Formation of hole-edge cracks in a combustor liner of an aero engine-Reference-Cited by-同舟云学术

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Formation of hole-edge cracks in a combustor liner of an aero engine

Published:2015-09 Issue: Volume:55 Page:148-156
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Chen Y.D.,Feng Q.,Zheng Y.R.,Ding X.F.

Funder

National High Technology Research and Program of China

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference14 articles.

1. Failure analysis of an aero-engine combustor liner;Lv;Eng Fail Anal,2010

2. Thermal fatigue analysis and life prediction of combustor liner;Geng;J Mech Strength,2007

3. Study on initiation and propagation mechanism of crack on dilution hole edge in combustor liner;Geng;J Propulsion Technol,2006

4. Oxidation behavior of bilayered ceramic particle-reinforced enamel composite coating on nickel-based superalloy;Shen;Corros Sci Prot Technol,2012

5. Process of base coat free single enameling on steel;Zhang;J Dalian Jiaotong Univ,2008

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1. Thermal fatigue behaviors of thin-walled structures with holes: Experiments and phase field fracture modeling;International Journal of Fatigue;2024-08

2. Phase field modeling of thermal fatigue crack growth in elastoplastic solids and experimental verification;Mechanics of Materials;2024-01

3. Very-High-Cycle-Fatigue Property of IN 718 Manufactured by Selective Laser Melting at Elevated Temperature: Microstructure-Related Failure Behavior and Life Prediction;Journal of Materials Engineering and Performance;2023-06-08

4. Unified constitutive modeling of Haynes 230 including cyclic hardening/softening and dynamic strain aging under isothermal low-cycle fatigue and fatigue-creep loads;International Journal of Plasticity;2021-03

5. Effect of cooling hole configurations on combustion and heat transfer in an aero-engine combustor;Applied Thermal Engineering;2021-01

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