• Transactions of the Korean Society of Mechanical Engineers A
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• v.41 no.10
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• pp.959-965
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• 2017

In recent years, major airplane manufacturers have been using the laminate failure theory to estimate the strain of composite structures for airplanes. The laminate failure theory uses the failure strain of the laminate to analyze composite structures. This paper describes a procedure for the experimental assessment of laminate tensile failure characteristics. Regression analysis was used as the experimental assessment method. The regression analysis was performed with the response variable being the laminate failure strain and with the regressor variables being two-ply orientation ($0^{\circ}$ and ${\pm}45^{\circ}$) variables. The composite material in this study is a carbon/epoxy unidirectional (UD) tape that was cured as a pre-preg at $177^{\circ}C(350^{\circ}F)$. A total of 149 tension tests were conducted on specimens from 14 distinct laminates that were laid up at standard angle layers ($0^{\circ}$, $45^{\circ}$, $-45^{\circ}$, and $90^{\circ}$). The ASTM-D-3039 standard was used as the test method.

• Journal of the Korea Convergence Society
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• v.10 no.1
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• pp.155-161
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• 2019

As composite is the light weight material whose durability and mechanical property are more superior than the existing general material. By taking notice of the composite with light weight, this study was about to investigate the static fracture characteristic of the bonded CFRP structure jointed with adhesive. Also, CFRP double cantilever beam with the variable of laminate angle was designed and the static fracture analysis was carried out. The laminate angles of CFRP double cantilever beam designed for this study were $30^{\circ}$, $45^{\circ}$ and $60^{\circ}$ individually. As the study result, the specimen with the laminate angle of $45^{\circ}$ was shown to have the durability better than those with the layer angles of $30^{\circ}$ and $45^{\circ}$. It was checked that the specimen with the laminate angle of $30^{\circ}$ had the weakest durability among all specimens. The damage data of the bonded CFRP structure by laminate angle could be secured through this study result. As the damage data of bonded interface obtained on the basis of this study result are utilized, the esthetic sense can be shown by being grafted onto the machine or structure at real life.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2013.05a
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• pp.1317-1318
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• 2013

• Journal of the Korean Academy of Esthetic Dentistry
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• v.1 no.1
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• pp.50-57
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• 1992

Intrinsic discoloration of permanent anterior teeth is a continuing esthetic problem. Tetracycline ingested during amelogenesis has long been recognized as predisposing factor in intrinsic staining. Methods for restoring original tooth color have included (1) complete PFM crown coverage (2) porcelain laminate veneers (3) direct bonding of composite resin, and (4) bleaching. In the case of tetracycline-stained upper anterior teeth, We authors, obtained the satisfactory results by means of gingivectomy, preliminary bleaching and porcelain laminate veneer restoration.

• Proceedings of the KSME Conference
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• 2003.11a
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• pp.1388-1393
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• 2003

In this study, analytic stress-displacement solutions are obtained by using a shear lag modeling constructed for the spliced joint area with a splicing gap filled with adhesive material of elastic modulus $E_{a}$ in the fiber metal laminate (FML) which is known to have excellent fatigue, corrosion and fire-flame resistant characteristics while with relatively low densities compared to the conventional aluminum alloys for lightweight structures.

• The Journal of the Korean dental association
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• v.27 no.8 s.243
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• pp.747-762
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• 1989

Enamal은 인간의 몸중에서 가장 단단한 조직이다. 이것은 치관을 덮고 있으며 Dentin을 보호한다. 치아의 색깔은 Dentin을 덮고있는 enamel의 두께에 의해 결정된다. 절단면은 Dentin이 없기 때문에 gray-white이며 치경부는 Dentin을 덮고 있는 enamel의 두께가 얇기 때문에 Yellow-white이다. 이러한 면에서 볼때 치관의 색깔은 Dentin이 투과성이 있는 enamel을 통과해서 나오는 색깔과 enamel자체의 색깔이 혼합되어서 만들어 진다고 할 수 있다. 현재 미형적(esthetic)으로 사용되고 있는 PFM은 이러한점을 완전히 만족시킬 수 없다. 잘 선택된 경우에 이러한 측면에서 SHADE를 완전히 만족시킬 수 있는 보철물이 있다. 바로 Porleain laminate veneer이다.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 1996.11a
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• pp.287-290
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• 1996

The behaviour of interfacial charge in EPDM/XLPE laminates has been investigated by measuring charge distributions using a pulsed electroacoustic (PEA) method. Homocharge develops in EPDM while heterocharge develops in XLPE. A broadly interfacial charge peak is observed at EPDM/XLPE interface. When EPDM /XLPE laminates are treated in high temperature for different times, the amount and polarity of interfacial charge are changed.

• Proceedings of the Korean Fiber Society Conference
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• 2001.10a
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• pp.326-326
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• 2001

Epoxy/glass fiber 복합재는 높은 strength와 stiffness를 갖는 장점이 있지만 impact strained energy를 효율적으로 발산시킬 수 있는 mechanism을 가지고 있지 않기 때문에 damping 능력이 떨어진다 Impact strength와 damping 성능을 증가시키기 위해 사용되어지고 있는 방법은 형상기억 고분자를 이용한 것으로 상대적으로 높은 strength와 impact에 대한 흡수 및 발산을 가지고 있다 형상기억 고분자는 glass transition temperature(G$_{g}$) 근처에서 높은 damping 능력을 가지고 있다. (중략)

• Proceedings of the Korean Fiber Society Conference
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• 2001.10a
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• pp.195-198
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• 2001

최근 지능재료에 관한 연구가 형상기억합금, 반도체 재료, 의료용 재료, 고분자 재료 등에서 활발히 이루어지고 있다. 지능재료 중 형상기억재료는 형상기억, 형상고정, 충격흡수 등의 효과를 갖기 때문에 열적, 역학적, 전기적 및 자기적(magnetic) 자극을 감지함으로써 형상, 위치, 탄성계수, damping, 마찰 등의 특성변화를 통하여 응답을 할 수 있어 응용이 다양하다 형상기억고분자의 경우 가볍고 형상회복률이 높으며 가공성이 우수한 장점을 가지고 있다. (중략)

• Structural Engineering and Mechanics
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• v.5 no.6
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• pp.705-713
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• 1997

The residual thermal stresses at the interface corner between the elastic fiber and the viscoelastic matrix of a two-dimensional unidirectional laminate due to cooling from cure temperature down to room temperature were studied. The matrix material was assumed to be thermorheologically simple. The time-domain boundary element method was employed to investigate the nature of stresses on the interface. Numerical results show that very large stress gradients are present at the interface corner and this stress singularity might lead to local yielding or fiber-matrix debonding.