• Transactions of the Korean Society of Mechanical Engineers
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• v.8 no.4
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• pp.289-297
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• 1984

본 연구에서는 이상과 같은 점을 고려하고 흠함이 존재하기 쉬운 용접부 표면 에 인공적으로 1/4원형에 해당하는 표면피로크랙을 시험편 모서리에 넣고 이러한 시험 편에 굽힘응력을 가하여 다음과 같은 사항들을 고찰하였다. 피로크랙의 표면 및 측 면에서의 전파과정, 피로크랙의 모양비(b/a)의 변화, 피로크랙의 표면 및 측면의 전파 속도와 크랙길이와의 관계등을 알아보았다. 여기에서 크랙의 표면길이란 흠함이 시 험편 모서리에 존재할 때 그것을 기점으로 표면에 전파하는 크랙의 길이를 말하며, 크 랙의 측면길이란 그것을 기점으로 측면의 표면에 전파하는 크랙의 길이를 말한다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.9 no.3
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• pp.301-308
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• 1985

본 논문에서는 불규칙 하중을 받는 부재에 대한 연구의 고초로서 간단한 응력 모델을 설정하고 이들 변동응력이 가해지는 시기를 명확히 구분하여 크랙전파곡선의 거동을 고찰하였다. 특히 부하되는 응력 진폭의 크기에 따라서 크랙선단부의 미시적 인 변화의 크기가 다르고 이로인하여 크랙전파에 대한 피해의 정도가 달라진다고 하면 크랙전파의 지연 및 가속현상이 나타날 것이 예측이 되고 따라서 이때 나타나는 피해 정도의 크기를 미소 경도치로 환산하여 그것과 피로크랙 전파 특성과를 비교 검토 하 였다.

• Journal of Welding and Joining
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• v.15 no.3
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• pp.1-11
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• 1997

용접이음부에서는 피로크랙 전파거동이 모재와 다르다는 것은 이미 알려져 있으며 그 원인으로서는 용접부에 있어서의 금속조직의 변화와 잔류응력 등이 일컬어 진다. 금속조직의 변화에 따른 영향에 대하여서는 비교적 그 영향이 작으며 또한 피로 크랙 전파속도에 대해서 안전한 쪽으로 역할을 한다고 보고되어져 있다. 따라서 용접 이음부에 있어서의 피로크랙 전파에 대하여서는 주로 잔류 응력의 영향에 주목하여, 잔류응력이 피로크랙의 전파속도에 어떻게 영향을 미치는가를 파악하여야 한다. 이러 한 관점에서 지금까지 용접잔류응력장을 전파하는 피로크랙을 대상으로 하여 잔류응력 이 피로크랙 전파에 미치는 영향을 정량적으로 평가하고자 하느 시도가 많은 연구진에 의해 수행되어 왔다. 표1에 이러한 연구의 흐름을 평가방법과 평가에 고려된 사항을 중심으로 나타내었다. 이러한 배경으로부터, 본고에서는 피로크랙 전파거동에 미치는 잔류응력의 영향에 대해서 지금까지 수행된 연구의 내용을 연구 발전형태에 주목하여 검토하였다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.10 no.2
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• pp.188-197
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• 1986

With respect to structural carbon steel(SM 22C), it was studied how the overstress or the understress has effects on fatigue inside crack propagation curve of a two level stress. Obtained results are summarized as follows. (1) The overstress or the understress, at a slip band occurrence stage, does not change the inside crack propagation curve because the crack closure and opening phenomena do not happen. (2) The overstress, at a crack propagation stage, does not change the inside crack propagation curve because the crack closure of overstress in compressive state is nearly same that of base stress in compressive state. (3) The understress, at a crack propagation stage, give rise to an acceleration of crack growth because the crack closure of understree in compressive state is more open than that of base stress in compressive state and the phenomenon is the essential increase of the actual applied stress of the specimen.

• Transactions of the Korean Society of Mechanical Engineers
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• v.13 no.1
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• pp.115-124
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• 1989

Near-threshold fatigue crack-growth behavior at room temperature for a duplex stainless steel weldments was investigated to evaluate the effect of load ratio, microstructural change, and residual stresses. Near-threshold fatigue crack propagation behavior is found to show a marked sensitivity to .alpha./.gamma. phase ratio, and little residual stress effects. Threshold values in the heat affected zones are higher than those of base metals and threshold values for crack growth decrease with increasing the load ratio in the base metals and weldments. The fractrographic features in base metals, weldments and heat affectred zones were discussed in terms mechanism of crack growth.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.6 no.6
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• pp.531-535
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• 2005

This study investigates the behavior of fatigue crack propagating between holes or holes lilted with another materials. It is experimentally and analytically confirmed that the center crack stops when its tip reaches near the center line of the holes and a small crack is initiated from the boundaries of holes or the holes filled with another materials and it propagates to final fracture. The mechanical behaviors of center crack near the another materials are also investigated. The phenomenon that this crack propagates to fracture is investigated by compliance method.

• Transactions of the Korean Society of Mechanical Engineers
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• v.15 no.3
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• pp.880-886
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• 1991

본 연구에서는 이미 크랙전파의 제단계에 있는 평골재의 정유 크랙을 대상으 로, COD를 고정밀도로 측정하는 것을 주된 수단으로하여, 피로한도의 존재유무를 지배 하는 미소크랙의 정유구조를 상세히 밝히고자 한다. 또한 변형시교에 근거한 현상으 로만 알려져온 과소응력효과, coaxing효과를 크랙폐구현상의 관점에서 검토하여, 크랙 정유현상의 본질적인 이해를 얻고자 한다.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 1994.10a
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• pp.820-825
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• 1994

It is improtant to examine life or crack propagation behavior of structures because of its safety evaluation. The purpose of this study is to investigate the effect of crack-crack interaction to evaluate fatigue life and crack behavior. In this study, the behavior of the interaction of two cracks is studied by experiment. The vertical distance of two cracks is varied to make different interaction stress field. In addition, the effect of plastic zone is considered to examine crack propagation path and propagation rate.

• Transactions of the Korean Society of Mechanical Engineers
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• v.9 no.4
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• pp.421-429
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• 1985

This study has been made to investigate into the relation between fatigue crack behavior and ferrite grain size. As experimental observation of the low-carbon steel specimen with the drilled micro-hole under rotating bending stress was made to accomplish this investigation. Obtained results are as follows; (1) The fatigue limit of micro-hole depends upon the magnitude of ferrite grain size, as indicated by the Hall-Petch formula. (2) The fatigue crack occurring around the micro-hole is of shear type, and the frequency of fatigue crack initiation depends upon the ferrite grain size. (3) The magnitude of ferrite grain size affects the behavior of fatigue crack propagation up to the crack size of 0.3mm. The effect, however, is negligible for the crack size larger than 0.3mm.

• Transactions of the Korean Society of Mechanical Engineers
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• v.16 no.7
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• pp.1373-1380
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• 1992

The local cyclic strain distribution near the crack tip has been investigated by the fine Dot Grid Strain Measurement Method, which had been suggested strain measurement method to resolve experimental difficulties by authors. It has been found that the magnitude of the local cyclic strain distribution(.DELTA..epsilon.$_{eq}$ )near a crack tip has been varied by the applied cyclic load level and material, but the shape of the local cyclic strain distribution near the crack tip has been experimentally scrarcely altered : that is .DELTA..epsilon.$_{eq}$ = .DELTA.A.f(.theta.). $r^{-1}$ . Consequently, the local cyclic strain field near the crack tip could be favorably characterized by a single parameter fatigue strain intensity factor .DELTA.A. In addition, with the viewpoint that .DELTA.A depends on material and load level, .DELTA.A has been applied to evaluate the fatigue crack propagation rate and usefulness of the result has been considered. As a result, it has been ascertained that .DELTA.A has been a useful parameter to evaluate the fatigue crack propagation rate.