Failure mode and strength of uni-directional composite single lap bonded joints with different bonding methods
Source abstract
Abstract
Failure process, mode and strength of unidirectional composite single lap bonded joints were investigated experimentally with respect to bonding methods, that is, co-curing with or without adhesive and secondary bonding. The co-cured joint specimen without adhesive had the highest failure strength. Progressive failures along an adhesive layer occurred in the secondary bonded specimen. In the co-cured specimen with adhesive film, delamination failure occurred and the joint strength was lower than that of secondary bonded specimens. Delamination failure did not occur in the secondary bonded specimen because of early crack growth and progressive failure in the adhesive layer. Therefore, The failure strength of composite bonded joint is not always proportionate to adhesion strength of adhesive due to the weakness of delamination in composite materials. The influences of surface roughness, bondline thickness and fillets in the secondary bonded specimens were also studied.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Mechanical Behavior of Composites · Structural Load-Bearing Analysis · Electronic Packaging and Soldering Technologies
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (16)
Show source-provided references
1. Surface pretreatment of carbon fibre-reinforced composites for adhesive bonding10.1016/0010-4361(82)90011-8 ↗
2. Characteristics of plasma surface treated composite adhesive joints at high environment temperature10.1016/S0263-8223(02)00060-0 ↗
3. Investigation of optimal surface treatments for carbon/epoxy composite adhesive joints10.1163/156856103762864651 ↗
4. The effect of a spew fillet on adhesive stress distributions in laminated composite single-lap joints10.1016/0263-8223(95)00059-3 ↗
5. Failure of adhesive-bonded composite single lap joints with embedded cracks10.2514/2.385 ↗
6. Failure of adhesive bonded composite lap shear joints with embedded precrack10.1016/S0266-3538(02)00054-4 ↗
7. Understanding and control of adhesive crack propagation in bonded joints between carbon fibre composite adherends, I. Experimental10.1016/S0143-7496(01)00020-3 ↗
8. Testing of adhesives for bonding of polymer composites10.1016/S0143-7496(02)00006-4 ↗
9. Investigation of prepreg bonded composite single lap joint10.1016/S1359-8368(01)00045-2 ↗
10. Strength and failure modes of bonded single lap joints between cross-ply adherends10.1016/0010-4361(93)90017-3 ↗
11. Analysis of single-lap adhesive composite joints with delaminated adherends10.1016/S1359-8368(02)00066-5 ↗
12. Stress and failure analysis of adhesive-bonded composite joints using ASTM D3165 specimen
13. Stress–strain analysis of adhesive-bonded single-lap composite joints under cylindrical bending10.1016/0961-9526(93)90020-K ↗
14. Stress concentrations caused by bond cracks in single-lap adhesive composite joints10.1016/S0263-8223(01)00090-3 ↗
15. Understanding and control of adhesive crack propagation in bonded joints between carbon fibre composite adherends, II. Finite element analysis10.1016/S0143-7496(01)00021-5 ↗
16. The influence of adhesive bonded thickness imperfections on stresses in composite joints10.1080/00218460309578 ↗