Adhesive strength improvement by providing steps in joints and differentiating initial and final debonding stresses

Step adhesive joints have a special characteristic quite different from other joints. When initial delamination occurs in other joints such as butt, lap and scarf joints, final failure always occurs. In these cases, the external stress causing initial delamination σcInitial is equal to the final failure stress as σcFinal = σcInitial. However, in step joints, the final failure stress σcFinal can be greater than the initial delamination stress σcInitial < σcFinal. To clarify the adhesive improvement mechanism, first, this paper discusses the ISSF (Intensity of Singular Stress Fields) for fully bonded step joint by varying the number of steps NS. Second, the singular stress field causing 2nd debonding is discussed by analyzing partially delaminated step joint. The results show that 2nd debonding requires larger external load than the initial debonding as σcInitial < σcFinal. This is because under the same external load the singular stress causing the 2nd deboning is smaller than the one causing the initial debonding. When NS≥6 and suitable overlap length, the final bond strength σcFinal can be more than 3.6 ∼ 4.4 times larger than the initial delamination stress σcInitial ≪σcFinal resulting in much larger bond strength.

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Publication Details

Journal
Materials & Design
Published
2024-08-22
DOI
https://doi.org/10.1016/j.matdes.2024.113258
Citations
2
Primary Topic
Mechanical Behavior of Composites
Type
article
Field-Weighted Citation Impact
0.54
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article

Adhesive strength improvement by providing steps in joints and differentiating initial and final debonding stresses

N. Noda, Rei Takaki
2 citations
Materials & Design
Mechanical Behavior of Composites
0.54
article

Adhesive strength improvement by providing steps in joints and differentiating initial and final debonding stresses

N. Noda, Rei Takaki
article en
2 citations

Abstract

Step adhesive joints have a special characteristic quite different from other joints. When initial delamination occurs in other joints such as butt, lap and scarf joints, final failure always occurs. In these cases, the external stress causing initial delamination σcInitial is equal to the final failure stress as σcFinal = σcInitial. However, in step joints, the final failure stress σcFinal can be greater than the initial delamination stress σcInitial < σcFinal. To clarify the adhesive improvement mechanism, first, this paper discusses the ISSF (Intensity of Singular Stress Fields) for fully bonded step joint by varying the number of steps NS. Second, the singular stress field causing 2nd debonding is discussed by analyzing partially delaminated step joint. The results show that 2nd debonding requires larger external load than the initial debonding as σcInitial < σcFinal. This is because under the same external load the singular stress causing the 2nd deboning is smaller than the one causing the initial debonding. When NS≥6 and suitable overlap length, the final bond strength σcFinal can be more than 3.6 ∼ 4.4 times larger than the initial delamination stress σcInitial ≪σcFinal resulting in much larger bond strength.

Materials & DesignVol. 245
Kyushu Institute of Technology (JP), Nippon Bunri University (JP)
Openalex Percentile: Top 40%
Mechanical Behavior of Composites
0.54
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