首页|Corrigendum to “Turbine wheel fracture analysis of Jet Fuel Starter (JFS) engine used on F16 military aircraft” [Eng. Fail. Anal. 128 (2021) 105616] (Engineering Failure Analysis (2021) 128, (S1350630721004775), (10.1016/j.engfailanal.2021.105616))
Corrigendum to “Turbine wheel fracture analysis of Jet Fuel Starter (JFS) engine used on F16 military aircraft” [Eng. Fail. Anal. 128 (2021) 105616] (Engineering Failure Analysis (2021) 128, (S1350630721004775), (10.1016/j.engfailanal.2021.105616))
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NSTL
Elsevier
? 2021 Elsevier LtdThe author regret, Ref. [16] should be read as [16] 1. HBFM. 1st Air Maintenance Factory Directorate, Eskisehir, Turkey. The author regret, Ref. [16] is inadvertently omitted for Figs. 4–10. The figures should be read as: Fig. 4. The damaged turbine wheel [16]. Fig. 5. The material loss and part breaking from turbine wheel [16]. Fig. 6. Cracks on blade surface of turbine wheel [16]. Fig. 7. The detected cracks via BSM method [16]. Fig. 8. Asymmetrical circumferential wearing, crushing and starching on turbine wheel aft surface [16]. Fig. 9. Heat affected zones and discoloration on blade surfaces of turbine blade [16]. Fig. 10. Multiple cracks and pitting surfaces on turbine wheel blade [16]. The authors would like to apologise for any inconvenience caused.
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1’st Air Maintenance Factory Directorate (1.HBFM) General Directorate of Military Factories (AFGM) Ministry of National Defence (MND)
NSTL
Elsevier
