The DOI matches its Crossref record; 4 of the 4 references it cites were found in a registry or an index.
Failure analysis of gas turbine rotor blades
Overview
Integrity signals
Registry
Cites
Statistics
Verification
Claims the paper makes
Claims other papers make about this one
Each is checked against this paper’s own text: does it say what the citing paper says it does?
In the citing paper
“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
Cites
Natural Frequencies of Turbine Blading -- A Survey
Rao, J. S. (1973) · The Shock and Vibration Digest · doi:10.1177/058310247300501002 · Cited by 36
Walls, D. P., deLaneuville, R. E., & Cunningham, S. E. (1997) · Journal of Engineering for Gas Turbines and Power · doi:10.1115/1.2815538 · Cited by 35
Evaluation of service-induced damage and restoration of cast turbine blades
Persson, C., & Persson, P. O. (1993) · Journal of Materials Engineering and Performance · doi:10.1007/bf02661742 · Cited by 21
Creep Failure Assessment of a Turbine Disc Using Non-Linear Finite Element Method
Hou, J., Wicks, B. J., Stocks, G., Slater, S., & Antoniou, R. A. (1999) · Cited by 11
Research works printed but not linked: 4
- Yao, 2002, Analysis and prevention of turbine breakage in an engine starting motor, Mater Mech Eng, 26, 40
- Liu, 2007, Fracture failure analysis of high-pressure turbine blades of II stage, Heat Treat Met, 32, 714
- Tao, 2002, Analysis and prevention of turbine breakage in an engine starting motor, Mater Mech Eng, 26, 40
- Reddy TSR, et al. A review of recent aeroelastic analysis methods for propulsion at NASA Lewis research centre. NASA Technical Paper 3406; 1993.
Cited by
Sorted by citations
A critical review on gas turbine cooling performance and failure analysis of turbine blades
Chowdhury, T. S., Mohsin, F. T., Tonni, M. M., Mita, M. N. H., & Ehsan, M. M. (2023) · International Journal of Thermofluids · doi:10.1016/j.ijft.2023.100329 · Cited by 170
An Improved Multiple Signal Classification for Nonuniform Sampling in Blade Tip Timing
Wang, Z., Yang, Z., Wu, S., Li, H., Tian, S., & Chen, X. (2020) · IEEE Transactions on Instrumentation and Measurement · doi:10.1109/tim.2020.2980912 · Cited by 116
Failure analysis of gas and wind turbine blades: A review
Mourad, A. I., Almomani, A. F., Sheikh, I. A., & Elsheikh, A. H. (2023) · Engineering Failure Analysis · doi:10.1016/j.engfailanal.2023.107107 · Cited by 111
Hot corrosion failure in the first stage nozzle of a gas turbine engine
Salehnasab, B., Poursaeidi, E., Mortazavi, S. A., & Farokhian, G. H. (2015) · Engineering Failure Analysis · doi:10.1016/j.engfailanal.2015.11.057 · Cited by 106
Gao, H., Fei, C., Bai, G.-C., & Ding, L. (2015) · Aerospace Science and Technology · doi:10.1016/j.ast.2015.12.017 · Cited by 79
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
About these checks
Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.
Statistics and arithmetic are recomputed, not judged.
Confidence bands are shown only for fields calibrated on our annotated test set. None is calibrated yet, so no band is shown.
What counts as a claim ›How we measure confidence ›How we check this ›
Are you an author, or do you see a problem with this page? Request a review
How to cite
Cite CoChat for the checks on this page, and the paper for its own findings.
- This page
- CoChat. (2026). Citation check: Failure analysis of gas turbine rotor blades. https://app.cochat.ai/papers/10.1016/j.engfailanal.2014.06.003
- The paper
- Kumari, S., Satyanarayana, D. V. V., & Srinivas, M. (2014). Failure analysis of gas turbine rotor blades. Engineering Failure Analysis. https://doi.org/10.1016/j.engfailanal.2014.06.003