• 한국자동차공학회논문집
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• 제13권6호
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• pp.63-69
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• 2005

For the case that center crack is surrounded by four small cracks which are symmetrically distributed around center crack, the same values of normalized stress intensity factor of center crack according to the position of the tip of small cracks are located on the smooth curve. And the stress intensity factor according to any position of small cracks can be sufficiently obtained from this curve. The plastic zones between distributed cracks are also investigated by changing the positions of nearly small cracks. The occurrence of plastic zone due to the interaction between center crack and small cracks are analyzed by finite element method. The mechanical behavior at the vicinity of crack tips is investigated by plastic areas. The changes of plastic zones according to positions of distributed cracks are drawn schematically. The safety of materials is also analyzed.

• 한국자동차공학회논문집
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• 제11권2호
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• pp.172-181
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• 2003

In this study, the stress intensity factor of center crack tip is calculated by the superposition method when it is surrounded by symmetrically distributed small cracks. The values of stress intensity factors of center crack tips are compared with those of the center crack tips calculated by the superposition method. These compared errors are influenced by the locations of distributed small cracks. These errors are inspected. When small cracks overlap and approach near the center crack tip, the effect of interaction caused by these cracks becomes noticeable and these errors become larger. In case of multiple distributed small cracks except this case, the stress intensity factor of the center crack tip is easily calculated by the superposition method.

• 한국정밀공학회지
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• 제15권11호
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• pp.244-250
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• 1998

In this study, the stress intensity factors of center crack are analyzed when it is surrounded by symmetrically distributed small cracks. The values of stress intensity factors of the center crack are greatly influenced by the locations of distributed small cracks. When small cracks overlap or approach near the tip of a center crack, the effect of interaction arisen by these cracks becomes noticeable. In case of multiple distributed small cracks, the stress intensity factor of a center crack is found to be efficiently determined by the superposition method.

• 대한기계학회논문집
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• 제17권12호
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• pp.3105-3114
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• 1993

previously, several basic studies in the experimental analysis of stress intensity factors of cracks by slab analogy have been presented by authors. But, for the application of above mentioned method to the analysis of the arbitrarily distributed cracks, there still is several bottlenecks to be overcome in terms of its experimental process and data treatment. Moreover, authors recently proposed an improved experimental method to use the fixed slab analogy device which has promised more accurate measurement of S.I.F. of small cracks. In this paper, for the completion of slab analogy analysis of distributed cracks, a grating imaginary rotation method is introduced. And, to prove its validity, this combined method is applied to the determination of stress intensity factors of theoretically known distributed cracks. The results show good agreement with the existing theoretical solutions and physical crack propagation tendencies.

• Journal of Advanced Marine Engineering and Technology
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• 제26권1호
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• pp.76-82
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• 2002

In this study, the rotary bending fatigue test was carried out with low carbon steel(SM25C). The specimens were heat-treated in order to change the grain size, and investigated items are fatigue limit, small crack initiation, fatigue crack propagation behavior and possibility of fatigue life prediction according to the different grain size. The summarized result are as follows ; Fatigue limit of the smooth specimen was dependent upon the grain size. The fatigue crack initiation of the small grain size specimen was delayed more than that of the large grain size specimen. And the small cracks of small grain size specimen were distributed in the narrow region of the main crack circumference contrary to the large grain size specimen. The main crack was grown along the grain boundary having co-alliance with small cracks. The experiment material has quantitatively disclosed the possibility of fatigue life prediction because the fatigue crack propagation behavior is dependent upon the grain size.

• 소성∙가공
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• 제28권3호
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• pp.154-158
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• 2019

The hole expansion tests using conical punch, flat punch or hemispherical punch are widely used for stretch flangeability verification of HSS. In this study, we investigate the strain distribution on the shear edges of the hole expansion test using grid marking and a projector. A small crack at the edge is distributed, resulting in a large gap between the HER and the crack strain. The strain distribution at the edges is irregular due to anisotropy of sheet metal. While an edge perpendicular to the rolling direction indicate a lower strain level compared to an edge parallel to the rolling direction, edge cracks occur at the edge perpendicular to the rolling direction. To predict the manifestation of edge cracks in FE analysis, the result of the hole expansion test with a crack strain measurement may well be a better tool than FLD. In this case, the level of strain and the direction of the edge relative to the rolling direction should be well considered.

• 대한기계학회논문집
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• 제16권1호
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• pp.53-62
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• 1992

본 연구에서는 약 10년 정도 사용하여 경년 열화가 되었다고 예상되는 실구조 물의 일부를 입수하였으며 열화재의 특성과 비교하기 위하여 열처리에 의해 충격치를 회복시킨 재료를 회복재로 하여 두가지 재료에 대해 시험편을 제작하였따.열확현상 을 파악하기 위하여 평활재로 피로과정, 즉 미소 균열의 발생, 진전 및 복수 균열이 간섭합체하여 파단에 달하는 과정에 대하여 파괴역학적 견지에서 열화재와 회복재를 해석하고 이결과로 부터 확율변수를 추정하여 통계학적인 수명예측방법의 하나를 제시 하여 실구조물에 적용하는 방법에 대해 시도해 보았다.

• 대한기계학회논문집A
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• 제40권7호
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• pp.637-646
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• 2016

실온에서 인코넬 718의 UNSM(Ultrasonic nanocrystal surface modification)처리재, 수소취화재(100 bar, $300^{\circ}C$에서 120 h) 및 수소취화재의 UNSM처리재의 회전굽힘피로시험에 의해 얻어진 결과, 수소취화재는 미처리재의 S-N곡선보다 피로수명이 약 10~20 % 감소하며 부식피로나 비철재료처럼 피로한도 없이 점진적으로 감소하였다. 표면균열수는 수소취화의 영향으로 평균입경($13{\mu}m$)보다 작은 균열의 비율이 약 80 %를 차지하였다. 결정입계, 표면 흠 등에 수소침투에 의한 취화현상으로 티어링(tearing)하면서 복수로 발생한 작은 표면균열은 불규칙적으로 분포하며 티어링하면서 성장, 합체되어 피로수명이 감소하는 것으로 추정된다. 미처리재에 비해서 UNSM처리재의 피로수명은 전 영역에서 크게 증가하였고, 수소취화된 시험편을 UNSM 처리한 후 피로시험을 실시하면 700 MPa에서 10배 이상, 600 MPa에서 20배 이상 증가하였다.

• 한국지역지리학회지
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• 제14권2호
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• pp.173-188
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• 2008

본 보고서는 도시개발에 따른 지형변화를 비교 분석하기 위하여, 팔공산지 등단의 산록에 위치한 대구 혁신도시 개발예정지의 지형자원의 분포를 조사한 것이다. 조사 결과를 요약하면 다음과 같다. 첫째, 배후산지의 소규모 하곡 전면에는 소규모 선상지들이 분포하며, 하곡 측면에는 배후의 산지로부터 이어지는 구릉지가 분포한다. 둘째, 소규모 하곡이 구릉지를 측방침식 한 경우에는 수직의 하식애와 평탄한 기반암 하상이 잘 드러나며, 셰일 하상에는 건열과 연흔 화석이 나타나기도 한다. 일부 하곡에서는 절리를 따라 암괴가 제거되어 감입곡류가 형성되는 과정을 보여주기도 한다. 셋째, 신서지구의 선상지는 약 7m의 층후를 보인다. 선상지를 관류하는 신서천 하곡 내에는 2m 내외의 하안단구가 형성되어 있다. 이 하안단구는 후빙기 선상지가 개석되는 과정에서 형성된 것으로, 하안단구 형성과정의 새로운 가능성을 제시해 준다.

• Structural Engineering and Mechanics
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• 제5권5호
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• pp.507-521
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• 1997

The ultimate behavior of a reinforced concrete hyperbolic paraboloid saddle shell under uniformly distributed vertical load is investigated using an inelastic, large displacement finite-element program originally developed at North Carolina State University. Unlike with the author's previous study which shows that the saddle shell possesses a tremendous capacity to redistribute the stresses, introducing tension stiffening in the model the cracks developed are no longer through cracks and formed as primarily bending cracks. Even though with small tension stiffening effect, the behavior of the shell is changed markedly from the one without tension stiffening effect. The load-deflection curves are straight and the slope of the curves is quite steep and remains unchanged with varying the tension stiffening parameters. The failure of the shell took place quite suddenly in a cantilever mode initiated by a formation of yield lines in a direction parallel to the support-to-support diagonal. The higher the tension stiffening parameters the higher is the ultimate load. The present study shows that the ultimate behavior of the shell primarily depends on the concrete tensile characteristics, such as tensile strength (before cracking) and the effective tension stiffening (after cracking). As the concrete characteristics would vary over the life of the shell, a degree of uncertainty is involved in deciding a specified ultimate strength of the saddle shell studied. By the present study, however, the overload factors based on ACI 318-95 are larger than unity for all the cases studied except that the tension stiffening parameter is weak by 3 with and without the large displacement effect, which shows that the Lin-Scordelis saddle shell studied here is at least safe.