Influence of residual stress distribution and microstructural characteristics on fatigue failure mechanism in Ni-based Superalloy
The influence of residual compressive stress (RCS) depth and magnitude generated through surface treatments such as shot peening (SP), deep cold rolling (DCR), and vibro-peening (VP) on fatigue crack mechanisms of Ni-based superalloy is investigated. The fatigue performance with associated failure m...
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sg-ntu-dr.10356-1595742022-06-28T01:02:30Z Influence of residual stress distribution and microstructural characteristics on fatigue failure mechanism in Ni-based Superalloy Kumar, Dharmesh Idapalapati, Sridhar Wang, Wei School of Mechanical and Aerospace Engineering Advanced Remanufacturing andTechnology Centre, A*STAR Singapore Institute of ManufacturingTechnology, A*STAR Engineering::Mechanical engineering Deep Cold Rolling Electron-Back Scattered Diffraction The influence of residual compressive stress (RCS) depth and magnitude generated through surface treatments such as shot peening (SP), deep cold rolling (DCR), and vibro-peening (VP) on fatigue crack mechanisms of Ni-based superalloy is investigated. The fatigue performance with associated failure mechanisms is measured under strain-controlled fatigue testing upto 104 cycles with total strain in the range of 0.9%–1.4% at an R ratio of 0.1 and 400°C followed by load controlled fatigue until failure. In-depth understanding of the failure mechanism is obtained through fractography analysis, cyclic stress–strain plot, and microstructural features. A pronounced improvement in fatigue life tested at low strain range (0.9%–1.1%) is achieved after inducing RCS up to 400 μm depth. However, the fatigue life is reduced when RCS increased to 800–1000 μm depth. Failure is primarily driven by micro-cracks formed due to balancing tensile stresses and high intensity stress concentration generated as the result of dislocation pile-ups and slip bands. Results are discussed in detail through the evidence of grain refinement, addition of low angle grain boundaries (LAGBs), strain accumulation, and intragranular deformation in the sub-surface. Nanyang Technological University Authors thank Nanyang Technological University (NTU), Singapore, and Advanced Remanufacturing and KUMARET AL.1599 Technology Centre (ARTC), Singapore, for providing research funding support to this project, and Rolls-Royce Singapore for materials support. D. Kumar thanks NTU for the financial support in the form of NTU Research Scholarship. 2022-06-28T01:02:30Z 2022-06-28T01:02:30Z 2021 Journal Article Kumar, D., Idapalapati, S. & Wang, W. (2021). Influence of residual stress distribution and microstructural characteristics on fatigue failure mechanism in Ni-based Superalloy. Fatigue and Fracture of Engineering Materials and Structures, 44(6), 1583-1601. https://dx.doi.org/10.1111/ffe.13454 8756-758X https://hdl.handle.net/10356/159574 10.1111/ffe.13454 2-s2.0-85103163507 6 44 1583 1601 en Fatigue and Fracture of Engineering Materials and Structures © 2021 John Wiley & Sons, Ltd. All rights reserved. |
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Engineering::Mechanical engineering Deep Cold Rolling Electron-Back Scattered Diffraction Kumar, Dharmesh Idapalapati, Sridhar Wang, Wei Influence of residual stress distribution and microstructural characteristics on fatigue failure mechanism in Ni-based Superalloy |
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The influence of residual compressive stress (RCS) depth and magnitude generated through surface treatments such as shot peening (SP), deep cold rolling (DCR), and vibro-peening (VP) on fatigue crack mechanisms of Ni-based superalloy is investigated. The fatigue performance with associated failure mechanisms is measured under strain-controlled fatigue testing upto 104 cycles with total strain in the range of 0.9%–1.4% at an R ratio of 0.1 and 400°C followed by load controlled fatigue until failure. In-depth understanding of the failure mechanism is obtained through fractography analysis, cyclic stress–strain plot, and microstructural features. A pronounced improvement in fatigue life tested at low strain range (0.9%–1.1%) is achieved after inducing RCS up to 400 μm depth. However, the fatigue life is reduced when RCS increased to 800–1000 μm depth. Failure is primarily driven by micro-cracks formed due to balancing tensile stresses and high intensity stress concentration generated as the result of dislocation pile-ups and slip bands. Results are discussed in detail through the evidence of grain refinement, addition of low angle grain boundaries (LAGBs), strain accumulation, and intragranular deformation in the sub-surface. |
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School of Mechanical and Aerospace Engineering |
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School of Mechanical and Aerospace Engineering Kumar, Dharmesh Idapalapati, Sridhar Wang, Wei |
format |
Article |
author |
Kumar, Dharmesh Idapalapati, Sridhar Wang, Wei |
author_sort |
Kumar, Dharmesh |
title |
Influence of residual stress distribution and microstructural characteristics on fatigue failure mechanism in Ni-based Superalloy |
title_short |
Influence of residual stress distribution and microstructural characteristics on fatigue failure mechanism in Ni-based Superalloy |
title_full |
Influence of residual stress distribution and microstructural characteristics on fatigue failure mechanism in Ni-based Superalloy |
title_fullStr |
Influence of residual stress distribution and microstructural characteristics on fatigue failure mechanism in Ni-based Superalloy |
title_full_unstemmed |
Influence of residual stress distribution and microstructural characteristics on fatigue failure mechanism in Ni-based Superalloy |
title_sort |
influence of residual stress distribution and microstructural characteristics on fatigue failure mechanism in ni-based superalloy |
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2022 |
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https://hdl.handle.net/10356/159574 |
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1738844841320644608 |