The investigation utilized uniaxial step-wise compression creep tests on specimens subjected to temperatures ranging from 20 °C to 800 °C. The primary focus was to compare and analyze the effects of aggregate types on total strain, load-induced thermal strain (LITS), creep deformation, and rate patterns. This experimental design allowed for a direct comparison of how normal-weight and lightweight aggregates respond to thermal exposure and subsequent mechanical loading.

Below 200 °C, the LWAC exhibited a higher load-induced thermal strain than the NWAC. Specifically, the LITS of the lightweight concrete was approximately 83.3% higher than that of the normal-weight concrete. The study attributes this difference to the lower modulus of the lightweight aggregate, which results in a different initial strain response compared to the denser normal-weight material.

A significant divergence in behavior was observed above 400 °C. At this temperature threshold, the NWAC experienced a rapid increase in creep strain. The researchers identified the thermal expansion mismatch between the aggregate and the cement paste at the interface transition zone (ITZ) as the driving factor for this accelerated deformation. This mismatch creates internal stresses that alter the creep rate of the normal-weight concrete.

In contrast, the LWAC containing fly ash ceramsite aggregate displayed a different response mechanism. The porous structure of the fly ash ceramic aggregate was found to play a “thermal mitigating” effect. This porosity effectively inhibited the propagation of microcracks within the material. As a result, the LWAC was able to maintain a longer steady-state creep period compared to the NWAC, indicating a more stable deformation profile under sustained load after high-temperature exposure.

Scanning electron microscopy (SEM) analysis provided microstructural evidence supporting these mechanical observations. At high temperatures, the ITZ of the NWAC developed tensile cracks measuring several micrometers in width. These cracks are consistent with the rapid increase in creep strain observed in the normal-weight specimens. Conversely, the LWAC specimens maintained a relatively intact structure at the interface, with fewer signs of the microcracking seen in the NWAC.

The study also evaluated the applicability of the Burgers model to the creep data of the lightweight concrete. The fitting degree of the Burgers model for the LWAC creep data was high, with an R-squared value of 0.99. This high correlation verifies the model’s applicability in describing the deceleration and constant-speed creep behavior of LWAC after high-temperature treatment. The successful fit provides a mathematical framework for characterizing the specific creep phases of this material.

The findings reveal the deformation mechanism of fly ash ceramic aggregate in high-temperature environments. The research provides a theoretical basis for the design and post-disaster assessment of the fire resistance of LWAC structures. By understanding how the porous aggregate mitigates thermal stresses and inhibits crack propagation, the study offers insights into the long-term deformation performance of lightweight concrete after exposure to extreme temperatures.

Subject of Research: Creep behavior of lightweight concrete containing fly ash ceramsite aggregate after high-temperature exposure

Article Title: Creep behavior of lightweight concrete containing fly ash ceramsite aggregate after exposure to high temperatures

Article References: Xiao, D., Chen, S., Wen, L., Dou, Y., Liu, H., & Zhao, J. (2026). Creep behavior of lightweight concrete containing fly ash ceramsite aggregate after exposure to high temperatures. Scientific Reports. https://doi.org/10.1038/s41598-026-77256-4

Image Credits: AI Generated

DOI: 10.1038/s41598-026-77256-4

Keywords: lightweight concrete, fly ash ceramsite, creep behavior, high temperature, structural engineering, load-induced thermal strain, interface transition zone, Burgers model, Creep, behavior, lightweight, concrete

The research team set out to determine whether thermomechanical treatment, or TMT, could reshape the internal architecture of an as-forged ODS-FeCrAl alloy in ways that would improve its resistance to creep at 650 degrees Celsius, a temperature squarely relevant to advanced reactor operation. Thermomechanical treatment is a deceptively simple concept: the alloy is heated to a chosen temperature and then deformed by a controlled amount, forcing the grains and defects inside the metal to reorganize. But the outcome depends exquisitely on the parameters chosen. The researchers applied treatments at different temperatures and deformation levels, and then subjected the processed samples to a battery of creep tests under stresses ranging from 120 to 180 megapascals. To understand what they were seeing, they characterized grain morphology, dislocation structures, oxide nanoparticles, and fracture surfaces both before and after creep, building a detailed picture of how microstructure governs deformation.

The results reveal a striking sensitivity to processing conditions. When the alloy was treated at 950 degrees Celsius with 65 percent deformation, it delivered the best creep performance of any condition tested. At the benchmark condition of 650 degrees Celsius and 150 megapascals, this sample exhibited a minimum creep rate of 5.87 times ten to the minus five per hour—nearly half the rate of 1.10 times ten to the minus four per hour measured in the as-forged material. In practical terms, the treated alloy deforms under load at a substantially slower pace, which translates directly into longer, more predictable service life for reactor components. The improvement did not come from any single microstructural feature, the authors suggest, but from a favorable balance among three competing factors: the shape of the grains, the amount of dislocation density stored in the metal, and the ability of the oxide dispersoids to pin those dislocations in place.

That balance proved fragile. When the deformation level was pushed to 80 percent at the same 950-degree treatment temperature, the alloy’s grains became strongly elongated and anisotropic, and the creep performance deteriorated markedly. The heavily deformed sample not only crept faster but also failed in a distinctive way: its fracture surface was elliptical rather than flat, and it displayed parallel cracks, signatures of damage accumulating along the elongated grain boundaries. This finding carries an important lesson for alloy engineers. More deformation is not automatically better. Excessive straining during thermomechanical processing can introduce grain-morphology anisotropy that creates easy pathways for creep damage, undermining the very strengthening mechanisms the treatment is meant to enhance. The parallel cracks observed on the fracture surface point to deformation localized along boundaries oriented unfavorably with respect to the applied stress, a classic failure mode in highly textured, elongated-grain materials.

Temperature, too, proved to be a critical variable. When the treatment temperature was raised to 1150 degrees Celsius at the same 65 percent deformation, the resulting sample actually crept faster than the as-forged alloy, although it survived slightly longer before rupturing. This mixed outcome—worse steady-state creep rate but marginally improved rupture life—illustrates that the two headline metrics of creep performance do not always move together. A material can resist final fracture while still deforming steadily at an unacceptably high rate, or vice versa. For reactor designers, who must guarantee both dimensional stability and structural integrity over decades, such partial improvements are of limited value. The authors conclude that the 1150-degree treatment offered only a limited overall benefit, underscoring that excessively high processing temperatures can degrade the fine microstructural features that give ODS alloys their creep resistance, likely by coarsening grains or altering the dislocation substructure.

To probe how the best-performing microstructure would hold up under varying loads, the team conducted stress-dependent creep tests across the 120 to 180 megapascal range. The 950-degree, 65-percent sample maintained relatively low creep rates at 120 and 150 megapascals, confirming its robustness under moderate loading conditions typical of cladding service. However, when the stress was raised to 180 megapascals, the sample rapidly entered the accelerated creep stage, the terminal phase in which damage accumulates quickly and rupture follows. This threshold-like behavior is characteristic of dispersion-strengthened alloys, in which a population of hard oxide particles imposes an effective barrier to dislocation motion. Below a certain stress, dislocations are forced to climb over or bypass the particles at great energetic cost, keeping deformation slow; above it, the barriers are overwhelmed and the material yields to accelerated flow.

The underlying physics of this behavior connects to decades of theory on particle-strengthened creep. In ODS alloys, nanometer-scale oxide dispersoids interact with moving dislocations through what researchers describe as an attractive interaction: dislocations pin to the particles and must climb over them, a process that imposes a threshold stress below which creep is dramatically suppressed. The effectiveness of this mechanism depends on the spacing, size, and stability of the particles, as well as on the dislocation network that threads between them. Thermomechanical treatment perturbs all of these variables at once. Moderate deformation multiplies dislocations, creating a dense storage network that further impedes flow, while the oxide particles pin that network in place and prevent it from annealing away. But if the deformation is too severe or the temperature too high, the grain structure becomes elongated and anisotropic, or the delicate dislocation-particle balance is disrupted, and the alloy’s defenses crumble.

Why does this matter beyond the laboratory? ODS-FeCrAl alloys are being developed as accident-tolerant fuel cladding, a response to the lessons of severe reactor accidents in which conventional zirconium-alloy cladding reacted violently with steam at high temperature. The aluminum in FeCrAl forms a protective alumina scale that resists oxidation even under loss-of-coolant accident conditions, buying precious time during an emergency. But cladding tubes must also withstand sustained mechanical loading at operating temperatures for years, which is where creep becomes the limiting factor. A cladding material that slowly stretches under the weight and pressure it carries will eventually thin, bulge, or crack. The new results suggest that processing routes can be tuned to deliver both oxidation resistance and creep stability in a single material, resolving a trade-off that has hampered the alloy class since its inception.

The study’s broader message is one of cautious optimization. Moderate thermomechanical treatment—here, 950 degrees Celsius with 65 percent deformation—improves creep stability by balancing grain morphology, dislocation storage, and dispersoid pinning, while excessive deformation or an excessively high treatment temperature is detrimental. There is no universal recipe; the sweet spot reflects a specific interplay between the alloy’s starting condition and the processing parameters. As advanced reactors move from design boards toward construction, findings like these provide the processing-microstructure-property maps that engineers need to manufacture cladding that is not only accident-tolerant on paper but reliably stable in service. The work was supported by the National Natural Science Foundation of China, the S&T Program of Hebei, and the Beijing Natural Science Foundation, and it adds a practical, quantitative demonstration that in high-temperature alloys, how a metal is worked can matter as much as what it is made of.

Subject of Research: Thermomechanical processing effects on the microstructure and high-temperature creep behavior of oxide-dispersion-strengthened FeCrAl alloys for advanced nuclear reactors

Article Title: Effects of thermomechanical treatment on the microstructure and creep behavior of an ODS-FeCrAl alloy

Article References: Han, L., Jia, H., Wang, Y., Guan, H., Yin, C., Wang, Y., Tong, Z., Zheng, W., Wang, Y., & Zhou, Z. (2026). Effects of thermomechanical treatment on the microstructure and creep behavior of an ODS-FeCrAl alloy. Journal of Materials Science. https://doi.org/10.1007/s10853-026-13833-2

Image Credits: AI Generated

DOI: 10.1007/s10853-026-13833-2

Keywords: ODS-FeCrAl, thermomechanical treatment, creep behavior, nuclear cladding, oxide dispersion strengthening, grain morphology, dislocation structure, accident-tolerant fuel, high-temperature alloys, microstructure, Journal of Materials Science, advanced reactors