Adhesive tongue-and-groove joints for thick composite laminates
Source abstract
Abstract
Abstract A new approach is explored for the joining of thick, woven E-glass/vinyl-ester composite laminated plates to steel or other composite plates, with applications in naval ship structures. Adhesive is applied along through-thickness contoured interfaces, employing tongue-and-groove geometry. Both experimental and finite element modeling results are presented. They show that adhesively bonded tongue-and-groove joints between steel and composite plates loaded in monotonically increasing longitudinal tension are stronger than conventional strap joints even in relatively thin plates. In particular, a single 0.25 inch wide and 8 or 12 inch long steel tongue, bonded by the Dexter-Hysol 9339 adhesive to a groove in a 0.5 inch thick laminated plate, can support a 20,000 lbs tension force. This force is expected to increase in proportion to plate thickness. Simple design rules indicate that the adhesive bond can be made stronger than that of the tongues, so that failure is transferred from the adhesive to the adherends. High joint efficiency can be achieved for any thickness of the joined plates.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Mechanical Behavior of Composites · Composite Structure Analysis and Optimization · Structural Analysis of Composite Materials
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (17)
Show source-provided references
1. Stress analysis and failure properties of carbon-fibre-reinforced-plastic/steel double-lap joints10.1080/00218468608073238 ↗
2. Strength predictions for lap joints, especially with composite adherends. A review10.1080/00218468908048207 ↗
3. A method for the stress analysis of lap joints10.1080/00218469208030455 ↗
4. Adams · 1997
5. Elastic analysis and engineering design formulae for bonded joints10.1016/0143-7496(89)90066-3 ↗
6. A comparison of numerous lap joint theories for adhesively bonded joints10.1080/00218469108030435 ↗
7. Simplified procedures for designing adhesively bonded composite joints10.1177/073168449101000102 ↗
8. Fracture load predictions for adhesive joints10.1016/0266-3538(94)90091-4 ↗
9. Further developments in the design and analysis of adhesively bonded structural joints10.1520/STP33472S ↗
10. Hart-Smith LJ. The key to designing durable adhesively bonded joints. Composites 1994.10.1016/0010-4361(94)90033-7 ↗
11. Strength of adhesively bonded scarf joints between glass fibre-reinforced plastics and metal10.1016/0143-7496(90)90104-6 ↗
12. The efficient design of adhesively bonded joints10.1080/00218467508075049 ↗
13. An assessment of failure criteria to predict the strength of adhesively bonded composite double lap joints10.1177/073168449701600803 ↗
14. Stresses in adhesively bonded joints10.1115/1.3157618 ↗
15. Viscoelastic analysis of adhesively bonded joints10.1177/002199838101500305 ↗
16. MacNeal-Schwendler Corporation, Los Angeles, CA, MSC/PATRAN User's Mannual, version 7.5, 1997.
17. Hibbitt, Karlsson and Sorensen Inc., Rhode Island. ABAQUS User's Mannual/Standard, version 5.8, 1997.