The DOI matches its Crossref record; 13 of the 13 references it cites were found in a registry or an index.
Numerical stress and crack initiation analysis of the compressor blades after foreign object damage subjected to high-cycle fatigue
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“Detecting those defect types is important as they can lead to fatigue cracks [13] resulting in material separation and breakage of the entire blade under centrifugal load [14], which has the potential to cause severe damage to the engine and aircraft.”
From Automated Defect Detection and Decision-Support in Gas Turbine Blade Inspection (2021) · cites this paper as [13]
Citations
Cites
Statistical evaluation of strain-life fatigue crack initiation predictions
Meggiolaro, M. A. (2003) · International Journal of Fatigue · doi:10.1016/j.ijfatigue.2003.10.003 · Cited by 262
Failure analysis of turbine disc of an aero engine
Witek, L. (2005) · Engineering Failure Analysis · doi:10.1016/j.engfailanal.2004.12.028 · Cited by 146
Self-citationWitek, L. (2009) · Engineering Failure Analysis · doi:10.1016/j.engfailanal.2009.02.014 · Cited by 114
Self-citationFailure analysis of Ti6Al4V gas turbine compressor blades
Kermanpur, A., Sepehri‐Amin, H., Ziaei‐Rad, S., Nourbakhshnia, N., & Mosaddeghfar, M. (2007) · Engineering Failure Analysis · doi:10.1016/j.engfailanal.2007.11.018 · Cited by 106
Analysis of a J69-T-25 engine turbine blade fracture
Park, M., Hwang, Y., Choi, Y.-S., & Kim, T.-G. (2002) · Engineering Failure Analysis · doi:10.1016/s1350-6307(02)00003-1 · Cited by 77
Failure analysis of gas turbine blades in a thermal power plant
Vardar, N., & Ekerim, A. (2006) · Engineering Failure Analysis · doi:10.1016/j.engfailanal.2006.06.001 · Cited by 69
Analysis of superalloy turbine blade tip cracking during service
Xie, Y., Wang, M., Zhang, G., et al. (2005) · Engineering Failure Analysis · doi:10.1016/j.engfailanal.2005.07.022 · Cited by 67
Fracture analysis of compressor blade of a helicopter engine
Witek, L., Wierzbińska, M., & Poznańska, A. (2008) · Engineering Failure Analysis · doi:10.1016/j.engfailanal.2008.10.022 · Cited by 55
Self-citationFatigue failure of a compressor blade
Lourenço, N. J., Graça, M. L. A., Franco, L. A. L., & Silva, O. M. M. (2007) · Engineering Failure Analysis · doi:10.1016/j.engfailanal.2007.11.006 · Cited by 48
Failure analysis of a set of compressor blades
Silveira, E., Atxaga, G., & Irisarri, A. M. (2007) · Engineering Failure Analysis · doi:10.1016/j.engfailanal.2007.10.002 · Cited by 41
Research works printed but not linked: 3
- Poznanska A, Sniezek M, Wierzbinska M. Pitting corrosion – main factor generating fracture of the compressor of aeroengine blades under operation. In: Proceedings of IX conference. Turbomachinery, Rzeszow; 2003 [in Polish].
- Xu, 2007, An investigation on the failed blades in a locomotive turbine, Eng Fail Anal, 14, 1322, 10.1016/j.engfailanal.2006.11.041 · DOI
- Witek L, Kowalski T, Mamrowicz J. Numerical stress and fatigue analysis of the first stage of turbine for helicopter engine. In: Proceedings of international conference on aeronautical fatigue, Napoli; 2007.
Cited by
Sorted by citations
Automated Defect Detection and Decision-Support in Gas Turbine Blade Inspection
Aust, J., Shankland, S., Pons, D., Mukundan, R., & Mitrovic, A. (2021) · Aerospace · doi:10.3390/aerospace8020030 · Cited by 66
“Detecting those defect types is important as they can lead to fatigue cracks [13] resulting in material separation and breakage of the entire blade under centrifugal load [14], which has the potential to cause severe damage to the engine and aircraft.”
BackgroundTaxonomy of Gas Turbine Blade Defects
Aust, J., & Pons, D. (2019) · Aerospace · doi:10.3390/aerospace6050058 · Cited by 68
Metadata
- Authors
- Witek, L.
- Affiliations
- Rzeszów University of Technology (PL)
- Corresponding author
- Witek, Lucjan
- ORCID
- Witek, Lucjan
- Venue
- Engineering Failure Analysis
- Publisher
- Elsevier BV
- Published
- 2011-12
- Volume
- 18
- Issue
- 8
- Pages
- 2111-2125
- ISSN
- 1350-6307 (ISSN-L)
- OpenAlex
- W1998222420
- Cited by
- 56
- References
- 13
- Citations by year
- 2026: 3 · 2025: 1 · 2024: 4 · 2023: 3 · 2022: 2 · 2021: 2 · 2020: 8 · 2019: 3 · 2018: 6 · 2017: 4 · 2016: 3 · 2015: 2 · 2014: 10 · 2013: 3 · 2012: 2
- FWCI
- 7.24
- Type
- journal article
- Language
- en
- Open access
- closed
- Licence
- Locations
- Engineering Failure Analysis (publishedVersion)
- Topics
- Physical Sciences › Engineering › Mechanics of Materials › Fatigue and fracture mechanics
- Physical Sciences › Engineering › Mechanical Engineering › Bladed Disk Vibration Dynamics
- Physical Sciences › Engineering › Mechanical Engineering › Mechanical Failure Analysis and Simulation
- Keywords
- compressor blades, foreign object damage, high cycle fatigue, crack initiation, transverse vibration, V-notch, fatigue crack growth, Miner's rule, linear damage summation, fatigue behavior, notch radius, ultimate tensile strength, vibration amplitude
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