Fatigue design criteria for strengthening metallic beams with bonded CFRP plates

Publikation: Beitrag in FachzeitschriftArtikelForschungPeer-Review

Autoren

  • Elyas Ghafoori
  • Masoud Motavalli
  • Xiao Ling Zhao
  • Alain Nussbaumer
  • Mario Fontana

Externe Organisationen

  • Eidgenössische Materialprüfungs- und Forschungsanstalt (EMPA)
  • Monash University
  • ETH Zürich
  • University of Tehran
  • École polytechnique fédérale de Lausanne (EPFL)
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Details

OriginalspracheEnglisch
Seiten (von - bis)542-557
Seitenumfang16
FachzeitschriftEngineering structures
Jahrgang101
Frühes Online-Datum11 Aug. 2015
PublikationsstatusElektronisch veröffentlicht (E-Pub) - 11 Aug. 2015
Extern publiziertJa

Abstract

Different failure criteria used to prevent fatigue crack initiation in metallic members are described. A series of closed-form analytical solutions were developed to predict the fatigue resistance of metallic beams after strengthening with carbon fiber-reinforced polymer (CFRP) laminates. The model was used to determine Young's modulus, pre-stress level and dimensions of the CFRP laminates such that the metallic detail is shifted from a 'finite-life' regime to the 'infinite-life' regime. This method is capable of predicting changes in both the stress range and the mean stress after strengthening. The results show that increasing the stiffness and pre-stress levels of the CFRP laminate can affect the fatigue life of the retrofitted member through different mechanisms. The latter preserves the alternating stress and decreases the mean stress level, whereas the former decreases both the mean and alternating stresses proportionally. To validate this model, a series of fatigue tests were performed on five steel beams, including one reference beam and four strengthened beams. The beams were strengthened with normal modulus (NM), high modulus (HM) and ultra-high modulus (UHM) laminates. Finally, a design example for the fatigue strengthening of a typical riveted metallic girder is presented. The developed analytical model was used to find the most effective fatigue strengthening solution under different cyclic load scenarios. Although the major focus in this paper is on steel members, it also describes others, such as wrought iron and cast iron.

ASJC Scopus Sachgebiete

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Fatigue design criteria for strengthening metallic beams with bonded CFRP plates. / Ghafoori, Elyas; Motavalli, Masoud; Zhao, Xiao Ling et al.
in: Engineering structures, Jahrgang 101, 11.08.2015, S. 542-557.

Publikation: Beitrag in FachzeitschriftArtikelForschungPeer-Review

Ghafoori, E., Motavalli, M., Zhao, X. L., Nussbaumer, A., & Fontana, M. (2015). Fatigue design criteria for strengthening metallic beams with bonded CFRP plates. Engineering structures, 101, 542-557. Vorabveröffentlichung online. https://doi.org/10.1016/j.engstruct.2015.07.048
Ghafoori E, Motavalli M, Zhao XL, Nussbaumer A, Fontana M. Fatigue design criteria for strengthening metallic beams with bonded CFRP plates. Engineering structures. 2015 Aug 11;101:542-557. Epub 2015 Aug 11. doi: 10.1016/j.engstruct.2015.07.048
Ghafoori, Elyas ; Motavalli, Masoud ; Zhao, Xiao Ling et al. / Fatigue design criteria for strengthening metallic beams with bonded CFRP plates. in: Engineering structures. 2015 ; Jahrgang 101. S. 542-557.
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title = "Fatigue design criteria for strengthening metallic beams with bonded CFRP plates",
abstract = "Different failure criteria used to prevent fatigue crack initiation in metallic members are described. A series of closed-form analytical solutions were developed to predict the fatigue resistance of metallic beams after strengthening with carbon fiber-reinforced polymer (CFRP) laminates. The model was used to determine Young's modulus, pre-stress level and dimensions of the CFRP laminates such that the metallic detail is shifted from a 'finite-life' regime to the 'infinite-life' regime. This method is capable of predicting changes in both the stress range and the mean stress after strengthening. The results show that increasing the stiffness and pre-stress levels of the CFRP laminate can affect the fatigue life of the retrofitted member through different mechanisms. The latter preserves the alternating stress and decreases the mean stress level, whereas the former decreases both the mean and alternating stresses proportionally. To validate this model, a series of fatigue tests were performed on five steel beams, including one reference beam and four strengthened beams. The beams were strengthened with normal modulus (NM), high modulus (HM) and ultra-high modulus (UHM) laminates. Finally, a design example for the fatigue strengthening of a typical riveted metallic girder is presented. The developed analytical model was used to find the most effective fatigue strengthening solution under different cyclic load scenarios. Although the major focus in this paper is on steel members, it also describes others, such as wrought iron and cast iron.",
keywords = "Failure analysis, Fatigue resistance design approach, Pre-stressing, Riveted metallic structures, Strengthening, Ultra-high modulus carbon-fiber-reinforced polymer",
author = "Elyas Ghafoori and Masoud Motavalli and Zhao, {Xiao Ling} and Alain Nussbaumer and Mario Fontana",
note = "Funding Information: The authors would like to thank the technicians of the Structural Engineering Research Laboratory of Empa for their excellent cooperation in performing the experiments. The authors also gratefully acknowledge the support from the Epsilon Composite Company, France , and the S&P Clever Reinforcement Company AG, Switzerland , for providing the materials for this study. This paper was written while the first author was visiting the Department of Civil Engineering at Monash University, Melbourne, Australia. Support from the Australian Research Council Linkage Grant ( LP140100543 ) is also appreciated. ",
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TY - JOUR

T1 - Fatigue design criteria for strengthening metallic beams with bonded CFRP plates

AU - Ghafoori, Elyas

AU - Motavalli, Masoud

AU - Zhao, Xiao Ling

AU - Nussbaumer, Alain

AU - Fontana, Mario

N1 - Funding Information: The authors would like to thank the technicians of the Structural Engineering Research Laboratory of Empa for their excellent cooperation in performing the experiments. The authors also gratefully acknowledge the support from the Epsilon Composite Company, France , and the S&P Clever Reinforcement Company AG, Switzerland , for providing the materials for this study. This paper was written while the first author was visiting the Department of Civil Engineering at Monash University, Melbourne, Australia. Support from the Australian Research Council Linkage Grant ( LP140100543 ) is also appreciated.

PY - 2015/8/11

Y1 - 2015/8/11

N2 - Different failure criteria used to prevent fatigue crack initiation in metallic members are described. A series of closed-form analytical solutions were developed to predict the fatigue resistance of metallic beams after strengthening with carbon fiber-reinforced polymer (CFRP) laminates. The model was used to determine Young's modulus, pre-stress level and dimensions of the CFRP laminates such that the metallic detail is shifted from a 'finite-life' regime to the 'infinite-life' regime. This method is capable of predicting changes in both the stress range and the mean stress after strengthening. The results show that increasing the stiffness and pre-stress levels of the CFRP laminate can affect the fatigue life of the retrofitted member through different mechanisms. The latter preserves the alternating stress and decreases the mean stress level, whereas the former decreases both the mean and alternating stresses proportionally. To validate this model, a series of fatigue tests were performed on five steel beams, including one reference beam and four strengthened beams. The beams were strengthened with normal modulus (NM), high modulus (HM) and ultra-high modulus (UHM) laminates. Finally, a design example for the fatigue strengthening of a typical riveted metallic girder is presented. The developed analytical model was used to find the most effective fatigue strengthening solution under different cyclic load scenarios. Although the major focus in this paper is on steel members, it also describes others, such as wrought iron and cast iron.

AB - Different failure criteria used to prevent fatigue crack initiation in metallic members are described. A series of closed-form analytical solutions were developed to predict the fatigue resistance of metallic beams after strengthening with carbon fiber-reinforced polymer (CFRP) laminates. The model was used to determine Young's modulus, pre-stress level and dimensions of the CFRP laminates such that the metallic detail is shifted from a 'finite-life' regime to the 'infinite-life' regime. This method is capable of predicting changes in both the stress range and the mean stress after strengthening. The results show that increasing the stiffness and pre-stress levels of the CFRP laminate can affect the fatigue life of the retrofitted member through different mechanisms. The latter preserves the alternating stress and decreases the mean stress level, whereas the former decreases both the mean and alternating stresses proportionally. To validate this model, a series of fatigue tests were performed on five steel beams, including one reference beam and four strengthened beams. The beams were strengthened with normal modulus (NM), high modulus (HM) and ultra-high modulus (UHM) laminates. Finally, a design example for the fatigue strengthening of a typical riveted metallic girder is presented. The developed analytical model was used to find the most effective fatigue strengthening solution under different cyclic load scenarios. Although the major focus in this paper is on steel members, it also describes others, such as wrought iron and cast iron.

KW - Failure analysis

KW - Fatigue resistance design approach

KW - Pre-stressing

KW - Riveted metallic structures

KW - Strengthening

KW - Ultra-high modulus carbon-fiber-reinforced polymer

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DO - 10.1016/j.engstruct.2015.07.048

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AN - SCOPUS:84939141000

VL - 101

SP - 542

EP - 557

JO - Engineering structures

JF - Engineering structures

SN - 0141-0296

ER -

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