[First Topic: Evaluation of Small Cracks] The stress intensity factor (Κ) is essential for analyzing fracture and fatigue crack growth in metals and ceramics. While the threshold stress intensity factor (ΔΚRth) increases with crack length...

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https://www.riss.kr/link?id=T17545755
부산 : 국립부경대학교 대학원, 2026
학위논문(박사) -- 국립부경대학교 대학원 , 재료공학과 , 2026. 8
2026
한국어
부산
V, 136 ; 26 cm
지도교수: 남기우
I804:21031-200001029360
0
상세조회0
다운로드다국어 초록 (Multilingual Abstract)
[First Topic: Evaluation of Small Cracks] The stress intensity factor (Κ) is essential for analyzing fracture and fatigue crack growth in metals and ceramics. While the threshold stress intensity factor (ΔΚRth) increases with crack length...
[First Topic: Evaluation of Small Cracks]
The stress intensity factor (Κ) is essential for analyzing fracture and fatigue crack growth in metals and ceramics. While the threshold stress intensity factor (ΔΚRth) increases with crack length, it becomes constant beyond a certain length. This study utilized evaluation equations proposed by Tange et al. and Ando et al. to assess ΔΚRth(s) and the fatigue limit (Δσwc) for small cracks in F690 steel. Despite their different conceptual origins, the results from both equations were nearly identical, proving their utility in evaluating crack length dependence across all steel grades.
[Second Topic: Rendering Cracks Harmless via Needle Peening]
Semi-circular cracks (depth 0.4–1.6 mm) were machined into DNV F690 steel, followed by needle peening (NP) and four-point bending fatigue tests. The fatigue limits estimated by Ando’s equation aligned well with the experimental results. NP-induced compressive residual stress significantly enhanced the fatigue limit of both smooth and cracked specimens. Notably, cracks up to 0.8 mm in depth were rendered harmless, maintaining over 95% of the smooth specimen's fatigue limit. The maximum "harmless" crack depth for this NP treatment was estimated to be 1.14 mm.
[Third Topic: Reliability and Maintenance Strategies]
High-strength steels like F690 are susceptible to rapid microcrack growth, making it vital to render such cracks harmless for the safety of offshore structures. This study evaluated the maximum harmless crack depth (αhml) under various conditions of aspect ratio (As), ΔΚth, and residual stress. Key findings include: ① αhml increases as the compressive residual stress distribution becomes larger and deeper. ② Larger values of As and ΔΚth(l) also lead to an increased αhml. ③ With a safety factor (N) of 2.0, long-term reliability can be secured using needle peening. ④ Standard non-destructive inspection (NDI) may struggle to detect cracks that significantly reduce fatigue limits, necessitating more sensitive NDI techniques. ⑤ The study reviewed the relationship between αhml, detectable crack depth (σNDI), and critical crack depth (σcrN) to establish effective maintenance protocols.
목차 (Table of Contents)
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