• Transactions of the Korean Society of Mechanical Engineers A
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• v.36 no.12
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• pp.1521-1528
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• 2012

The present paper provides the elastic stress intensity factors (SIFs) and the crack opening displacements (CODs) of a thick-walled pipe with a slanted axial through-wall crack. For estimating these elastic fracture mechanics parameters, systematic three-dimensional elastic finite element (FE) analyses were performed by considering geometric variables, i.e., thickness of pipe, reference crack length, and crack length ratio, affecting the SIFs and CODs. As for loading condition, the internal pressure was considered. Based on the FE results, the SIFs and CODs of slanted axial through-wall cracks in a thickwalled pipe along the crack front and the wall thickness were calculated. In particular, to calculate the SIFs of a thick-walled pipe with a slanted axial through-wall crack from those of a thick-walled pipe with an idealized axial through-wall crack, a slant correction factor representing the effect of the slant crack on the SIFs was proposed.

• Journal of the Korean Society of Fisheries and Ocean Technology
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• v.36 no.2
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• pp.147-154
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• 2000

실온 대기 중에서 탄소강배관(STS370)의 피로시험을 행하였다. 배관에는 외부결함을 인공적으로 상정하여, 피로균열진전 및 관통의 거동, 균열형상, 누설 및 파단수명, 균열개구변위를 실험과 이론의 양면으로부터 비교·검토하였다. 특히, 배관의 벽두께 관통후에 있어서의 응력확대계수를 평가하기 위하여 새로운 식을 제안하였다. 피로균열이 관벽을 관통하기 전에 있어서는 판모델에 의한 Newman-Raju의 응력확대계수 평가식을 이용하므로서 aspect비와 누설수명 등 관통전의 피로균열성장거동을 평가할 수 있음을 나타내었다. 또한, 피로균열이 관벽을 관통한 후에 있어서는 본 논문에서 제안한 배관모델에 의한 응력확대계수의 평가식을 이용하여 관통후의 균열형상, 파단수명 및 균열개구변위 등 관통후의 피로균열성장거동을 평가하였다.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.02a
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• pp.132-132
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• 2010

3-5족 화합물 반도체는 직접천이형 반도체이며, 여러가지 우수한 특성으로 인하여 고효율의 태양전지물질로 각광을 받고 있다. 또한 3중접합 구조를 이용한 집광형태양전지의 경우, 40% 이상의 높은 효율을 보인다고 보고 되고 있다. 이러한 고효율 태양전지를 실리콘 기판위에 성장할 경우, 대면적에서의 태양전지제작이 가능해지며, 단가절감이 가능할 것이라고 예상된다. 하지만, 하부셀로 사용되는 게르마늄과 실리콘의 4.2%의 격자상수차이로 인하여, 고품질의 게르마늄 박막을 실리콘 기판위에 성장하는 데에 있어서 많은 문제점이 있으며, 이러한 문제점을 극복하기 위하여, 저온에서 성장한 게르마늄 박막을 완충층으로 사용하는 2단계 성장법이 제안되었다. 하지만, 2단계 성장법에서 저온 완충막의 성장조건이 게르마늄 박막에 미치는 영향은 명확하지 않다. 본 연구팀은 초고진공 화학기상증착법을 이용하여 순수 게르마늄 박막을 실리콘 기판 위에 성장하였으며, 저온 완충막의 두께를 20 nm에서 120 nm까지 변화시켜서, 완충막의 두께가 게르마늄박막에 미치는 영향에 대해서 연구해 보았다. 그 결과, 40 nm이하의 두께를 갖는 완충막을 사용할 경우, 박막 내부에 실리콘 게르마늄을 형성하면서, 거친 표면이 형성되었다. 반면에, 40 nm보다 두꺼운 완충막을 사용할 경우 평탄한 표면을 갖는 순수게르마늄박막이 형성되었다. 이를 통해서, 순수 게르마늄박막 성장을 위해서는 일정 두께 이상의 저온 완충막이 사용되어야함을 알 수 있었다. 또한 게르마늄박막의 관통 전위 밀도를 분석해 본 결과 완충막의 두께가 80 nm까지 두꺼워짐에 따라서 초기에는 관통전위밀도가 $1.2\;{\times}\;10^6\;cm^{-2}$ 까지 감소하는 경향을 보였으나, 완충막의 두께가 더욱 증가할 경우 관통전위밀도가 증가하였다. 이러한 결과를 바탕으로 저온 완충막의 두께를 조절함으로써 최적화된 게르마늄의 성장이 가능함을 확인할 수 있었다.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.31 no.4A
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• pp.311-321
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• 2011

To analysis the effect of reinforcement ratio and impact velocity on local damage, a series of impact analyses are performed to predict local effects. According to these results, the reinforcement ratio has no effect on the penetration depth and perforation thickness, but notable change to the scabbing area were observed. The higher the missile velocity becomes, the greater the degree of local damage to the reinforced concrete slabs is. Analysis results will be useful in the impact-resistance design of containment buildings and structures.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.3
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• pp.257-268
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• 2018

We have studied the damage mechanism of a metallic thin plate by the highly energetic fragments generated from high explosive(HE) warhead. The penetration process has presumed that the velocity of a fragment is in the range of 350 m/s to 3353 m/s, the thickness of Aluminum 2024 target plate is in the range of 1 mm~6.3 mm thick. The mass of fragment with hemisphere nose shape is in the range of 0.32 g to 16 g. The analytical solution for penetration process has been derived by using the report of the project THOR. The results of analysis implied that the closed forms by an exponentially decay function well fit the change of the ballistic limit velocity, loss velocity and loss mass of fragment as the mass of fragment and the thickness of target plate increase.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.30 no.6A
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• pp.543-560
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• 2010

Safety-related concrete structures in a nuclear power plant must be protected against the impact of flying objects, referred to in the profession as missiles. In practice, the structural verification is usually carried out by means of empirical formulas, which relate the velocity of the impinging missile to the wall thickness needed to prevent scabbing or perforation. The purpose of this study is to reevaluate the predictability of the local effect prediction formulas for the penetration and scabbing depths and perforation thickness. Therefore, available formulas for predicting the penetration depth, scabbing thickness, and perforation thickness of concrete structures impacted by solid missiles are summarized, reviewed, and compared. A series of impact analyses is performed to predict the local effects of the projectile at impact velocities varing from 95 to 215 m/s. The results obtained from the numerical simulations have been compared with tests that were carried out at Kojima to validate numerical modelling. The simulation results show reasonable agreement with the Kojima test results for the overall impact response of the RC slabs. From these results, it seems that the Degen equation give a very good estimate of perforation thickness against a tornado projectile for test data. Finally, the results obtained from the impact analysis have been compared with Degen formula to determine the perforation thickness of the RC slab.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 1992.10a
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• pp.311-315
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• 1992

일반적으로 기계구조물에서는 비교적 응력확대계수 K의 해석이 용이한 판 두께를 관통하는 관통크랙보다는 표면에 존재하는 결함에서 발생, 전파하는 표면 크랙이 대부분이다. 표면은 내부보다 소성변형에 대한 저항이 작고, 대기에 직접 접해 있으며, 평활재에 있어서의 인장, 압축이외의 응력은 일반적으로 표면에서 최대가 되는 등의 이유로 내부보다 쉽게 피로재해를 받는다. 침탄질화 열처리를 하는 중요한 목적이 재료 표면에 있어서 경화능과 피로강도의 향상이므로 침탄질화 처리재의 표면 크랙에 관한 연구가 절실히 요구됨은 당연하다.

• Journal of the Korean Institute of Gas
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• v.3 no.1
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• pp.1-7
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• 1999

Fatigue behavior of before-and-after penetration was examined experimentally using surface pre-cracked specimens of aluminium alloy 5083-0. The fatigue crack shape before penetration is almost semicircular, and the measured aspect ratio is larger than the value obtained by calculation using K values proposed by Newman-Raju. It is found that the crack growth behavior on the back side after penetration is unique and can be divided into three stages. By using a crack propagation rule in case of long surface crack, the change in crack shape after penetration can be evaluated quantitatively.

• Journal of the Korean Society for Nondestructive Testing
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• v.33 no.2
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• pp.138-146
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• 2013

The present paper provides the elastic stress intensity factors(SIFs) of thick-walled cylinder with non-idealized circumferential through-wall cracks. For estimating these elastic SIFs, the systematic three-dimensional(3D) elastic finite element(FE) analyses were performed. In order to consider practical shape of thick-walled cylinder and non-idealized circumferential through-wall crack, the values of thickness of cylinder, reference crack length and crack length ratio were systematically varied. As for loading conditions, axial tension, global bending and internal pressure were considered. In particular, in order to calculate the SIFs of thick-walled cylinder with non-idealized circumferential through-wall crack from those of thick-walled cylinder with idealized circumferential through-wall crack, the correction factor representing the effect of non-idealized crack on the SIFs were proposed in this paper. The present results can be applied to accurately evaluate the rupture probabilities of nuclear piping considering actual crack growth behaviors.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.32 no.6A
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• pp.411-418
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• 2012

In this study, behavior of unpatched and patched cylindrical shells with through-wall cracks has been estimated using numerical experiments, and patching effect of them has been investigated according to various patching parameters. To show credibility of numerical models considered, two ways such as h- and p-methods have been adopted. Also, domain integral method and virtual crack extension method have been considered to calculate energy release rates based on linear elastic fracture mechanics. For examples, the unpatched cylindrical shells with circumferential cracks under remote tension have firstly been analyzed to show the validity of finite element modeling with h-method or p-method, and then the results have been compared with literature values published. Next, the sensitive analysis of patch repaired problems in terms of thickness of patch and adhesive, shear modulus of adhesive, composite material type of patch, crack length, etc. has been carried out.