Microstructure and composition of multi-layered oxide scale evolved during isothermal exposure of ZrB2–SiC–LaB6 composite to air at 1500°C
Author:
Affiliation:
1. Department of Metallurgical and Materials Engineering, Indian Institute of Technology Kharagpur, Kharagpur, India
Publisher
Informa UK Limited
Subject
Condensed Matter Physics
Link
https://www.tandfonline.com/doi/pdf/10.1080/09500839.2021.1912426
Reference34 articles.
1. Evaluation of ultra-high temperature ceramics foraeropropulsion use
2. The hypersonic environment: Required operating conditions and design challenges
3. Oxidation of ZrB2 and its composites: a review
4. High-Temperature Chemistry and Oxidation of ZrB2Ceramics Containing SiC, Si3N4, Ta5Si3, and TaSi2
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1. Statistical evaluation of mechanical characteristics of hot-pressed ceramics in ZrB2–SiC system;Vestnik Tomskogo gosudarstvennogo universiteta. Matematika i mekhanika;2023
2. Development of functionally graded ZrB2–B4C composites for lightweight ultrahigh-temperature aerospace applications;Ceramics International;2022-11
3. Effect of LaB 6 addition on compressive creep behavior with simultaneous oxide scale growth of spark plasma sintered ZrB 2 ‐SiC composites;Journal of the American Ceramic Society;2022-10-08
4. Oxidation Resistance and Evolution of Multi-layered Oxide Scale During Isothermal and Cyclic Exposure of ZrB2–SiC–LaB6 Composites at 1300 °C to 1500 °C;Metallurgical and Materials Transactions A;2021-11-06
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