• Proceedings of the Materials Research Society of Korea Conference
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• 2003.03a
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• pp.228-228
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• 2003

고강성 탄소섬유는 높은 비강도 및 고 강성 특성 때문에 탄소-탄소 복합재료의 가장 우수한 강화재로 각광을 받고 있다. 이 섬유는 미세 결정립의 높은 이방성을 나타내며, 이러한 높은 흑연화 특성은 기계적, 전기적, 전기적 그리고 화학적 특성 등을 좋게한다. 이러한 모든 방면에서의 우수한 특성 때문에 항공우주 재료분야에 의심 없이 가장 우수한 재료로 고려되고 있다. 이렇게 가벼우면서 고온강도가 요구되는 재료로써 탄소재료가 이용되면서 rocket의 nozzle이나 nosecone으로의 응용에는 고온 산화가 중요한 연구주제로 대두되어 왔다. 탄소재료의 산화반응은 결정구조 인자 및 그 배열에 가장 큰 영향을 받는다고 알려져 있는데, 출발원료 및 제조 조건에 따라 그 구조 및 배열이 현격하게 달라진다. 탄소재료의 구조 해석은 주로 TEM과 XRD를 이용해 왔다. 많은 연구자들은 오래 전부터 탄소재료 연구에 TEM에서 얻은 상이 불확실하고 문제가 있다고 보고하였고, 최근 TEM 장치의 발달과 더불어 실제 구조를 얻기가 가능함을 보여주고 있다 그러나 TEM 시편은 여전히 작고 시편으로부터 얻는 정보는 불과 nm 수준이다. 따라서 일반적으로 TEM으로 얻은 정량적인 정보는 불과 특정한 점에서의 정보이기 때문에 여전히 논란의 소지가 많다. XRD는 탄소재료의 미세구조 해석을 위하여 가장 널리 이용되는 분석기기이다.

• Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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• 1993.04a
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• pp.59-62
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• 1993

고품위의 동력전달 장치와 같은 고정밀 기능 부품들은 보다 높은 비강도, 고경도, 내마모성 및 내식성을 가져야 하며, 특히 소재의 마찰, 마모 특성은 기아제품 등의 수명, 정밀도 및 에너지 손실을 좌우하는 것으로서 물성의 열화를 극복할 수 있는 소재의 개발이 요구되고 있다. 지난 수년동안 금속기지에 $Al_2O_3$나 SiC등의 보강재를 첨가하여 복합재의 응착 및 연삭마모에 대한 저항성을 향상시키는 시도를 하고 있다. 주로 제조비용이 낮고 거의 등방적인 성질을 가지며 가공성이 좋은 입자 보강 복합재료에 대한 연구가 지배적이었지만, 입자 보강 복합재료의 경우 강도 및 탄성계수의 향상 정도가 적다는 단점을 지니고 있다. 본 연구에서는 분말야금법을 이용하여 금속기지에 세라믹상으로 SiC 입자 및 휘스커가 첨가된 복합재를 제조하여 제조공정변수에 따라 마모거동을 pin-on-disk 형태의 마모시험기에서 실험하였으며, 주사전자현미경으로 마모표면관찰 등으로 복합재의 마모기구를 연구하였다.

• Composites Research
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• v.16 no.2
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• pp.1-8
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• 2003

Thus paper summarizes the procedures to develop the downscaled payload kick motor for KSR-III by KARI. Filament winding-a well-known method of manufacturing composite motor case - is adopted to reduce structural weight. Netting and lamination theories are used to determine adequate winding thickness under required internal pressure. Dome shapes are designed considering feasible winding patterns and easiness of mandrel manufacturing. T-800 carbon fiber and Novolac type resin are selected for weight-reduction. The separate mandrels are disassembled and removed after filament winding. The manufacturing process of real payload kick motor is developed from the design experience of downscaled ones.

• Transactions of the Korean Society of Mechanical Engineers
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• v.16 no.5
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• pp.838-848
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• 1992

The objective of the study is to provide a theoretical tools for analyzing the fracture of leyered composites with a center crack. It is assumed that the composite is composed of successive accumulation of the fiber layer and resin layer with the fiber layer being perfectly bonded to the resin layer except the region of a center crack. In-plane shear loading (Mode II) and the anti-plane shear loading (Mode III) are considered separately. Boundary value problems are formulated by using a plane theory of elasticity and governing equations are reduced to a Fredholm integral equation of a second kind. The equation is solved numerically and the stress intensity factors are obtained. The normalized Mode II and Mode III stress intensity factors are evaluated for various combinations of material properties and for various geometrical parametes.

• Journal of KIISE:Software and Applications
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• v.29 no.1_2
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• pp.20-29
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• 2002

The composite stock cutting problem is to allocate rectangular and/or irregular patterns onto a large composite stock sheet of finite dimensions in such a way that the resulting scrap will be minimized. In this paper, the distributed simulated annealing with the new cost error tolerant spatial decomposition is applied to the composite stock cutting problem in MPI environments. The cost error tolerant scheme relaxes synchronization and chooses small perturbations on states asynchronously in a dynamically changed stream length to keep the convergence property of the sequential annealing. This paper proposes the efficient data structures for representation of patterns and their affinity relations and also shows how to determine move generations, annealing parameters, and a cost function. The spatial decomposition method is addressed in detail. This paper identifies that the final quality is not degraded with almost linear speedup. Composite stock shapes are not constrained to convex polygons or even regular shapes, but the rotations are only allowed to 2 or 4 due to its composite nature.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.20 no.9
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• pp.2782-2791
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• 1996

The effective longitudinal shear modulus(LSM) of continuous composites is studied theoretically and numerically using 3-phase unit cell model. Circular, hexagonal and rectangular shapes of reinforced fiber are considered to predict the shear modulus as a function of elastic modulus of each phase and volume fraction of interphase and reinforced fiber. It is found that rectangular fiber shape in low fiber volume fraction($v_f$<30%) and circular fiber shape in high volume fraction($v_f$>40%) shows the higher longitudinal shear modulus. Also the obtained values of LSM for rectangular array and by numerical analysis are higher than those of hexagonal array and by theoretical analysis respectively. The reinforcing effects of interphase are more significant in cases of higher fiber volume fraction and circular fiber shape. Not only the spatial distribution and shape of reinforcing fiber but also the volume of interphase have a pronounced effects on the overall LSM. It is also found that the tangent moduous of 2-and 3-phase polymer matrix composites is insensitive to the shape and distribution of reinforcing fibers.

• Proceedings of the Korean Society For Composite Materials Conference
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• 2002.05a
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• pp.195-198
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• 2002

Two types of conformal load-bearing antenna structure (CLAS) were designed with microwave composite laminates and Nomex honeycomb cores, to give both structural rigidity and good electrical performance. One is 4$\times$8 array for Synthetic Aperture Radar(SAR) system and the other is $5\times2$ array for wireless LAN system. Design was based on wide bandwidth, high polarization purity, low loss and good structural rigidity. We studied the design, fabrication and structural/electrical performances of the antenna structures. The flexural behavior was observed under a 3-point bending test, an impact test, and a buckling test. Electrical measurements were in good agreement with simulation results and these complex antenna structures have good flexural characteristics. The design of this antenna structure is extended to give a useful guide for sandwich panel manufacturers as well as antenna designers.

• Proceedings of the Korean Society For Composite Materials Conference
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• 2001.05a
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• pp.42-45
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• 2001

The characteristics of smart skin for wireless LAN system under compression load are investigated. The smart skin structure is composed of 3 layers of face material and 2 layers of core material. Theoretical formula for determining buckling load is derived by Rayleigh-Ritz method and compared with experimental result. The maximum length of specimen that buckling does not occur is determined by only face material. In the experiment, if load supporting capability and the antenna property such as radiation pattern and reflection coefficient were examined.

• Journal of the Korean Society for Nondestructive Testing
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• v.31 no.2
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• pp.150-156
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• 2011

In this paper, infrared thermography measurement technique has been used to develop standard measurement technique for nondestructive testing of composite materials which is widely used in aerospace industries. To increase the defect detection rate, the related experiment used the lock-in IR-thermographiy method. Therefore it is of considerable interest in the field of non-destructive testing for fast discontinuity detection by using ultrasonic lock-in infrared thermography. The result also shows that as the investigation period of light source is lengthened according to the thickness of specimen, the possibility of detecting defects gets higher as well. However, the reason why the result values were not favorable when less than 50 mHz of light source was provided is because it was difficult to detect defects as the defect parts became a state of thermal equilibrium in general when thermal diffusivity affects the entire materials.

• Composites Research
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• v.12 no.3
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• pp.36-44
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• 1999

The fabrication process of $Al_2O_{3p}/Al$ composite by in-situ process was investigated. The effects of processing variables such as addition type and content of Mg, processing temperature and time on the infiltration behavior of molten Al, microstructure and hardness were investigated. When the pure Al was infiltrated into mixtures of Mg and $Al_2O_3l$ powder, processing temperature required to spontaneous infiltration was decreased, and the content of Mg was the most powerful variable for infiltration of molten Al. But when the Al-Mg alloy was infiltrated into $Al_2O_3l$ particles, infiltration ratio indicated nearly same value regardless of Mg content in alloy and processing temperature, and critical processing temperature required to spontaneous infiltration was $800^{\circ}C$. The $Al_2O_{3p}/Al$ composites which were fabricated by mixtures of Mg and $Al_2O_3l$ powders resulted in high hardness value, but hardness values were scattered due to non uniform dispersion of $Al_2O_3l$ particles by excessive reaction of Mg.