• 한국윤활학회:학술대회논문집
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• 한국윤활학회 2002년도 proceedings of the second asia international conference on tribology
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• pp.415-416
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• 2002

Experiments have been conducted to investigate scuffing mechanism in oil lubricated piston-ring /cylinder sliding contacts. Samples were extracted from actual components to simulate the real contact geometry and other influencing conditions. A standard test machine. with some modifications, has been used for the investigation of the effects of surface temperature load and sliding velocity. preliminary tests were carried out to find the critical temperature of scuffing using gradient temperature under a constant load, reciprocating frequency and stroke. The experimental and analytical results show that a transition from lubricated contact to adhesion, accompanied by the phenomena such as material transfer between the two sliding surfaces, local contact welding and temperature rise, and sharp increase in friction coefficient, appears to contribute to the final failure of scuffing.

• 대한기계학회논문집A
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• 제26권4호
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• pp.677-682
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• 2002

Break-in is an intentional treatment to enhance the performance life of machinery parts and to maintain static friction behavior. Most studies on break-in have concerned only about surface conditions such as roughness or film formation. But the exact mechanism of break-in has not been found yet. Friction, scuffing behavior and wear of AISI 1045 were studied in relation to break-in and residual stress. The cylinder-on-disk type tribometer was used with the line-contact geometry. Scuffing tests were carried out using a constant load of 730N. In the break-in procedure the step load was applied from 100N to 200N. In this experiment, it was found that the break-in helps compressive residual stress to be formed well enough to enhance the scuffing life during the scuffing test. Specimens that had high compressive residual stress induced by shot-peening show better wear resistance than those were not shot-peened. Results of scuffing test, break-in procedure and wear amount in relation to residual stress have been discussed.

• 한국기계가공학회지
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• 제20권12호
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• pp.123-128
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• 2021

Liquid dispensing systems are extensively used in various industries such as display, semiconductor, and battery manufacturing. Of the many types of dispensers, drop-on-demand piezoelectric jetting systems are widely used in semiconductor industries because of their ability to dispense minute volumes with high precision. However, due to the problems of nozzle clogging and undesirable dispensing behavior in these dispensers, which often result in device failure, the use of highly viscous fluids is limited. Accordingly, we studied the behaviors of droplet formation based on changes in viscosity. The effects of surface energy and the inner diameters of needle-type nozzles were also studied. Results showed that nozzles with lower surface energies reduced the ejection volume of droplets when a smaller nozzle diameter (0.21 mm in this study) was applied. These results indicate that the hydrophobic treatment of nozzle surfaces and the use of smaller nozzle diameters are critical factors enabling the use of highly viscous fluids in precision dispensing applications.

• 한국지반공학회논문집
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• 제38권8호
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• pp.39-52
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• 2022

사면의 안전율과 임계활동면을 다층 퍼셉트론 신경망(multi-layer perceptron, MLP)을 이용하여 구할 수 있도록 훈련하였다. 사면의 형상은 한국의 설계기준을 참고한 단순 사면으로, 건조한 경우와 지하수위가 존재하는 경우를 모두 고려하였으며 사면을 구성하는 토질의 물성은 세립분을 포함한 사질토로 고려하였다. 훈련에 필요한 데이터를 만들 때 한계평형해석법을 이용하여 42,000가지 경우의 사면안정해석을 수행하였고, 지하수위가 고려된 도메인의 해석에서 불포화토의 모관흡수력으로 인한 유효응력 증가를 고려하였다. 지하수와 유효응력의 분포를 사면안정해석에 적용할 수 있도록 정상상태 침투 해석을 수행하였다. 사면을 표현하는 물성을 입력하면 안전율과 원호 파괴면을 예측할 수 있는 MLP 모델과 모델의 성능을 정량적으로 평가할 수 있는 방법을 제시하였다.

• 한국지반공학회논문집
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• 제21권3호
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• pp.65-77
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• 2005

본 연구에서는 계단식 보강토 옹벽에 대한 측소 모형실험 수행하고 그 결과를 토대로 계단식 보강토 옹벽의 파괴 메카니즘을 분석하였다. 보강토 옹벽의 모형설험은 5m 높이의 현장옹벽에 대해 상사법칙을 적용하여 축소$\cdot$모사하였으며 상사법칙 적용 결과에 따라 보강재를 선택하여 실험을 실시하였다. 또한, 파괴 메카니즘 분석을 위해 자중에 의한 파괴를 성공적으로 유도하였다. 실험결과를 토대로 보강토 옹벽의 상$\cdot$하단 옹벽의 이격거리와 보강재 길이가 파괴 양상에 미치는 영향을 분석하였으며 아울러 현재 적용되고 있는 설계기준의 타당성 검토하였다.

• Geomechanics and Engineering
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• 제31권5호
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• pp.439-452
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• 2022

A forecast of slope behavior during catastrophic events, such as earthquakes is crucial to recognize the risk of slope failure. This paper endeavors to eliminate the significant supposition of predefined slip surfaces in the slope stability analysis, which questions the relevance of simple conventional methods under seismic conditions. To overcome such limitations, a methodology dependent on the slip line hypothesis, which permits an automatic generation of slip surfaces, is embraced to trace the extreme slope face under static and seismic conditions. The effect of earthquakes is considered using the pseudo-static approach. The current outcomes developed from a parametric study endorse a non-linear slope surface as the extreme profile, which is in accordance with the geomorphological aspect of slopes. The proposed methodology is compared with the finite element limit analysis to ensure credibility. Through the design charts obtained from the current investigation, the stability of slopes can be assessed under seismic conditions. It can be observed that the extreme slope profile demands a flat configuration to endure the condition of the limiting equilibrium at a higher level of seismicity. However, a concurrent enhancement in the shear strength of the slope medium suppresses this tendency by offering greater resistance to the seismic inertial forces induced in the medium. Unlike the traditional linear slopes, the extreme slope profiles mostly exhibit a steeper layout over a significant part of the slope height, thus ensuring a more optimized solution to the slope stability problem. Further, the susceptibility of the Longnan slope failure in the Huining-Wudu seismic belt is predicted using the current plasticity approach, which is found to be in close agreement with a case study reported in the literature. Finally, the concept of equivalent single or multi-tiered planar slopes is explored through an example problem, which exhibits the appropriateness of the proposed non-linear slope geometry under actual field conditions.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2002년도 추계학술발표대회 논문집
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• pp.88-91
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• 2002

The two dimensional size effect of specimen gauge section (length x width) was investigated on the compressive behavior of a T300/924 [45/-45/0/90]3s, carbon fiber-epoxy laminate. A modified ICSTM compression test fixture was used together with an anti-buckling device to test 3mm thick specimens with a 30$\times$30, 50$\times$50, 70$\times$70, and 90mm$\times$90mm gauge length by width section. In all cases failure was sudden and occurred mainly within the gauge length. Post failure examination suggests that $0^{\circ}$ fiber microbuckling is the critical damage mechanism that causes final failure. This is the matrix dominated failure mode and its triggering depends very much on initial fiber waviness. It is suggested that manufacturing process and quality may play a significant role in determining the compressive strength. When the anti-buckling device was used on specimens, it was showed that the compressive strength with the device was slightly greater than that without the device due to surface friction between the specimen and the device by pretoque in bolts of the device. In the analysis result on influence of the anti-buckling device using the finite element method, it was found that the compressive strength with the anti-buckling device by loaded bolts was about 7% higher than actual compressive strength. Additionally, compressive tests on specimen with an open hole were performed. The local stress concentration arising from the hole dominates the strength of the laminate rather than the stresses in the bulk of the material. It is observed that the remote failure stress decreases with increasing hole size and specimen width but is generally well above the value one might predict from the elastic stress concentration factor. This suggests that the material is not ideally brittle and some stress relief occurs around the hole. X-ray radiography reveals that damage in the form of fiber microbuckling and delamination initiates at the edge of the hole at approximately 80% of the failure load and extends stably under increasing load before becoming unstable at a critical length of 2-3mm (depends on specimen geometry). This damage growth and failure are analysed by a linear cohesive zone model. Using the independently measured laminate parameters of unnotched compressive strength and in-plane fracture toughness the model predicts successfully the notched strength as a function of hole size and width.

• Advances in aircraft and spacecraft science
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• 제4권4호
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• pp.353-369
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• 2017

Flutter is a dangerous phenomenon encountered in flexible structures subjected to aerodynamic forces. This includes aircraft, buildings and bridges. Flutter occurs as a result of interactions between aerodynamic, stiffness, and inertia forces on a structure. In an aircraft, as the speed of the flow increases, there may be a point at which the structural damping is insufficient to damp out the motion which is increasing due to aerodynamic energy being added to the structure. This vibration can cause structural failure, and therefore considering flutter characteristics is an essential part of designing an aircraft. Scientists and engineers studied flutter and developed theories and mathematical tools to analyze the phenomenon. Strip theory aerodynamics, beam structural models, unsteady lifting surface methods (e.g., Doublet-Lattice) and finite element models expanded analysis capabilities. Periodic Structures have been in the focus of research for their useful characteristics and ability to attenuate vibration in frequency bands called "stop-bands". A periodic structure consists of cells which differ in material or geometry. As vibration waves travel along the structure and face the cell boundaries, some waves pass and some are reflected back, which may cause destructive interference with the succeeding waves. This may reduce the vibration level of the structure, and hence improve its dynamic performance. In this paper, for the first time, we analyze the flutter characteristics of a wing with a periodic change in its sandwich construction. The new technique preserves the external geometry of the wing structure and depends on changing the material of the sandwich core. The periodic analysis and the vibration response characteristics of the model are investigated using a finite element model for the wing. Previous studies investigating the dynamic bending response of a periodic sandwich beam in the absence of flow have shown promising results.

• 터널과지하공간
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• 제13권1호
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• pp.64-75
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• 2003

본 연구에서는 2001년 Bakers와 Stephansson이 제안한 Punch Through Shear Test를 소개한다. 본 연구의 목적은 대전화강암을 사용하여 이 시험법이 암석의 전단 모드 파괴 인성 측정법으로서의 적합성을 알아보는 것이다. 또한, 전단모드 파괴인성을 구하기 위한 최적의 시료형상을 결정하고 전단모드 파괴인성과 봉압과의 관계를 규명하였다. 시험결과, 인장 파괴에서와 같이 거친 파괴면이 형성되지 않고 전단을 받았음을 알 수 있는 부드러운 파괴면이 관찰되었다. 시료형상에 대한 연속체 해석과 입자유동 해석 그리고 균열전파 시뮬레이션을 수행한 결과 시료내부에서 일어나는 균열의 발생은 주로 전단모드이고 이러한 전단균열들로 인해 시료의 파괴가 발생함을 입증할 수 있었으며, 결과적으로 Punch Through Shear Test는 암석의 전단모드 파괴인성 측정법으로서 적합함을 입증할 수 있었다.

• 한국지반공학회지:지반
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• 제9권2호
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• pp.41-54
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• 1993

본 연구는 이질토층의 c-o흙사면에 대한 2차원 및 3차원 안정해석을 제시한다. 가능파괴면은 층의 경계에서 파괴면이 내부마찰각에 따라 굴절되는 대수나선곡선을 사용하였다. 3 차원 해석에서는 회전활동토괴는, 중앙부는 Cylindroid이고 양쪽 끝단은 평면으로 사용하였 다. 지진력은 수평 및 수직진도를 고려하였다. 개발한 프로그램을 PCSTABLS와 비교하였고, 2차원 최소안전율에 대한 3차원의 최소안전율의 비를 조사하였고, 사면높이에 대한 Cylindroid길이의 비에 따른 안전율의 변화를 검토하였다. 그리고 절편의 수에 따른 안전율의 변 화도 조사하였다. 이러한 것을 기초로 다음의 결과가 얻어졌다 : (1)본 연구에서 개발된 프로그램의 2차원 안전율이 PCSTABLS보다는 더 크게 나타났다. (2)본 연구의 2차원 안전율은 흙의 내부 마 찰각이 증가함에 따라 PCSTABLS보다 더 큰차이를 나타냈다. (3) 3차원 안전율은 2차원 안전율보다 더 크게 나타났다. 따라서 3차원효과는 안전율을 증가시키는 경향이 있다. (4) 사면의 높이에 대한 3차원 파괴토괴의 폭의 비, bye가 증가함에 따라 2차원 안전율에 대한 폭, b를 가진 3차원 안전율의 비, Fb/F거 값은 감소하였고, bye가 약 14이상이면 1.0에 근접 했다. (4) 2차원 안전율에 대한 폭, b를 가진 3차원 안전율의 비, Fb/F거 값은 전단강도정수, 지하수위 그리고 수평진도의 값에 매우 민감한 것으로 나타났다. (5) 본 연구에서 개발된 프로그램을 사용하여 안전율을 계산할때,절편의 수는 30~40개 정도면 적당하였다.