Effects of Moulding Condition and Curing Atmosphere on the Flexural Properties of Vinyl Ester
Source abstract
Abstract
The effects of moulding condition and curing atmosphere on the flexural properties of a neat 33 wt.%-styrene epoxy vinyl ester (VE) were investigated. Specimens were prepared using either open or closed moulds, and thermally cured under either air or nitrogen atmosphere. Four-point bending tests were performed with both the top (“air-side”) and the bottom (“mould-side”) surfaces of the cured specimens in tension. The mean flexural moduli for nitrogen-cured and closed-mould specimens were 3% and 9% higher than for air-cured specimens, respectively. However, the mean flexural strength for open-mould air-cured specimens with their air-sides loaded in tension were 65% lower than the mean flexural strengths of open-mould nitrogen-cured or closed-mould specimens. This likely resulted from partial VE resin curing inhibition due to oxygen diffusion into the free surface region of the open-mould air-cured specimens. This creates gradients in the local stiffness and strength in the near-surface region due to lower crosslink density. This effect may be particularly important for thin specimens. These results underscore the significance of exposure to air during open-mould curing on the cured VE flexural properties. Such assessments are crucial for composite part manufacturing utilizing VEs.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Epoxy Resin Curing Processes · Injection Molding Process and Properties · Mechanical Behavior of Composites
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
The Dave C. Swalm School of Chemical Engineering, Mississippi State University, Mississippi State, MS 39762, USA
Center for Advanced Vehicular Systems (CAVS), Mississippi State, MS 39762-5405, USA
Department of Aerospace Engineering, Mississippi State University, Mississippi State, MS 39762, USA
Department of Chemistry, Mississippi State University, Mississippi State, MS 39762, USA
References (26)
Show source-provided references
1. Forsdyke K.L. · 2002
2. 10.1002/pen.76013011010.1002/pen.760130110 ↗
3. 10.1002/pc.1027010.1002/pc.10270 ↗
4. 10.1002/apmc.1985.05130011610.1002/apmc.1985.051300116 ↗
5. 10.1002/app.1990.07041113410.1002/app.1990.070411134 ↗
6. 10.1002/jbm.82027031410.1002/jbm.820270314 ↗
7. 10.1021/ma034970t10.1021/ma034970t ↗
8. 10.1002/(SICI)1099-0488(19990415)37:8<751::AID-POLB2>3.0.CO;2-V10.1002/(SICI)1099-0488(19990415)37:8<751::AID-POLB2>3.0.CO;2-V ↗
9. 10.1007/BF0027530610.1007/BF00275306 ↗
10. 10.1002/(SICI)1099-0488(19990401)37:7<725::AID-POLB23>3.0.CO;2-E10.1002/(SICI)1099-0488(19990401)37:7<725::AID-POLB23>3.0.CO;2-E ↗
11. 10.1016/S0032-3861(02)00490-110.1016/S0032-3861(02)00490-1 ↗
12. 10.1177/0022034590069010050110.1177/00220345900690100501 ↗
13. 10.1016/S0300-9440(03)00120-610.1016/S0300-9440(03)00120-6 ↗
14. 10.1023/B:JTAN.0000027140.27560.d110.1023/B:JTAN.0000027140.27560.d1 ↗
15. Abadie M.J.M. · 2003
16. 10.1016/S0034-3617(10)70215-010.1016/S0034-3617(10)70215-0 ↗
17. 10.1016/j.compositesa.2004.02.01610.1016/j.compositesa.2004.02.016 ↗
18. 10.1177/073168440606519410.1177/0731684406065194 ↗
19. 10.1016/j.compscitech.2006.07.01810.1016/j.compscitech.2006.07.018 ↗
20. 10.1016/j.compscitech.2008.06.02310.1016/j.compscitech.2008.06.023 ↗
21. 10.1177/002199831038502710.1177/0021998310385027 ↗
22. 10.1177/09673911080160070110.1177/096739110801600701 ↗
23. 10.1002/(SICI)1097-4628(19970425)64:4<769::AID-APP16>3.0.CO;2-P10.1002/(SICI)1097-4628(19970425)64:4<769::AID-APP16>3.0.CO;2-P ↗
24. 10.1002/pen.1145410.1002/pen.11454 ↗
25. 10.1016/S0014-3057(01)00244-010.1016/S0014-3057(01)00244-0 ↗
26. 10.1002/app.1040310.1002/app.10403 ↗