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Author:

Guo, Yi-Er (Guo, Yi-Er.) | Shang, De-Guang (Shang, De-Guang.) (Scholars:尚德广) | Zuo, Lin-Xuan (Zuo, Lin-Xuan.) | Qu, Lin-Feng (Qu, Lin-Feng.) | Chen, Chao-Lin (Chen, Chao-Lin.)

Indexed by:

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.

Keyword:

Composite laminates Fatigue life prediction Creep damage Elevated temperature Fatigue damage

Author Community:

  • [ 1 ] [Guo, Yi-Er]Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
  • [ 2 ] [Shang, De-Guang]Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
  • [ 3 ] [Chen, Chao-Lin]Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
  • [ 4 ] [Zuo, Lin-Xuan]Aviat Ind Corp China Ltd, Shenyang Aircraft Design & Res Inst, Shenyang, Peoples R China
  • [ 5 ] [Qu, Lin-Feng]Aviat Ind Corp China Ltd, Shenyang Aircraft Design & Res Inst, Shenyang, Peoples R China
  • [ 6 ] [Guo, Yi-Er]Chinese Acad Sci, CAS Ctr Excellence Nanosci, Natl Ctr Nanosci & Technol, Lab Theoret & Computat Nanosci, Beijing 100190, Peoples R 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: 2

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 1

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