Impacts of prior ablative damage and fiber breakage influence on flexural strength of 2D C/C composites with and without secondary high temperature treatments
Source abstract
Abstract
For reliable use of 2D Carbon–Carbon (C/C) composites in aerostructural applications, the sensitivity of the strength properties to prior damage (ablative and fiber breakage) needs to be assessed. A 0°/90° carbon fiber preform underwent a 6-cycle polymer infiltration and pyrolysis (PIP) schedule (standard process (SP)) using phenolic resin. A subset of samples was subjected to a high temperature treatment (HTT) at 2400 °C followed by another two PIP cycles. The HTT specimens exhibited a statistically significant increase in flexural strength compared to the SP specimens, due to an increased ordering of the matrix atomic structure, higher bulk density, and lower porosity. The HTT C/C presented a mixed mode failure type in flexural testing, with fiber-matrix debonding and fiber pullout leading to interlaminar shear at the neutral axis of the sample. The SP C/C failed from a crack emanating at the tensile free surface. The HTT C/C was more resistant to ablation than the SP C/C, with the HTT samples not exhibiting a statistically significant debit (6.6 %) in flexural strength due to prior ablation. Conversely, the SP specimens exhibited a 57.9 % reduction in strength after prior ablation. For the SP C/C, the presence of a small notch resulted in broken fibers and load redistribution, which significantly debited the flexural strength, although the notch had minimal effect on the flexural strength of previously ablated samples. This work quantifies the residual strength in the case of prior damage, thus identifying the processing-structure-properties relationships and mechanisms that regulate the durability of C/C composites. • For standard processed (SP) 2D C/C composite, a high temperature treatment (HTT) increased strength. • Failure mechanism shifted from tensile cracking (SP C/C) to delamination (HTT C/C). • HTT led to increased degree of matrix atomic ordering, density, thermal conductivity. • Prior ablation for SP decreased strength and had insignificant effect on HTT C/C. • A notch in SP C/C resulted in decreased or minimal changes in strength for cases without or with prior ablation, respectively.
Source: openalex_inverted_index · Quality: baseline
Research context
OpenAlex topics: Advanced ceramic materials synthesis · Graphite, nuclear technology, radiation studies · Graphene research and applications
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (42)
Show source-provided references
1. Fitzer · 1998
2. The properties of carbon-carbon composites
3. Thermal ablation experiments of carbon phenolic and SiC-Coated carbon composite materials using a high-velocity oxygen-fuel torch10.3390/ma16051895 ↗
4. Carbon–carbon composites in aerospace engineering
5. Effect of density and fibre orientation on the ablation behaviour of carbon-carbon composites10.1016/S1872-5805(09)60023-8 ↗
6. Tensile strength of carbon–carbon composites: I–effect of C–C density10.1177/0021998304044763 ↗
7. The crack development on the micro-and mesoscopic scale during the pyrolysis of carbon fibre reinforced plastics to carbon/carbon composites10.1016/j.compositesa.2007.06.013 ↗
8. Phenolic polymer infiltration and pyrolysis process for additively manufactured carbon/PEEK composites to produce carbon–carbon composites
9. The effect of pyrolysis on the mechanical properties and microstructure of carbon fiber‐reinforced and stabilized fiber‐reinforced phenolic resins for carbon/carbon composites10.1002/pc.750140310 ↗
10. Oxidation behavior and protection of carbon/carbon composites10.1016/0008-6223(87)90197-7 ↗
11. A new structural model of glass-like carbon10.1016/S0008-6223(01)00130-0 ↗
12. Characterization of carbon-carbon composites—Ii: oxidation behaviour10.1016/0008-6223(81)90098-1 ↗
13. Influence of matrix precursor on the oxidation behavior of carbon-carbon composites10.1016/0008-6223(93)90011-X ↗
14. Oxidation of carbon derived from phenolic resin10.1016/0008-6223(78)90109-4 ↗
15. Comparative study on the graphitization index of carbonaceous reducing agents used in silicon smelting10.1007/s12633-024-02910-3 ↗
16. Catalytic graphitization behavior of phenolic resins by addition of in situ formed nano-Fe particles10.1016/j.physe.2018.03.013 ↗
17. Why some carbons may or may not graphitize? The point of view of thermodynamics10.1016/j.carbon.2019.04.018 ↗
18. The effect of heat-treatment temperature (HTT) on the carbon matrix development of both polyarylacetylene-and phenolic-derived carbon–Carbon (C/C) composites10.1177/00219983231191165 ↗
19. Effect of graphitization temperature on microstructure, mechanical and ablative properties of C/C composites with pitch and pyrocarbon dual-matrix10.1016/j.ceramint.2022.09.269 ↗
20. Graphitization of carbon fibre/glassy carbon composites10.1016/0008-6223(74)90067-0 ↗
21. High-temperature oxidation behaviour of carbon materials in air10.1016/0008-6223(93)90148-4 ↗
22. Oxidation and fracture of a woven 2D carbon-carbon composite10.1016/0008-6223(91)90163-D ↗
23. Notch effects in carbon matrix composites10.1111/j.1151-2916.1994.tb04510.x ↗
24. Influence of material and process parameters on microstructure evolution during the fabrication of carbon–carbon composites: a review10.1007/s10853-021-06401-3 ↗
25. The effect of carbon fabric treatment on delamination of 2D-C/C composites10.1016/j.compscitech.2006.03.025 ↗
26. Microstructure and ablation performances of dual-matrix carbon/carbon composites10.1016/j.carbon.2006.01.017 ↗
27. Directional thermophysical, ablative and compressive behavior of 3D carbon/carbon composites10.1016/j.ceramint.2015.04.048 ↗
28. Sublimation and oxidation zone ablation behavior of carbon/carbon composites10.1016/j.ceramint.2015.08.043 ↗
29. ASTM C20-00-Standard test methods for apparent porosity, water absorption, apparent specific gravity
30. The surface topography and microstructure change of densified nanopore nuclear graphite impregnated with polyimide and irradiated by xenon ions10.1016/j.apsusc.2020.147408 ↗
31. Impact of pre-existing crystal lattice defects on the accumulation of irradiation-induced damage in a C/C composite10.1016/j.jnucmat.2022.153684 ↗
32. 2013
33. 2013
34. Fatemi · 2001
35. 1996
36. Ablation performance of rare Earth oxide (REO)-stabilized tetragonal and cubic zirconia coatings as a thermal protection system (TPS) for carbon/carbon composites10.1016/j.jeurceramsoc.2023.06.028 ↗
37. Residual elastic strain and survivability of stabilized zirconia coated carbon-carbon (C/C) composite10.1016/j.surfcoat.2023.129811 ↗
38. The role of additively manufactured niobium alloy C103 substrate's surface finish and corner geometry on the silicide diffusion coating's performance10.1016/j.surfcoat.2024.130510 ↗
39. Slow crack growth in laminate composites via in-situ X-ray tomography and simulations10.1016/j.ijfatigue.2021.106612 ↗
40. Observing progressive damage in carbon fiber epoxy laminate composites via 3D in-situ X-ray tomography10.1016/j.engfracmech.2021.107626 ↗
41. Fracture toughness of carbon-carbon composites10.1177/002199837300700101 ↗
42. Evolution of microstructure and properties of phenolic resin-based carbon/carbon composites during pyrolysis10.1016/S0254-0584(01)00358-3 ↗