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    Subcritical Debonding Characterization of GFRP-Concrete Bonded Interface Using Modified Single Cantilever Beam Specimens

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 001::page 04023096-1
    Author:
    Shuyan Fu
    ,
    Qinghui Liu
    ,
    Pizhong Qiao
    ,
    Hao Li
    DOI: 10.1061/JAEEEZ.ASENG-5166
    Publisher: ASCE
    Abstract: Subcritical debonding of glass fiber reinforced polymer (GFRP)-concrete bonded interface in both the air (room environment) and water is characterized using the modified single cantilever beam specimens. A modified specimen design is uniquely proposed to overcome the potential large deformation of the GFRP substrate; i.e., a thin aluminum beam is glued to the top of GFRP strip to form a stiffer composite beam. A two-parametric elastic foundation model is employed to calculate the compliance and energy release rate (ERR) of the modified specimens, and it is then used to indirectly calculate the crack length, which is verified by the direct experimental strain measurements. Experimental programs using the modified specimens are conducted to characterize the subcritical debonding behavior of the GFRP-concrete bonded interface, and the effect of moisture condition on the subcritical debonding rate is evaluated. Meanwhile, the water-based epoxy primer promoting the interface bonding is explored. In particular, the relationship between the applied ERR and measured debonding growth rate is established. The test results demonstrate that the subcritical debonding growth occurs at slow loading rate and the failure mode shifts from the cohesive failure within concrete to the adhesive failure along the bonded interface. The subcritical debonding test method developed and the modified specimen proposed can better reveal the actual degradation mechanism of bimaterial bonded interface under different environments and loading rates.
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      Subcritical Debonding Characterization of GFRP-Concrete Bonded Interface Using Modified Single Cantilever Beam Specimens

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4297198
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    contributor authorShuyan Fu
    contributor authorQinghui Liu
    contributor authorPizhong Qiao
    contributor authorHao Li
    date accessioned2024-04-27T22:39:45Z
    date available2024-04-27T22:39:45Z
    date issued2024/01/01
    identifier other10.1061-JAEEEZ.ASENG-5166.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4297198
    description abstractSubcritical debonding of glass fiber reinforced polymer (GFRP)-concrete bonded interface in both the air (room environment) and water is characterized using the modified single cantilever beam specimens. A modified specimen design is uniquely proposed to overcome the potential large deformation of the GFRP substrate; i.e., a thin aluminum beam is glued to the top of GFRP strip to form a stiffer composite beam. A two-parametric elastic foundation model is employed to calculate the compliance and energy release rate (ERR) of the modified specimens, and it is then used to indirectly calculate the crack length, which is verified by the direct experimental strain measurements. Experimental programs using the modified specimens are conducted to characterize the subcritical debonding behavior of the GFRP-concrete bonded interface, and the effect of moisture condition on the subcritical debonding rate is evaluated. Meanwhile, the water-based epoxy primer promoting the interface bonding is explored. In particular, the relationship between the applied ERR and measured debonding growth rate is established. The test results demonstrate that the subcritical debonding growth occurs at slow loading rate and the failure mode shifts from the cohesive failure within concrete to the adhesive failure along the bonded interface. The subcritical debonding test method developed and the modified specimen proposed can better reveal the actual degradation mechanism of bimaterial bonded interface under different environments and loading rates.
    publisherASCE
    titleSubcritical Debonding Characterization of GFRP-Concrete Bonded Interface Using Modified Single Cantilever Beam Specimens
    typeJournal Article
    journal volume37
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5166
    journal fristpage04023096-1
    journal lastpage04023096-10
    page10
    treeJournal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 001
    contenttypeFulltext
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