• Korean Journal of Materials Research
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• v.8 no.4
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• pp.293-298
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• 1998

The fracture behavior of $Si_3N_4N$, coated $Si_3N_4N$-BN composite was studied by the Hertzian indentation technique. New types of contact-induced cracks were found, and it was confirmed that these cracks have cone crack geometry. Contact damage was distributed in the substrate layer, which can absorb energy, as well as in the coating layer, so the propagation of initiated cracks in the coating layer were suppressed.

• CORROSION AND PROTECTION
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• v.12 no.1
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• pp.1-11
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• 2013

Alloy 600 재료의 PWSCC의 개념을 소개하고 그 발생과 전파에 미치는 미세조직, 온도, 응력, 수화학 환경등의 주요인자를 정리하였다. ◯ PWSCC란 니켈 기지 합금인 Alloy 600와 그 용접재인 Alloy 82/182 재료가 원자로 1차수 환경에서 보이는 응력부식균열을 의미한다. ◯ Alloy 600의 PWSCC에 미치는 주요 인자에는 재료의 미세조직, 응력, 온도, 환경등이 있으며 그 중에서 재료의 미세조직이 가장 지배적인 인자이다. ◯ 재료내의 탄화물은 탄소 함량과 열처리 조건에 따라 달리 형성되며 입계를 따라 준연속적으로 잘 발달된 입계탄화물을 가지는 재료가 PWSCC에 저항성을 가진다. ◯ 손상속도는 부가 응력의 네 제곱에 비례하여 증가하는 것으로 알려져 있다. ◯ PWSCC는 Arrhenius 관계의 열활성화 과정(thermally activated process)이다. ◯ 용존수소량에 따라 재료의 부식전위가 정해지는데 전극전위가 Ni/NiO 평형전위 부근에서 가장 큰 균열 성장 민감도를 보인다는 데는 연구자들 사이에 이견이 없다. 그러나 균열의 개시에 대한 용존수소량의 영향에 대해서는 이견이 있다.

• Proceedings of the Korean Society for Rock Mechanics Conference
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• 2009.03a
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• pp.83-90
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• 2009

• Proceedings of the Korean Ceranic Society Conference
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• 2000.04a
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• pp.84.2-84.2
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• 2000

• Journal of the KSME
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• v.25 no.5
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• pp.419-424
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• 1985

동적탄소성 균열전파 문제는 매우 복잡한 문제이며 따라서 아직까지 이론적으로 명쾌한 해가 발표되지 못하고 있는 형편이다. 따라서 실험적인 연구는 아주 미비하며 다만 몇편의 논문만 발표되고 있는 편이다. 여기서는 Lee(47)의 실험적인 연구내용 및 연구결과를 간단히 강의하기로 한다.

• Proceedings of the KSEE Conference
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• 2008.10a
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• pp.57-60
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• 2008

• Proceedings of the Korean Ceranic Society Conference
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• 2003.10a
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• pp.225.1-225
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• 2003

• Journal of Industrial Technology
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• v.21 no.B
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• pp.341-348
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• 2001

The effect of initial ${\alpha}^{\prime}$ in STS 304 Stainless Steel on fatigue resistance, and fatigue crack propagation behavior was studied with using C-T specimens. Higher ${\Delta}K_{th}$ was observed in the specimens with the content of 0% initial ${\alpha}^{\prime}$ than in the contents of 2% and 33% initial ${\alpha}^{\prime}$. The difference of da/dN at the same level of ${\Delta}K$ was distinctive in low and intermediate level of ${\Delta}K$ however became less different as the level of ${\Delta}K$ increased. It is because the formation of strain induced martensite occurred readily in lower ${\alpha}^{\prime}$ at the vicinity of the fatigue crack tip, which causes compressive residual stresses resulting in the enhancement of crack closure. In general fatigue cracks propagated transgranular mode and many segments of ridges were observed on the fracture surfaces. At the higher contents of initial ${\alpha}^{\prime}$ appeared the smaller size of ridge segments. Slips in austenite were blocked more frequently by the martensite colonies formed in austenite.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.26 no.11
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• pp.2287-2296
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• 2002

Most cracks in the structure occur under mixed mode loading and those fatigue crack propagation behavior heavily depends on the stress ratio. So, it is necessary to study the fatigue behavior under mixed mode loading as the stress ratio changes. In this paper, the fatigue crack propagation behavior was respectively investigated at stress ratio 0.1, 0.3, 0.5, 0.7 and we changed the loading application angle into 0$^{\circ}$, 30$^{\circ}$, 60$^{\circ}$ to apply various loading mode. The mode I and II stress intensity factor of CTS specimen used in this study was calculated by the displacement extrapolation method using FEM (ABAQUS). Using both the experiment and FEM analysis, we have concluded the relationship between crack propagation rate and stress intensity factor range at each loading mode due to the variation of stress ratio. Also, when the crack propagated under given stress ratio and loading mode condition, we have concluded the dominant factors of the crack propagation rate at each case.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.25 no.1
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• pp.54-60
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• 2001

This study is to investigate the mechanical properties and the fatigue crack propagation of fire resistance steel for frame structure as the chemical composition was changed by addition of N, B and rolled end temperature was varied. We used two kinds of specimen, the one is parallel and the other is perpendicular to the rolling directions. As rolled end temperature increased, volume fraction of ferrite and pearlite decreased, but volume fraction of baintie and grain size increased. Micro-hardness decreased as rolled end temperature increased, but tensile and yield strength increased. Volume fraction of ferrite and pearlite decreased by addition of N. But volume fraction of bainite, tensile and yield strength increased. Microstructure was changed to martensite by addition of B, and tensile and yield strength increased. Fatigue life of TL direction specimen was shorter than that of LT direction specimen. There was no significant effect to fatigue crack propagation rate by addition of N and changing rolling condition, but fatigue life was increased by addition of B.