• 대한기계학회논문집A
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• 제36권7호
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• pp.759-768
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• 2012

본 논문은 이차하중을 받는 고온 구조물의 $C(t)$-적분 예측을 위한 탄성추종 계수를 결정하는 기법을 제시한다. 이차하중을 받는 구조물의 과도 크리프 상태의 크리프 균열 진전률은 $C(t)$를 이용하여 정량화할 수 있다. 이차하중을 받는 구조물에서 발생할 수 있는 탄성추종 현상은 응력 완화를 방해하므로, 탄성추종 현상이 증가하면 $C(t)$와 크리프 균열 진전률이 증가한다. Ainsworth 와 Dean 은 참조응력법에 기반하여 $C(t)$ 예측식을 제시하였는데, 이 식을 계산하기 위해서는 탄성추종 계수가 필요하다. 본 연구에서 고온 균열 구조물의 크리프에 의한 탄성추종 계수를 결정하는 방법을 제시하였다. 소성-크리프 유사성을 이용하여 탄소성 유한요소해석으로 크리프 탄성추종 계수를 결정할 수 있다. 유한요소해석을 이용하여 이 탄성추종 계수 결정법을 검증하였다.

• 한국강구조학회 논문집
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• 제12권2호통권45호
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• pp.111-122
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• 2000

이 연구에서는 덮개판 형상이 피로특성에 미치는 영향을 정량적으로 평가하기 위해서 강교량을 구성하는 구조세목 중 덮개판 필렛용접부를 대상으로 일련의 피로실험을 실시하였다. 피로실험결과 덮개판 형상에 따라 피로강도에 다소 차이를 나타내고 있었으나 국내 및 외국의 피로설계기준을 만족함을 알 수 있었다. 또한 비치마크실험결과로부터 피로균열 발생점은 용접지단부의 형상에 밀접하게 관련되어 있음을 확인할 수 있었으며, 용접지단부의 여러 곳에서 동시다발적으로 발생한 피로균열이 반타원형의 표면균열의 형태로 성장하고 이 균열이 서로 합체되어 관통균열의 형태로 성장함으로써 결국 파단에 이르렀다. 한편, 파괴역학적 해석결과로부터 기존의 제안식 및 유한요소해석에서 구한 균열보정 계수 중기하학적형상보정계수가 가장 지배적임을 알 수 있었으며, 피로균열성장속도와 유한요소해석에서 구한 응력확대계수범위 사이의 관계로부터 덮개판 필렛용접부의 피로수명을 산정 할 수 있었다.

• 한국강구조학회 논문집
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• 제11권4호통권41호
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• pp.339-350
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• 1999

이 연구에서는 강교량 주부재의 연결에 주로 사용되는 횡방향 맞대기 용접부를 대상으로 입체결함의 일종인 블로우홀을 인위적으로 도입하고 블로우홀의 크기 및 형상에 따른 피로특성을 정량적으로 평가하기 위해서 일련의 실험을 실시하였다. 정적실험결과 블로우홀을 가진 횡방향 맞대기 용접부의 정적강도는 블로우홀의 크기 및 형상에 관계없이 일정한 경향을 나타내었다. 피로실험결과 블로우홀을 가진 횡방향 맞대기 용접부의 피로강도는 용접루트부 내부에 존재하는 블로우홀의 기하학적 형상이나 결함률에 크게 영향을 받으므로 이로부터 결함률과 피로강도 사이의 상관관계를 정량적으로 규명하였다. 또한 피로균열성장속도와 응력확대계수범위 사이의 관계로부터 블로우홀을 가진 횡방향 맞대기 용접부의 피로수명을 정확하게 산정할 수 있었다.

• 한국분말재료학회지
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• 제4권1호
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• pp.9-17
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• 1997

The mullite-zirconia composites were prepared by the pressureless sintering with addition of 10~20 vol% ZrO$_2$(TZ3Y) in the fused mullite and sol-gel mullite matrix. The densification rate of sol-gel mullite was higher than that of fused mullite, and the addition of ZrO$_2$(TZ3Y) was effective on the densification of fused mullite. The enhancement of densification and anisotropic growth of mullite in ZrO$_2$added specimen can be explained by the solid solution effect of $Zr^{+4}$ ion in mullite. Both mechanical strength and fracture toughness of mullite-zirconia composite were enhanced compared to those of mullite. The enhancement of mechanical properties is attributed to the hinderance of grain growth and the combined toughening effects of tetra-mono phase transformation and crack deflection due to the residual stress between mullite/ZrO$_2$.

• 한국표면공학회지
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• 제13권2호
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• pp.81-86
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• 1980

The mechanical properties of aluminized steel were investigated after the JIS SB 41 plates were dipped in molten aluminum bath. (1) The growth rate of iron-aluminum alloy layer was fast in early stage of alumizing, and then gradually decreased with increasing time. However, over the time period above 10 minutes the growth of alloy layer did not occur. (2) The constituent of alloy layer formed on the steel surface was identified to be intermetallic compound of $Fe_2\;Al_5$. (3) The ultimate tensile strength and elongation of aluminized steel showed a nearly constant value over all thickness below about 0.15 mm. However, both properties decreased rapidly in showed a nearly constant value over all thickness above about 0.20 mm. (4) In case of aluminized steel with greater thickness, crack was formed below yield point of base metal, which is considered to be attributed to the alloy layer failure.

• 한국표면공학회지
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• 제16권4호
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• pp.153-159
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• 1983

The growth rate equation of Fe-Zn alloy layer was represented by x = Kt, and hence the growth of alloy layer was considered to be controlled by diffusion process. The constituent of alloy layer formed on the steel surface was identified to be intermetallic compound of Fe3Zn10 and FeZn10. The ultimate tensile strength and elongation of galvanized steel showed a nearly constant value at the thickness below about 30$\mu\textrm{m}$, and both properties decreased with increasing thickness above about 30$\mu\textrm{m}$. In the case of galvanied steel with a great thickness of alloy layer, crack was formed below yield point of base metal, which is considered to be attributed to the alloy layer failure.

• 대한조선학회논문집
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• 제60권4호
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• pp.213-221
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• 2023

The demand for Liquefied Natural Gas (LNG) carriers and LNG-fueled ships has significantly increased in recent years due to the sulfur-oxide emission regulations by the International Maritime Organization (IMO). The main goal of this paper is to introduce the process for the Engineering Critical Assessment (ECA) of IMO independent type-B cargo tanks made from 9% nickel alloy. A methodology proposed by the British Standard was used to conduct ECA for any structure with initial flaws. Based on this standard, a Matlab code was developed to perform ECA. Coarse mesh Finite Element Analysis (FEA) was performed on an independent type-B LNG cargo tank with a capacity of 15,000 m³. The location with the highest development of maximum principal stress was identified at the bottom of the cargo tank. Fine mesh FEA was performed to obtain the stress range required for ECA. The dynamic cargo tank loads used for FEA were determined using some ship rules presented by Det Norske Veritas. As a result of performing a 20-year long-term crack propagation analysis with a semi-elliptical surface crack, the fracture-to-yield ratio exceeded the Fracture Assessment Line (FAL) and some structural reinforcement was necessary. Performing a 15-day short-term crack propagation analysis, the fracture-to-yield ratio remained within the FAL, and no significant LNG leaks were expected. This paper is believed to provide a guide for performing ECA of LNG cargo tanks in the future by providing the basic theory and application sample necessary to perform ECA.

• International Journal of Railway
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• 제2권2호
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• pp.43-49
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• 2009

Wear and rolling contact fatigue (RCF) defects are most important causes of rail damage, and often interaction competitive at present railway track. Head check is one of rolling contact fatigue (RCF) defects, and generally occurs in mild circular curves and transition curves that are set at both ends of sharp circular curves. Wear tends to limit the crack growth of head checks by removing the material from the RCF surface. In order to clarify the conditions of the occurrence and growth of head checks, the authors measured the interacting forces between wheels and rails and the angle of attack of wheelset, and carried out contact analyses using the actual profile data of wheels and rails. The effects of the lateral force, the contact geometry, and the wear rate at rail gauge comer on the formation of head checks were also analyzed by using the worn profiles of actual wheels and rails and the data obtained by a track inspection car. Some specific range of wear rate at the gauge comer was identified as having close relation with occurrence of head checks.

• Composites Research
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• 제13권3호
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• pp.38-47
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• 2000

기재위에 입혀진 코팅에서 발생하는 크랙킹 현상을 파괴역학을 이용해서 분석하였다. 코팅/기재 구조에서 굽힘모드시 발생하는 코팅크랙킹을 변분법을 이용하여 분석하였으며, 본 연구에서 유도된 변위에너지 방출량을 통해 기재위에 입혀진 코팅층에서 크랙이 확장되는 것을 예측할 수 있다. 본 연구를 통해 얻어진 코팅의 임계 변위에너지 방출량은 재료의 고유성질이며 코팅크랙킹의 보다 근본적인 의미를 제공할 수 있다.

• Steel and Composite Structures
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• 제35권3호
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• pp.439-447
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• 2020

This paper presents two sets of full three-dimensional thermoelastic finite element analyses of superimposed thermo-mechanically loaded Spar Wingskin Joints made with laminated Graphite Fiber Reinforced Plastic composites. The study emphasizes the influence of residual thermal stresses and material anisotropy on the inter-laminar delamination behavior of the joint structure. The delamination has been pre-embedded at the most likely location, i.e., in resin layer between the top and next ply of the fiber reinforced plastic laminated wingskin and near the spar overlap end. Multi-Point Constraint finite elements have been made use of at the vicinity of the delamination fronts. This helps in simulating the growth of the embedded delamination at both ends. The inter-laminar thermoelastic peel and shear stresses responsible for causing delamination damage due to a combined thermal and a static loading have been evaluated. Strain energy release rate components corresponding to the Mode I (opening), Mode II (sliding) and Mode III (tearing) of delamination are determined using the principle of Virtual Crack Closure Technique. These are seen to be different and non-self-similar at the two fronts of the embedded delamination. Residual stresses developed due to the thermoelastic anisotropy of the laminae are found to strongly influence the delamination onset and propagation characteristics, which have been reflected by the asymmetries in the nature of energy release rate plots and their significant variation along the delamination front.