• 한국항공우주학회지
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• 제31권9호
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• pp.18-25
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• 2003

본 연구에서는 탄소/페놀릭 8-매 주자직 복합재료인 ACP302의 등가열전도계수를 단위구조해석을 통하여 계산하였고 또한 실험적으로 측정하였다. 먼저 8-매 주자직 복합재료의 직조섬유다발구조를 3차원 유한요소를 사용하여 미세역학적으로 상세히 모델링하였으며, 단위구조 경계면에는 주기경계조건을 가하고 해석을 수행하였다. 계산결과로부터 적층 형상 및 굴곡도, 섬유 체적비 등이 등가열전도도에 미치는 영향을 조사하였다. 또한 실험을 수행하여 열전도도를 계측하였으며 그 결과를 계산결과와 비교하였다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2002년도 추계학술발표대회 논문집
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• pp.48-51
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• 2002

This paper predicted the thermal conductivity of spun carbon/phenolic composites by the thermal resistance method. This method uses the analogy between the diffusion of heat and electrical charge. To verify the theoretical predictions, the thermal conductivity of spun carbon/phenolic composites was examined experimentally. The reported thermal conductivities of graphite/epoxy composite of a eight harness satin laminate was used of the comparison with the prediction values of the model and it was noticed that a good agreement has been found.

• 한국전산구조공학회논문집
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• 제14권4호
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• pp.455-467
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• 2001

본 논문에서는 일축인장하중을 받고 있는 8-매 주자직 복합재료의 적층 위상변화가 등가물성치 및 응력분포에 미치는 영향을 연구하였다. 등가물성치 및 응력은 임의의 배열을 갖는 적층 구조물에 대한 단위구조 해석을 통해 계산하였으며, 마크로요소를 사용하여 효율적인 계산을 수행하였다. 계산 결과, 섬유다발 미세구조의 변화는 응력분포에 큰 영향을 미치는 것으로 나타났다. 섬유다발 및 수지에서의 응력은 섬유다발의 이동에 따라 서로 다른 분포를 보였고, 수지영역에서의 최대응력은 매우 넓은 범위에 걸쳐 분포하였다.

• 한국항공우주학회지
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• 제31권7호
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• pp.41-52
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• 2003

본 연구에서는 탄소/페놀 8-매 주자직 복합재료의 기하학적 매개변수를 고려하여 3차원 열적 및 기계적 등가물성치를 예측하였다. 등가탄성계수와 열팽창계수는 일축인장하중과 순수전단, 가상의 온도변화 등을 수치적으로 모사하는 수치실험을 통하여 계산하였다. 8-매주자직 복합재료의 미세구조는 마크로요소를 통하여 모델링 하였고 단위구조해석을 위해 주기경계조건을 유도하였다. 또한 다양한 층간 위상차를 고려하기 위해 모작위 표본 해석을 수행한 후 그 결과에 대하여 통계처리를 수행하였고, 해석결과는 인접층간 위상차와 적층수 및 굴곡도 등의 매개변수가 등가물성치에 미치는 영향의 관점에서 조사되었다. 그리고 시편에 대한 실험을 실시하여 계산결과와 비교하였다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2001년도 추계학술발표대회 논문집
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• pp.74-78
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• 2001

In this study, out-of-plane properties and CTEs were predicted for 8-harness satin weave textile composites. The properties were calculated by unit cell analysis for configurations with varied waviness ratio and phase shifts. Macro elements were employed to reduce the computer resource requirement. It was found that the out-of-plane properties and CTEs were varied as the phase shift changed. However the dependency was much weaker than the in-plane properties.

• 대한가정학회지
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• 제27권1호
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• pp.1-8
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• 1989

In order to investigate the mechanical properties such as tensile, bending, shearing, thickness and weight of the wool fabrics were measured by KES-F system. Samples were classified into blend ratio, weave type, fabric count. Blend ratio was classified into two groups, which are P/W blended fabric (p=63~65%, w=35~37%) and all wool fabric. Weave type was classified into four groups, which are plain, 3 harness twill, 4harness twill, satin. Cloth count was classified into three groups, which are loose, medium, tight. Statistical analysis was performed using T-test, F-test. The results were as follows; 1. There was significant difference in the thickness, tensile, bending, shearing according to the blend ratio. 2. According the weave, there was significant difference in the bending, weight and thickness in the P/W blended fabrics. There was significant difference in the tensile, weight, thickness, bending, shearing, shearing hysterisis (2HG) in the all wool fabrics. 3. There was significant difference in the shearing properties according to the fabric count.

• 대한기계학회논문집
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• 제18권8호
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• pp.2053-2061
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• 1994

The static and fatigue tensile tests have been conduted to predict the fatigue life of 8-harness satin woven and plain woven carbon/epoxy composite plates containing a circular hole. A fatigue residual strength degradation model, based on the assumption that the residual strength for unnotched specimen decreases monotonically, has been applied to predict statistically the fatigue life of materials used in this study. To determine the parameters(c, b and K) of the residual strength degradation model, the minimization technique and the maximum likelihood method are used. Agreement of the converted ultimate strength by using the minimization technique with the static ultimate strength is reasonably good. Therefore, the minimization technique is more adjustable in the determination of the parameter and the prediction of the fatigue life than the maximum likelihood method.

• 대한기계학회논문집
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• 제19권8호
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• pp.1915-1926
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• 1995

The Fatigue characteristics of 8-harness satin woven CFRP composites with a circular hole are experimentally investigated under constant amplitude tension-tension loading. It is found in this study that the fatigue damage accumulation behavior is very random and history-independent, and the fatigue cumulative damage is linearly related with the mean number of cycles to a specified damage state. From these results, it is known that the fatigue characteristics of CFRP composites satisfy the basic assumptions of Markov chain theory and the parameter of Markov chain model can be determined only by mean and variance of fatigue lives. The predicted distribution of the fatigue cumulative damage using Markov chain model shows a good agreement with the test results. For the fatigue life distribution, Markov chain model makes similar accuracy to 2-parameter Weibull distribution function.

• 대한기계학회논문집A
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• 제35권8호
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• pp.913-920
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• 2011

본 논문은 4-매 주자직 유리섬유/에폭시 적층 복합재가 적용된 철도차량 경량 대차프레임의 피로 수명 및 강도 평가에 대해 기술한다. 대차프레임 경량화 재질로 적용된 유리섬유/에폭시 4-매 주자직 적층 복합재료의 피로특성 평가를 위하여 경사, 위사 그리고 $0^{\circ}/90^{\circ}$ 방향으로 적층된 시험편에 대하여 인장-압축 피로시험을 수행하였다. 유리섬유/에폭시 4-매 주자직 적층 복합재료의 피로시험은 5Hz의 주파수, -1의 응력비(R), $10^7$의 피로수명을 갖도록 하였다. 또한, JIS E 4207의 하중조건에 따른 대차프레임의 피로강도 평가를 Goodman 선도를 통하여 수행하였다. 유리섬유/에폭시 적층 복합재 경량 대차프레임의 피로수명 및 강도 평가기준을 만족하였으며, 무게를 고려할 경우 기존 대차프레임 재질인 SM490A 금속재에 비하여 우수한 피로특성을 갖는다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 1999년도 추계학술발표대회 논문집
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• pp.160-163
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• 1999

The mechanical properties and failure behaviour of carbon/phenolic composites were inverstigated by tension and compression. Carbon/phenolic composites were fabricated by infiltration of matrix into 8 harness satin woven fabric of PAN-based carbon fibers. The tensile and compressive tests were performed at 25℃ under air atmosphere and, at 400℃ and 700℃ under N₂ atmosphere. The tensile strengths of carbon/phenolic composites in with-laminar/0° warp direction were about 10 times higher than those in with-laminar/45° warp direction, which was analyzed due to a change of fracture mode from fiber pull-out by shear to tensile fracture of fibers. The fracture of carbon/phenolic composites in with-laminar/45° direction was analyzed due to delamination by buckling. Tensile and compressive strength of carbon/phenolic composites decreased to about 50% at 400℃, and to about 10% at 700℃ compared to that at room temperature. The main reason for the decrease of tensile or compressive strength with increasing temperature was analyzed due to a reduction of bond strength between fibers and matrix resulting from thermal degradation of phenolic resin.