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Failure analysis of gas turbine rotor blades
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“Aircraft engines are exposed to extreme environmental factors such as mechanical loadings, high pressures and operating temperatures, and foreign objects. These contribute to the risk of damage to the engine blades [1-4].”
From Automated Defect Detection and Decision-Support in Gas Turbine Blade Inspection (2021) · cites this paper as [4]
Citations
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Metadata
- Authors
- Kumari, S., Satyanarayana, D. V. V., & Srinivas, M.
- Affiliations
- Defence Metallurgical Research Laboratory (IN)
- Corresponding author
- Kumari, Sweety
- Venue
- Engineering Failure Analysis
- Publisher
- Elsevier BV
- Published
- 2014-10
- Volume
- 45
- Pages
- 234-244
- ISSN
- 1350-6307 (ISSN-L)
- OpenAlex
- W2024429458
- Cited by
- 82
- References
- 4
- Citations by year
- 2026: 8 · 2025: 10 · 2024: 8 · 2023: 12 · 2022: 3 · 2021: 11 · 2020: 9 · 2019: 2 · 2018: 5 · 2017: 6 · 2016: 4 · 2015: 4
- FWCI
- 5.44
- Type
- journal article
- Language
- en
- Open access
- closed
- Locations
- Engineering Failure Analysis (publishedVersion)
- Topics
- Physical Sciences › Engineering › Mechanical Engineering › Mechanical Failure Analysis and Simulation
- Physical Sciences › Engineering › Mechanical Engineering › High Temperature Alloys and Creep
- Physical Sciences › Materials Science › Surfaces, Coatings and Films › High-Temperature Coating Behaviors
- Keywords
- turbine rotor blades, nickel-based superalloy, localized oxidation, coating delamination, fatigue crack initiation, blade fracture
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