Percolation effects on fracture in ductile-phase toughened oxide coatings

Abstract The toughness and damage behaviors of ductile-phase toughened oxide coatings were characterized as the reinforcement volume fraction varied across the percolation threshold. The coatings, consisting of Ni particles in a borate glass-ceramic matrix, showed a rising resistance curve, with the extent of stable crack growth increasing with Ni content. While initiation toughness was relatively insensitive to reinforcement topology, peak toughness increased sharply once the Ni reinforcement percolated, reaching a maximum value of ~ 160 J/m 2 in an interpenetrating composite coating with 35 vol% Ni. This toughness is sufficiently high to resist failure in the target application of rocket engine turbomachinery, where coatings must withstand rapid thermal transients upon engine startup and shutdown. Characterization of the crack path confirmed that this toughening increment corresponded to a transition from crack deflection to crack bridging as the dominant toughening mechanism. The implications of these results on design of ductile-phase toughened coatings are discussed. Graphical abstract

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Journal
Journal of materials research/Pratt's guide to venture capital sources
Published
2025-03-25
DOI
https://doi.org/10.1557/s43578-025-01560-4
Primary Topic
High-Temperature Coating Behaviors
Type
article
Field-Weighted Citation Impact
0.00

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article

Percolation effects on fracture in ductile-phase toughened oxide coatings

Zachary C. Cordero, Isha Gupta, Annika M. L. Vaidyanathan, Aliya K. Kpamegan
Journal of materials research/Pratt's guide to venture capital sources
High-Temperature Coating Behaviors
article

Percolation effects on fracture in ductile-phase toughened oxide coatings

Zachary C. Cordero, Isha Gupta, Annika M. L. Vaidyanathan, Aliya K. Kpamegan
article en

Abstract

Abstract The toughness and damage behaviors of ductile-phase toughened oxide coatings were characterized as the reinforcement volume fraction varied across the percolation threshold. The coatings, consisting of Ni particles in a borate glass-ceramic matrix, showed a rising resistance curve, with the extent of stable crack growth increasing with Ni content. While initiation toughness was relatively insensitive to reinforcement topology, peak toughness increased sharply once the Ni reinforcement percolated, reaching a maximum value of ~ 160 J/m 2 in an interpenetrating composite coating with 35 vol% Ni. This toughness is sufficiently high to resist failure in the target application of rocket engine turbomachinery, where coatings must withstand rapid thermal transients upon engine startup and shutdown. Characterization of the crack path confirmed that this toughening increment corresponded to a transition from crack deflection to crack bridging as the dominant toughening mechanism. The implications of these results on design of ductile-phase toughened coatings are discussed. Graphical abstract

Journal of materials research/Pratt's guide to venture capital sourcesVol. 40(13)
American Institute of Aeronautics and Astronautics (US), Massachusetts Institute of Technology (US)
Massachusetts Institute of Technology
Openalex Percentile: Top 92%
High-Temperature Coating Behaviors
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Percolation effects on fracture in ductile-phase toughened oxide coatings — Zachary C. Cordero, Isha Gupta, et al. · Journal of materials research/Pratt's guide to venture capital sources (2025) | TGRS Research Map | TGRS