Research on the Adhesive Strength and Bending Creep Performance of CFRP-Al Adhesive Structures.

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Title: Research on the Adhesive Strength and Bending Creep Performance of CFRP-Al Adhesive Structures.
Authors: Wen, Xianglong1,2 (AUTHOR), Wang, Guangqian1 (AUTHOR), Liu, Wei1 (AUTHOR), Fu, Kai1 (AUTHOR), Song, Chunsheng1 (AUTHOR), Zhang, Jinguang1,3 (AUTHOR) jgzhang@whut.edu.cn
Source: Mechanics of Composite Materials. May2025, Vol. 61 Issue 2, p391-408. 18p.
Subjects: Flexural modulus, Elastic modulus, Structural stability, Bending strength, Engineering
Abstract: The adhesive structure is a common connection, which has the advantages of high stiffness and no damage to the adhesive parts. However, in practical engineering, the adhesive structure will produce creep, resulting in the reduction of the strength and elastic modulus of the structure, which will affect the stability and reliability of the structure. The optimal adhesive layer thickness of 0.3 mm and ambient temperature of 30°C were determined for the adhesive single lap structure studied. The effects of creep on the strength and elastic modulus of adhesive structures at different stress levels were investigated under optimal adhesive layer thickness and ambient temperature. The strength of the non-creep test specimen was 1295.17 MPa, the bending modulus was 49.43 GPa, and the strength retention rates after 10 h of creep under different stress levels were 98.203, 96.015, 93.527, and 90.471%. The retention rates of elastic modulus were 97.571, 95.456, 92.802, and 89.923%. Finally, a theoretical model was established to analyze and predict the creep behavior of adhesive structures, and the fitting degree of more than 0.98 between the theoretical and experimental results was established. This research provides a broad application prospect for the design and manufacture of fuselage, body panel, chassis, and other structures. [ABSTRACT FROM AUTHOR]
Copyright of Mechanics of Composite Materials is the property of Springer Nature and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
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  Data: Research on the Adhesive Strength and Bending Creep Performance of CFRP-Al Adhesive Structures.
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  Data: <searchLink fieldCode="JN" term="%22Mechanics+of+Composite+Materials%22">Mechanics of Composite Materials</searchLink>. May2025, Vol. 61 Issue 2, p391-408. 18p.
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  Data: <searchLink fieldCode="DE" term="%22Flexural+modulus%22">Flexural modulus</searchLink><br /><searchLink fieldCode="DE" term="%22Elastic+modulus%22">Elastic modulus</searchLink><br /><searchLink fieldCode="DE" term="%22Structural+stability%22">Structural stability</searchLink><br /><searchLink fieldCode="DE" term="%22Bending+strength%22">Bending strength</searchLink><br /><searchLink fieldCode="DE" term="%22Engineering%22">Engineering</searchLink>
– Name: Abstract
  Label: Abstract
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  Data: The adhesive structure is a common connection, which has the advantages of high stiffness and no damage to the adhesive parts. However, in practical engineering, the adhesive structure will produce creep, resulting in the reduction of the strength and elastic modulus of the structure, which will affect the stability and reliability of the structure. The optimal adhesive layer thickness of 0.3 mm and ambient temperature of 30°C were determined for the adhesive single lap structure studied. The effects of creep on the strength and elastic modulus of adhesive structures at different stress levels were investigated under optimal adhesive layer thickness and ambient temperature. The strength of the non-creep test specimen was 1295.17 MPa, the bending modulus was 49.43 GPa, and the strength retention rates after 10 h of creep under different stress levels were 98.203, 96.015, 93.527, and 90.471%. The retention rates of elastic modulus were 97.571, 95.456, 92.802, and 89.923%. Finally, a theoretical model was established to analyze and predict the creep behavior of adhesive structures, and the fitting degree of more than 0.98 between the theoretical and experimental results was established. This research provides a broad application prospect for the design and manufacture of fuselage, body panel, chassis, and other structures. [ABSTRACT FROM AUTHOR]
– Name: AbstractSuppliedCopyright
  Label:
  Group: Ab
  Data: <i>Copyright of Mechanics of Composite Materials is the property of Springer Nature and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)
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        Value: 10.1007/s11029-025-10282-x
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      – Code: eng
        Text: English
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        PageCount: 18
        StartPage: 391
    Subjects:
      – SubjectFull: Flexural modulus
        Type: general
      – SubjectFull: Elastic modulus
        Type: general
      – SubjectFull: Structural stability
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      – SubjectFull: Bending strength
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      – SubjectFull: Engineering
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      – TitleFull: Research on the Adhesive Strength and Bending Creep Performance of CFRP-Al Adhesive Structures.
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            NameFull: Wen, Xianglong
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            – D: 01
              M: 05
              Text: May2025
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              Y: 2025
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