• Polymer(Korea)
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• v.32 no.4
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• pp.313-321
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• 2008

Acrylic pressure sensitive adhesive(PSA) was prepared by UV radiation curing and the peel energy and physical properties of PSA were investigated. The increase of amount of acrylic acid leads to improve the peel energy, associated with the substrate having smooth surface and high layer thickness. The high peel energy is obtained when the direction of irregularity in substrate is horizontal with the peeling direction. This is attributed to the increase of resistance to peeling in spite of decrease of wetting and the result corresponds to our supposition.

• Journal of Korean Society of Steel Construction
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• v.8 no.4 s.29
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• pp.51-58
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• 1996

연직하중을 받는 적층보에서 박리좌굴하중을 산정하는 방법을 제시하였다. 재료역학적 방법에 근거하여 박리된 보의 변위함수를 설정하였으며 힘과 변위의 적합조건을 이용하여 연직하중과 박리좌굴하중과의 관계식을 유도하였다. 또한 박리의 진전을 판단하기 위한 변형도에너지 방출율(release rate)을 산정하였다. FRP로 보강된 GLULAM보에 대한 실험과 비교한 이론해는 정확한 결과를 보여 주었으며 연직하중을 받는 적층보의 박리 진전현상은 축하중을 받는 보와는 다른 거동을 보였다.

• Journal of the Korean Society for Nondestructive Testing
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• v.17 no.1
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• pp.1-10
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• 1997

In this paper, the effects of temperature change (low and high temperature) on the impact damages of CFRP laminates was experimentally studied. Composite laminates used for this experiment are CF/epoxy orthotropic laminated plates, which have two-interfaces $[0^{\circ}\;_6/90^{\circ}\;_6]s$ and $[0^{\circ}\;_4/90^{\circ}\;_4]s$. And CF/PEEK orthotropic laminated plates, which have two-interfaces $[0^{\circ}\;_4/90^{\circ}\;_4]s$. And, this study aims experimentally to present the interrelations between the impact energy vs. impact damages (i.e. delamination area and matrix crack) of CFRP laminates (CF/epoxy, CF/PEEK) subjected to FOD(foreign object damage) under low and high temperatures. A steel ball launched by the air gun collides against CFRP laminates to generate impact damages.

• Proceedings of the Korean Vacuum Society Conference
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• 2016.02a
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• pp.334.1-334.1
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• 2016

다른 재료에 비해 에너지 변환 효율의 관점에서 높은 경쟁력을 가진 결정질 실리콘은 지난 수십 년 동안 그 특성이 태양전지 분야에 널리 이용되어 왔다. 하지만 결정질 실리콘 웨이퍼는 일반적으로 제조 단계에서 많은 양의 에너지를 소비하고 절단 단계에서 절단 손실(Kerf-loss)이 발생된다. Epoxy Resin을 이용한 Kerf-less Wafering은 초박형 실리콘 웨이퍼 제조 기술 중 하나로, 비교적 간단한 장비와 공정을 통하여 절단 손실 없이 $50{\mu}m$이하의 초박형 실리콘 웨이퍼를 얻을 수 있는 기술이다. 실리콘과 Epoxy Resin 간의 열팽창 계수 차이를 이용하여 초박형 실리콘을 박리 시키는 기술로, 실리콘 기판 위에 Epoxy Resin으로 stress inducing layer를 올려 공정을 진행한다. stress inducing layer를 경화시키는 열처리가 끝나고 급냉되는 과정에서 stress inducing layer에 의해 실리콘 기판에 큰 응력이 가해지게 되고 실리콘 기판에 crack이 발생된다. 공정이 계속 됨에 따라 발생된 crack은 실리콘 표면과 평행한 방향으로 전파 되고 초박형 실리콘 layer가 실리콘 기판에서 박리 된다. 본 실험에서 중요한 공정 변수로는 stress inducing layer의 구성성분 및 두께, 열처리 온도 및 시간, cooling rate 등이 있다. 이러한 공정 변수들을 조절 하여 Epoxy Resin을 이용하여 $100{\mu}m$ 이하의 박리된 wafer를 얻을 수 있었다. 박리된 wafer의 단면과 두께를 Scanning Electron Microscopy(SEM)을 통해 관찰 하였고, 이를 통해 초박형 실리콘 박리 공정에 대한 연구를 진행하였다.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2009.10a
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• pp.104-104
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• 2009

금값 폭등과 에너지자원 고갈에 따라 폐 인쇄회로기판의 유가금속 및 에너지자원을 효과적으로 회수하고자, 최근 국내외 금 회수 및 폐백보드 활용방안을 제시하였다. 금을 회수하는 방법으로는 침적박리, 농축처리, 중화처리, 수용액환원처리, 이온교환수지, 전해채취 등의 방법이 있다. 금은 상온침적박리 회수하며 폐백보드는 이동식 건축내장재로 활용하고자 한다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.39 no.10
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• pp.795-803
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• 2015

The boundary layer developing over the suction surface of a first-stage turbine blade for power generation has been investigated in this study. For three locations selected in the region where local thermal load changes dramatically, mean velocity, turbulence intensity, and one-dimensional energy spectrum are measured with a hot-wire anemometer. The results show that the suction-surface boundary layer suffers a transition from a laminar flow to a turbulent one. This transition is confirmed to be a "separated-flow transition", which usually occurs in the shear layer over a separation bubble. The local minimum thermal load on the suction surface is found at the initiation point of the transition, whereas the local maximum thermal load is observed at the location of very high near-wall turbulence intensity after the transition process. Frequency characteristics of turbulent kinetic energy before and after the transition are understood clearly from the energy spectrum data.

• Magazine of the Korea Concrete Institute
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• v.11 no.2
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• pp.177-186
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• 1999

The purpose of this study is to analyze the interface debonding of RC beams strengthened by carbon fiber sheet(CFS). The behavior of damaged RC beams strengthened with CFS is analytically investigated next using linear elastic fracture mechanics(LEFM) approach and the finite element method. The study includes an investigation of the separation mode by interface fracture of the strengthening materials due to the interfacial shear and normal stresses. The numerical method is presented to obtain the value of interfacial fracture parameter such as the strain energy release rate. Based on the results of this study, it is found that the critical case occurs when the interfacial cracks occur within a short region of the flexural crack. The CFS strengthening has not an adequate factor of safety against interfacial debonding of CFS. Furthermore, for the thicknesses of the adhesive studied[1mm~3mm], it is no noticeable effect on the strain energy release rate.

• Korean Journal of Optics and Photonics
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• v.26 no.5
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• pp.261-264
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• 2015

In this paper we show that the photoresist-protective film of a printed circuit board (PCB) can be delaminated from the underlying photoresist layer by a single pulse of a nanosecond laser at 532 nm. After locally peeling the edge of the PCB with a laser beam of 9 mm size, Scotch tape was attached to the irradiated region to peel off the whole protective film. For a certain range of pulse energies the peeling probability was 100%, without leaving any damage. Since the use of a laser in initial delamination is noncontact and nondamaging, it may be more efficiently utilized in the PCB industry than the conventional knurling method based on mechanical pressing.

• 한국신재생에너지학회:학술대회논문집
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• 2009.11a
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• pp.139-142
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• 2009

In this study, the performance degradation of SOFC single cell caused by the delamination between a cathode and an electrolyte is investigated. As the delamination rate increases, the voltage sharply decreases due to the decrease of reaction sites and losses increase. The current is concentrated to the intact area so that the current density is increased and the ohmic loss and the activation loss become higher. Most part of loss is due to the ohmc loss of electrolyte.

• Journal of the Korean Society of Propulsion Engineers
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• v.5 no.3
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• pp.60-70
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• 2001

The study of compatible liner with ADP-505 propellant based PCP was performed. HTPB/DDl was chosen as a binder of liner in order to prohibit migration of nitroester plasticizer from propellant. The possible formulations for liner were screened by peel test of EPDM insulation/liner, propellant/liner and insulation/liner/propellant. Also, the adhesion tests including tension and shear were conducted. The adhesion of liner and propellant fumed out to be very good. The peel value was shown 1.5∼1.8 daN/cm, tensile force was 5.5∼6.0bar and shear force was 4.2∼5.0bar. In the samples of insulation/liner/propellant, they also have shown good adhesion properties. The peel, tensile and shear strength were 1.8 daN/cm, 5.0∼6.0bar and 4.5∼5.0bar, respectively.