing, 100124, China

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Source :

Composites Science and Technology

ISSN: 0266-3538

Year: 2024

Volume: 258

9 . 1 0 0

JCR@2022

Cited Count:

WoS CC Cited Count:

SCOPUS Cited Count: 1

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 8

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