• Composites Research
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• 제18권1호
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• pp.38-44
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• 2005

본 연구에서는 단일방향 탄소섬유강화복합재료 판에서 $S_o$ 대칭모드의 군속도 분선곡선을 전파 방향을 변화시키먼서 계산하였다. 그리고 속노 분산 곡선에서 첫 번째 단절주파수 이하인 0.2 MHz-mm에 해당하는 $S_o$ 대칭모드 군속도를 가지고서 위상속도 곡선을 얻고 slowness 곡선을 도입하여 군속도 곡선으로 교정하였다. 단일방향 섬유강화복합재료 판에서 $S_o$ 대칭모드의 속도를 전파 방향을 변화시키면서 측정하였고 교정된 군속도 곡선과 비교하였다. 측정된 속도는 섬유 방향 근처의 cusp 영역을 제외하고는 교정된 군속도 곡선과 잘 일치하였다. 이것은 단일방향 탄소섬유강화복합재료 판에서 속도가 빠른 방향으로 에너지를 더 잘 전파하기 때문에 전파 방향이 주축방향과 일치하지 않을 때 군속도 방향은 섬유 방향 쪽으로 기울어지는 결과로 나타난 것이다.

• 한국산학기술학회논문지
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• 제11권2호
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• pp.426-434
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• 2010

본 논문에서는 충격손상을 갖는 유리섬유강화 복합재료의 강도 저하 특성과 이의 통계적 특성을 실험적으로 평가하였다. 평직 복합재료의 주요 충격손상은 섬유파단과 모재균열로서 이는 층간분리가 주된 충격손상인 일방향 적층복합재료와는 상이한 양상이다. 일방향 적층복합재료에 대하여 제안된 기존의 잔류강도 예측모델을 이용하여 충격손상을 갖는 평직 glass/epoxy 복합재료의 잔류강도를 평가하였다. 그 결과 Avva 및 Caprino의 잔류강도 예측모델은 평직 복합재료의 잔류강도에 대해서도 잘 평가되었다. 또한 유리섬유강화 복합재료의 잔류강도에 대한 통계적 특성 평가를 위한 모델을 제안하였으며, 이를 통한 예측결과는 복합재료의 두께와 관계없이 실험결과를 잘 묘사하였다.

• Composites Research
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• 제35권5호
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• pp.334-339
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• 2022

본 연구에서는 복합재료 제조 공정 과정 중 수지의 유동 저항성을 대변하는 인자인 투수 계수를 예측하는 알고리즘을 개발하였다. 단방향 연속 섬유 복합재료 내부에서 섬유와 수직인 방향 투수 계수의 정확한 예측을 위해 대표 체적 요소의 단면 형상을 고려하였다. 섬유의 유체 유동 저항성을 정량화하기 위한 인지로 섬유 간 간격이 사용되었고, 등가 길이는 섬유 배열에 따른 수지의 유로 변화를 나타내는 인자로 사용되었다. 전기-유압 유사성을 접목하여 투수 계수 예측 알고리즘을 개발하고 그 타당성을 확인하였다. 알고리즘은 Matlab과 Python으로 구성되고, 타당성 검증을 위해 FLUENT를 통해 예측된 투수 계수와 비교하였다. 알고리즘과 수치 해석을 통해 얻은 투수 계수가 거의 일치함을 확인하여 알고리즘을 검증하였으며, 소요 시간은 수치 해석 대비 약 1/450로 감소하였다.

• 비파괴검사학회지
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• 제13권1호
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• pp.15-20
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• 1993

This study describes ultrasonic reflection at a water/fiber reinforced polymer composite/water interface. Theoretical predictions of reflected beam amplitudes are also presented. Four different polymer composite laminates are investigated : T300/5208 graphite/epoxy $[0]_{31T},\;[45/90/-45/0]_{3S},\;[45/-45]_{2S}$, and S-2 glass/epoxy $[0/90]_{4S}$. The analytical leaky plate wave dispersion curves for the unidirectional laminate and other three laminates can be obtained by searching for the minimum magnitude of the reflection coefficient.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2001년도 춘계학술발표대회 논문집
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• pp.228-233
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• 2001

Satellite system experiences severe mechanical loads during the launch period. Therefore, positive margin of safety of the satellite system must be demonstrated for every possible mechanical loading condition during the launch period. This paper presents modal and stress analysis result due to quasi-static loads for the satellite antenna system. The failure tendency for the sandwich construction of the satellite antenna system has been studied with various lamination angles of unidirectional prepreg.

• 한국안전학회지
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• 제13권4호
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• pp.41-48
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• 1998

In this paper, an investigation was performed on the dynamic interlaminar fracture toughness of CFRP(carbon fiber reinforcement plastics) composite laminates. Composite laminates used in this experimentation are CF/EPOXY and CF/PEEK laminated plates. In the experiments, Split Hopkinson's Bar(SHPE) test was applied to dynamic and notched flexure test. The mode Ⅱ fracture toughness of each unidirectional CFRP was estimated by the analyzed deflection of the specimen and J-integral with the measured impulsive load and reactions at the supported points. As an experimental result, the vibration amplitude of CF/PEEK laminates appear more than that of CF/EPOXY laminates for the J-integral and displacement velocity at a measuring point. Also, it is thought that the dynamic fracture toughness of two kind specimens(CFRP/EPOXY and CF/PEEK) with the in crease of displacement velocity becomes a little greater at a measuring point within the range of measurement.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2012년도 추계학술대회 논문집
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• pp.110-114
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• 2012

We studied on the nondestructive evaluation of the elastic wave signal of SiC ceramics and SiC/SiC composite ceramics under monotonic tensile loading. The elastic wave signal of cross and unidirectional SiC/SiC composite ceramics were obtained by pencil lead method and bending test. It was applied for the time-frequency method which used by the discrete wavelet analysis algorithm. The time-frequency analysis provides time variation of each frequency component involved in a waveform, which makes it possible to evaluate the contribution of SiC fiber frequency. The results were compared with the characteristic of frequency group from SiC slurry and fiber. Based on the results, if it is possible to shift up and design as a higher frequency group, we will can make the superior material better than those of exiting SiC/SiC composites.

• 한국항공운항학회지
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• 제17권4호
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• pp.42-47
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• 2009

Recently, the wide range of the composite materials is used for the making airplanes, trains and automobiles body for the lightweight. Despite having complex structures, composite materials usually have well defined mechanical characteristics. However, composite materials are difficult to understand the fracture mechanism clearly by simple mechanical test. Nondestructive evaluation (NDE) combined with mechanical testing can play a more important role and especially Acoustic Emission Testing (AET) would become known to be a useful tool to assess damage and fracture behavior of composites. In this study The experiment was performed to acquire the acoustic emission signal during tensile test using unidirectional CFRP specimen and the data was analyzed the acoustic emission parameters with the waveform.

• 한국안전학회지
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• 제24권2호
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• pp.23-29
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• 2009

The hybrid composite materials are recently used in many field as an advanced material due to their high resistance to fracture. However, hybrid composite materials have several problems, especially delamination, compared with homogeneous materials such as an aluminum alloy, etc. In this study, we carried out the tensile test to study the tension failure appearances and tensile ultimate strength of CFRP/Al/CFRP hybrid composite materials. The CFRP material used in the experiment is a commercial material known as CU175NS in unidirectional carbon prepreg. Also Al/CFRP/Al hybrid composites with three kind length of a single edge crack were investigated for the relationship between an aluminium volume fraction and a crack length. The crack length was measured by a traveling microscope under a universal dynamic tester. Futhermore the stress intensity factor behavior was examined according to a volume fraction and an initial crack length ratio to a width.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집A
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• pp.401-406
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• 2001

When propagating the thickness direction of composite laminates ultrasound waves interacts strongly with the orientation and sequence of the plies in a layup. Also the layup orientation greatly influences its properties in a composite laminate. If one ply of the layup orientation is misaligned, it could result in the part being rejected and discarded. Now, most researchers cut a small coupon from the waste edge and use a microscope to optically verify the ply sequences on important parts. Those may add a substantial cost to the product since the test is both labor hard and performed after the part is cured. A nondestructive technique would be very beneficial, which could be used to test the part after curing and require less time than the optical test. Therefore we have developed, reduced, and implemented a novel ply-by-ply vector decomposition model for composite lam mates fabricated from unidirectional plies. This model decomposes the transmission of a linearly polarized ultrasound wave into orthogonal components through each ply of a laminate. It is found that a high probability shows between the model and tests developed in characterizing cured layups of the laminates.