• Elastomers and Composites
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• 제34권4호
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• pp.341-349
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• 1999

본 연구에서는 산화방지제의 종류에 따라 천연고무 가황물이 어떠한 내열성과 내크랙성을 가지는지를 평가해 보았다. 가교시스템에 의한 영향을 방지하기 위해 촉진제/황 비율을 0.25로 고정하여 실험을 실시하였다. 페닐렌디아민계 산화방지제는 가교에 참여하여 가교밀도를 증가시킴으로 가황물의 인장강도를 향상시키는 것으로 나타났고, 분산성의 차이에 의해 인열강도는 산화방지제에 따라 거의 2배의 차이가 있음을 보였다. 인열에너지는 인열강도와 유사한 경향을 보였는데 불규칙한 크랙경로를 나타낸 페닐렌디아민계 산화방지제가 첨가된 가황물이 가장 우수하였다. Pure shear test에서도 페닐렌디아민계 신화방지제가 첨가된 가황물이 낮은 크랙 성장 속도와 높은 탄성율에 따른 높은 변형에너지 완화율을 가진 것으로 나타났다. 고무배합물 속에서 뛰어난 분산성과 높은 가교밀도를 보인 페닐렌디아민계 산화방지제가 첨가된 가황물이 우수한 내열성과 내크랙성을 가짐을 알 수 있었다.

• Journal of the Korean Wood Science and Technology
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• 제24권4호
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• pp.64-73
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• 1996

고인성 종이의 탄성-소성 파괴를 파괴역학을 이용하여 분석하였다. 탄성-소성 물질의 파괴에 있어서 균열이 언제 진행되기 시작하는지 이론적 판단 기준을 유도하고, mode I 파괴를 linear image strain analysis(LISA)로 관찰한 후, 파괴역학 변수들을 계산하였다. 크랙(crack)이 있는 물질에 외부하중이 작용할 때 변형율 에너지 발산 속도(strain energy release rate)가 그 물질이 견딜 수 있는 파괴저항(fracture resistance)에 도달하면 안정적인 파괴가 진행된다. 이를 이용하여 크랙의 초기 진행시 결점주위의 응력, 파괴저항, 크랙 진행거리, 기하인자(geometry factor) 등을 구하였다. 이 변수들은 종이의 파괴역학적 특성을 정량적으로 나타내므로 유용하게 활용될 수 있을 것이다.

• 한국융합학회논문지
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• 제5권1호
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• pp.23-27
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• 2014

본 연구에서는 소형 인장 시험편에 편심된 집중하중을 가하였을 때, 크랙 주변에서의 구멍의 존재유무, 개수 및 위치에 따른 전파 거동에 대하여 규명하였다. 시뮬레이션 해석을 통하여 시험편에서 발생하는 Strain energy와 변형량, 응력에 대해 알 수 있었다. 그리고 이들 Strain energy와 변형량을 바탕으로 응력확대계수를 구하였으며, 본 연구결과를 이용하면 구조물 내에 결함이나 구멍 등이 있을 때 그 파괴 가능성을 검증할 수 있다고 사료된다.

• 대한기계학회논문집
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• 제17권10호
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• pp.2391-2397
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• 1993

The distribution of fatigue crack growth rate is influenced by the measuring interval and methods of calculation of crack growth rate. The purpose of this paper is to suggest a method for the evaluation of crack growth rate distribution without the influence. The constant ${\Delta}P$ test and the constant .DELTA.K test are executed by using the CT specimen. The measuring interval of (${\Delta}a$/W=0.0067~0.014) crack length is not affected by methods of the calculation of the fatigue crack growth rate is suggested.

• 한국기계가공학회지
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• 제9권6호
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• pp.78-86
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• 2010

This paper aims to investigate the natural frequency of a cracked cantilever L-beams with a coupled bending and torsional vibrations. In addition, a theoretical method for detection of the crack position and size in a cantilever L-beams is presented based on natural frequencies. Based on the Euler-Bernoulli beam theory, the equation of motion is derived by using extended Hamilton's Principle. The dynamic transfer matrix method is used for calculation of a exact natural frequencies of L-beams. In order to detect the crack of L-beams, the effect of spring coefficients for bending moment and torsional force is included. In this study, the differences between the actual data and predicted positions and sizes of crack are less than 0.5% and 6.7% respectively.

• Journal of Advanced Marine Engineering and Technology
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• 제32권6호
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• pp.834-840
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• 2008

We carried out fatigue testing with materials of aluminum alloyC7075-T6, 2024-T4) by rotary bending fatigue tester. We investigated fatigue limit, fatigue crack initiation, fatigue crack propagation behavior and possibility of fatigue life prediction to the different small circular hole defect. The summarized result are as follows; Fatigue limit of the smooth specimens were related tensile strength and yield strength. In case of more large applied stress and small circular hole crack defect, the fatigue crack was grown rapidly. The fatigue crack propagation behavior proceed at according to inclusion. Fatigue crack propagation ratio appeared instability and retardation phenomenon in the first half of fatigue life but appeared stability and replied in the latter half. On other hand, this experimental data of the materials are appeared fatigue life predictability.

• 대한기계학회논문집
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• 제16권11호
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• pp.2072-2081
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• 1992

본 연구에서는 다매개변수(multiple parameters)사용시 모드 I과 모드 II에 나타나는 응력장의 특성을 분석하였고, 실험적으로 계산된 응력강도계수를 이론적인 수치해석 및 다른 실험결과에서 얻어진 값과 비교하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제30권6호
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• pp.724-730
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• 2006

Fracture behavior of brittle solids is closely related to microcracking. A meso-scale analysis method using the natural element method is proposed for the analysis of brittle microcracking solids. The microcracking is assumed to occur along Voronoi edges in the Voronoi diagram generated using the nodal points as the generators. The mechanical effect of microcracks is considered by controlling the material constants in the neighborhood of the microcracks. The meso-analysis method is applied to the simulation of the microcracking behaviors of brittle solids subjected to tensile macrostress. The method is also applied to the analysis of the propagation of a macrocrack accompanied by the coalescence with microcracks formed near the macrocrack-tip.

• Journal of Advanced Marine Engineering and Technology
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• 제19권2호
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• pp.36-46
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• 1995

In this paper, fatigue crack propagation behaviors were investigated experimentally for the materials, carbon steel forgings (SF45A, SF50A, SF60A) which are used in the marine propeller shaft. The results obtained are as follows: The number of cycles required to grow crack length 1.30mm from microcrack initiation was about 60% of the total fatigue life. Fatigue crack propagation rate was expressed by the equation d(2a)/dN_B 2a/$N_f$ and the result was agreed well with the experimented data. And the equation d(2a)/dN=$C{\sigma}_a^m(2a)^n$ was evaluated also. Obtained material property m and n are 3~5 and 1-1.5 respectably, and the result was reasonably agreed to the data obtained from experiments.

• 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.