Failure investigation of fatigue crack initiation and propagation in compressor blade
Bibliographic record
Abstract
No abstract is available for this record. The assistant can identify its topic from the title, but cannot infer the study’s results.
Source: Not provided · Quality: missing
Research context
OpenAlex topics: Fatigue and fracture mechanics · High Temperature Alloys and Creep · Turbomachinery Performance and Optimization
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (26)
Show source-provided references
1. M.P. Boyc, Gas Turbine Engineering Handbook, Fourth Edition, Gas Turbine Engineering Handbook, Fourth Edition (2011) 1–956. doi: 10.1016/C2009-0-64242-2.10.1016/C2009-0-64242-2 ↗
2. Cooling channel blockage effect on TBC and substrate behavior in a Gas turbine blade failure10.1016/j.engfailanal.2022.106682 ↗
3. Failure Analysis of a GTD-111 Turbine Blade Using Metallurgical Analysis and Fractography10.1007/s11668-019-00732-9 ↗
4. A comprehensive review on mechanical failures cause vibration in the gas turbine of combined cycle power plants10.1016/j.engfailanal.2022.106094 ↗
5. Fatigue crack growth simulation in a first stage of compressor blade10.1016/j.engfailanal.2014.06.018 ↗
6. Stress analysis of a second stage gas turbine blade under asymmetric thermal gradient
7. Failure analysis of a gas turbine blade: A review10.1088/1757-899X/1034/1/012156 ↗
8. Fatigue crack growth prediction in a gas turbine casing10.1016/j.engfailanal.2014.05.010 ↗
9. On the failure behavior of fifth stage gas turbine blade10.1016/j.engfailanal.2020.104766 ↗
10. M. García-Martínez, J.C. del Hoyo Gordillo, M.P. Valles González, A. Pastor Muro, B. González Caballero, Failure study of an aircraft engine high pressure turbine (HPT) first stage blade, Eng Fail Anal 149 (2023) 107251. doi: 10.1016/J.ENGFAILANAL.2023.107251.10.1016/j.engfailanal.2023.107251 ↗
11. Failure analysis of a second-stage rotor blade in TRT10.1016/j.engfailanal.2022.106978 ↗
12. Mechanism and modeling of fatigue crack initiation and propagation in the directionally solidified CM186 LC blade of a gas turbine engine10.1016/j.engfracmech.2019.106842 ↗
13. An experimental and numerical study of the solid particle erosion damage in an industrial cement large-sized fan10.1016/j.engfailanal.2023.107058 ↗
14. Numerical simulation method of surge experiments on gas turbine engines10.1016/j.cja.2022.08.007 ↗
15. Unsteady body force model for rotating stall in axial compressor with various inlet conditions10.15632/jtam-pl/174960 ↗
16. Vibrational responses and fatigue life of dynamic blades for compressor in gas turbines10.1016/j.engfailanal.2023.107827 ↗
17. Experimental and numerical analysis of Pitting Corrosion in CUSTOM 450 Stainless Steel10.1016/j.engfailanal.2021.105589 ↗
18. Fretting fatigue in dovetail blade roots: Experiment and analysis10.1016/j.triboint.2006.02.044 ↗
19. An overview on how failure analysis contributes to flight safety in the portuguese air force10.1016/j.engfailanal.2016.03.003 ↗
20. Failure analysis of compressor blades of a helicopter engine10.1016/j.engfailanal.2019.05.024 ↗
21. M. Lavella, D. Botto, Fretting Fatigue Analysis of Additively Manufactured Blade Root Made of Intermetallic Ti-48Al-2Cr-2Nb Alloy at High Temperature, Materials 2018, Vol. 11, Page 1052 11 (2018) 1052. doi: 10.3390/MA11071052.10.3390/ma11071052 ↗
22. Investigation and efficient modeling of an dovetail attachment in aero-engine10.1016/j.mspro.2014.07.495 ↗
23. Experimental crack propagation and failure analysis of the first stage compressor blade subjected to vibration10.1016/j.engfailanal.2009.02.014 ↗
24. Dynamic and fatigue compressor blade characteristics during fluid-structure interaction: Part I—Blade modelling and vibration analysis10.1016/j.engfailanal.2017.02.002 ↗
25. Fatigue Fracture of a Compressor Blade of an Aeroengine: What Caused this Failure10.1007/s11668-015-9961-4 ↗
26. Total Life Estimation of a Compressor Blade with Corrosion Pitting, SCC and Fatigue Cracking10.1007/s11668-018-0417-5 ↗