• Proceedings of the Korean Society of Precision Engineering Conference
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• 2000.11a
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• pp.417-420
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• 2000

The theoretical analyses for stresses induced in axial direction in the buried pipelines are reviewed. The influences of the axially directed stresses on the surface elliptical crack are studied in detail and thus some engineering technical informations are provided to use reliability assessment of buried pipelines. The change in temperature, the effect of inner pressure and soil friction in the buried pipeline constrained in axial direction are included to determine the axial stresses in the buried pipeline. Furthermore, the stress induced by the pipeline bending are also considered. The stress intensity factors calculated by two models such as a simple plane crack and an elliptical surface crack for a circumferential surface elliptical crack are compared.

• Journal of Ocean Engineering and Technology
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• v.9 no.1
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• pp.83-91
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• 1995

Surface defects in structural members are apt to be origins of fatigue cracks growth, which may cause serious failure of whole structures. Most structure has a part where stress concentrates such as welded joints, corner parts, etc. And then, analysis on crack growth and penetration from these defects, therefore, is one of the most important subjects for the reliability of LBB design. The present paper has performed an experimental and analysis on the fatigue crack propagation by variety in crack length of surface cracked plate with stress concentration part. The crack growth behavior can be explained quantitatively by using Newman-Raju equation and the stress partitioning method proposed by ASME B&P Code Sec. XI. The stress concentration factor $K_t$ has affected on the crack growth. The crack growth after penetration depends upon the initial front side crack length.

• Proceeding of EDISON Challenge
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• 2012.04a
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• pp.69-72
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• 2012

본 연구에서는 정사각형으로 모델링된 실린더 주위에 균일한 유동이 흐를 때 나타나는 이차원 난류 유동을 분석하였다. EDISON-CFD를 이용하여 정사각 실린더 표면에서의 전단응력 분포 및 유동 현상을 시뮬레이션 하였다. 선행 연구 결과의 $\bar{C_D}$, ${C_L}^{\prime}$ 값과 비교하여 결과의 유효성을 검증하였다. 또한, 비정상 층류 유동(Re=100)과 비교하여 난류 유동(Re=22,000)의 특성을 분석하였고, 와 흐름에 의하여 정사각 실린더 표면이 받는 전단응력을 자세히 분석하였다.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2014.11a
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• pp.211-211
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• 2014

스퍼터링에 의한 박막의 형성에서 박막의 박리나 기판의 휨은 박막내의 내부 응력과 깊은 관련이 있다. 특히 Ti/TiN구조로 많이 사용되는 TiN은 반도체 barrier 층으로 사용이 되기도 하며 하드 코팅 재료로도 많은 연구가 이루어지고 있다. 특히 TiN에 존재하는 높은 압축응력은 연성기판재나 무른 금속재질의 기판을 휘게도 하며, 심할 경우 박막의 박리 현상이 자주 관찰된다. 이렇게 높은 스트레스를 제어하기 위한 기초 연구로 다양한 금속층 박막의 스트레스와 완화시키기 위한 공정 조건 및 스트레스 특성을 확인하였다.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2012.05a
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• pp.299-300
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• 2012

본 연구는 고속 저응력 무전해 Cu 도금액 개발에 관한 것으로 환원제로 포름알데히드와 차아인산나트륨을 혼합하여 개발하였다. 이때 도금액에 차아인산나트륨이 혼합될 경우 도금속도는 증가되나 도금액의 안정성은 감소하여 착화제로 글리신을 혼합하였다. 일정량의 착화제가 포함된 도금액에 차아인산 나트륨의 첨가량을 변화시켜 개발된 도금액의 도금속도를 관찰한 결과($7.2{\mu}m/hr{\rightarrow}12.5{\mu}m/hr$)로 도금속도는 급격히 증가한 것을 확인할 수 있었다. 또한 개발된 도금액의 응력값은 ($-150Mpa{\rightarrow}-50{\sim}10Mpa$)로 급격히 감소하는 것을 확인하였다.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2014.11a
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• pp.202-203
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• 2014

금형 내부의 마모를 줄이기 위한 경질 박막의 안정성 향상과 표면에 인가된 압축 잔류 응력이 고주기 피로 특성에 미치는 영향을 연구하기 위해 정밀 플라스틱 사출 금형강에 주로 사용되는 Fe-3.0%Ni-0.7%Cr-1.4%Mn-X강에 스크린 질화처리와 DLC 코팅을 시간과 단일, 복합처리의 변수를 두어 코팅하였다. PAPVD법으로 DLC($3{\mu}m$), 스크린 질화(3h, $50{\mu}m$)/DLC($3{\mu}m$) 코팅 후 고주기 피로 시험을 행하여 고주기 피로 특성을 평가하였다. 스크래치 시험, 마모 시험, 잔류응력 측정을 통해 질화 처리 여부에 따른 코팅의 안정성을 평가하였다. DLC, 스크린질화/DLC 코팅한 경우 압축 잔류 응력의 영향으로 모두 피로 수명이 향상되었고 스크린질화/DLC 코팅한 경우 그 향상폭은 더 컸다. 질화 처리 후 DLC 코팅한 경우 질화층은 버퍼레이어로 작용하여 코팅의 박리를 억제함을 확인하였다.

• Journal of the Korea Concrete Institute
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• v.14 no.5
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• pp.766-773
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• 2002

The failure phenomenon of overlaid concrete structures, such as surface crack, and peel-off failure, shear bond failure in the end contact zone, was investigated due to humidity changes. To investigate this failure phenomenon, the surface tensile stress, and the shear stress, the vertical tensile stress in the contact zone were analysed using the non-linear stress-strain relationship of material such as strain-hardening- and strain-softening diagrams. Overlay thickness and overlay material were the main variables in the analyses. It is assumed that the initial surface humidity of overlaid concrete structures was 100％ r.H. With a atmospheric humidity of 55％ r.H. and two load cases for drying(LCI), curing and drying(LC2), the stress states of overlaid concrete structures were calculated. The result shows that only fictitious cracks occurred in the overlay surface of CM2O, ECM25, and no shear bond failure occurred in the contact zone without CM2O. The peel-off failure was proved to be the main cause of the damage in the overlaid concrete structures. Only for overlay thickness of 1cm occurred no peel-off failure in the case of drying after a long-term public use(LC1). In the case of curing and drying during overlay work(LC2) occurred the peel-off failure within 1.5days for all the overlaid concrete structures.

• Journal of the Korea Concrete Institute
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• v.13 no.5
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• pp.491-498
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• 2001

The failure phenomenon of overlaid concrete structures, such as surface crack and peel-off failure in the contact zone, was investigated due to temperature shock(rainfall). To investigate this failure phenomenon, the surface tensile stress, and the shear stress, the vertical tensile stress in the contact zone were analysed using the non-linear stress-strain relationship of material such as strain-hardening- and strain-softening diagrams. Rainfall intensity, overlay thickness and overlay material were the main variables in the analyses. It is assumed that the initial temperature of overlaid concrete structures was heated up to 55$\^{C}$ by the solar heat. With a rain temperature 10$\^{C}$ and the rainfall intensity of nR=1/a, tR=10min, 60min, the stress states of overlaid concrete structures were calculated. The result shows that only fictitious cracks occurred in the overlay surface and no shear bond failure occurred in the contact zone. The vortical tensile stress increasing with overlay thickness was proved to be the cause of peel-off failure in the contact zone. The formulae for relationship between the vertical tensile stress and overlay thickness, material properties were derived. Using this formulae, it is possible to select proper material and overlay thickness to prevent failure in the contact zone due to temperature shock caused by rainfall.

• Journal of the Korean Ceramic Society
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• v.40 no.8
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• pp.770-776
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• 2003

#140 mesh and #600 mesh wheels were adopted to grind (111) and (100) oriented single crystalline silicon wafer and the grinding induced change of the surface integrity was investigated. For this purpose, microroughness, residual stress and phase transformation were analyzed for the ground surface. Microroughness was analyzed using AFM (Atomic Force Microscope) and crystal structure was analyzed using micro-Raman spectroscopy. The residual stress and phase transformation were also analyzed after thermal annealing in the air. As a result, microroughness of (111) wafer was larger than that of (100) wafer after grinding. It was observed using Raman spectrum that the silicon was transformed from diamond cubic Si-I to Si-III(body centered tetragonal) or Si-XII(rhombohedral). Residual stress relaxation was also shown in cavities which were produced after grinding. The thermal annealing was effective for the recovery of the silicon phase to the original phase and the residual stress relaxation.

• Journal of the Society of Naval Architects of Korea
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• v.29 no.2
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• pp.115-122
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• 1992

A sandwich element is a special Hybrid structural form of the composite construction, which is consisted of three main parts : thin, stiff and relatively high density faces separated by a thick, light, and weaker core material. In a sandwich construction, the shear deformation of the faces. Therefore, in the calculation of the bending stiffness, the shear effect should be included. In this paper, the minimum weight is selected as an object function, as the weight critical structures are usually composed of these kind of construction. To obtain the minimum weight of sandwich panel, the principle of minimum potential energy is used and as for the design constraints, the allowable bending stress of face material, the allowable shear stress of core material, the allowable value of panel deflection and the wrinkling stress of faces are adopted, as well as the different boundary conditions. For the engineering purpose of sandwich panel design, the results are tabulated, which are calculated by using the nonlinear optimization technique SUMT.