• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 추계학술대회논문집
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• pp.527-533
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• 2000

It is investigated that the characteristics of rotating cantilevered composite beam with a breathing crack. In the present study, the crack is modeled as a breathing crack which opens and closes with the motion of the unidirectional graphite-fiber reinforced polyimide beam. For the finite element analysis, the cracked element is modelled by the local flexibility matrix calculated on the basis of fracture mechanics using Castiligano theorem. Rotating beam is considered only transverse bending motion so that the element includes two degrees of freedom per node such as the transverse deflection and slope. The time history and frequency response function of the beam with a breathing crack are studied by Newmark direct time integration method and FFT(Fast Fourier Transform)simulation. Effects of various parameters such as the crack depths, crack locations, ply angles, volume fraction ratios, and rotating speeds of the beam are also studied. Numerical results indicate that it is more reliable to be modelled as a breathing crack than an open crack.

• 항공우주시스템공학회지
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• 제15권6호
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• pp.19-25
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• 2021

This paper presents a method that uses the stress failure criteria to predict the tensile failure strength of open-hole laminates with stress concentrations. The composite material used in this study corresponds to a 177 ℃ cured, carbon/epoxy unidirectional tape prepreg. The results obtained by testing ten different laminates were compared and analyzed to verify the tensile strength of the open-hole laminates predicted using the proposed stress failure criteria. The findings of this study confirm that the tensile strength predictions performed using the proposed method are generally accurate, except in cases involving highly soft laminates (10% of 0° ply).

• Composites Research
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• 제17권4호
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• pp.7-17
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• 2004

본 연구에서 복합재의 압축 강도에 대한 두께 효과가 $[0_4]_{ns},{\;}[45/0/-45/90]_{ns},{\;}[45_n/0_n/-45_n/90_n]_s$ (n=2 to 8) 등의 적층 방법을 이용하여 체계적인 실험을 통해 조사되었다. 여기서 섬유 체적비, 기공률, 섬유 굴곡도, 층간 응력 등, 적층 두께 증가에 따른 압축 강도에 영향을 주는 파라미터들이 실험과 이론적으로 연구되었다. 또한 엇교차 대칭 복합재판의 파괴강도에 대한 적층 순서 효과도 조사되었다. 이를 위해 2종류의 다른 스케일링 효과를 갖는 (1) 폰라이-레벨 기법인 $[45_n/0_n/-45_n/90_n]_s$과 (2) 서브라미네이트-레벨 기법인 $[45_n/0_n/-45_n/90_n]_s$가 적용되었다. 일 방향 적층 시편 $[0_4]_{ns}$과 플라이-레벨인 $[45_n/0_n/-45_n/90_n]_s$에는 분명한 두께효과를 나타내었다. 그리고 섬유 굴곡도와 기공률의 두께효과에 기여하는 주요 파라미터 들임이 확인되었다. 그러나 서브라미네이트-레벨인 $[45/0/-45/90]_{ns}$의 압축강도는 시편 두께의 변화에도 불구하고 별 영향을 나타내지 않았으면, 서브라미네이트- 레벨 시편에서 구한 강토가 플라이-레벨 시편에서 구한 강도보다 약간 높았다. 이 같은 효과에 대한 이유는 섬유 굴곡도, 기공률, 자유단 효과 및 $0^{\circ}$층과 비 $0^{\circ}$층 사이의 응력 재 분포에 의한 영향인 것으로 보인다. 측정된 파괴강도는 예측 값과 비교되었다.

• 대한조선학회지
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• 제25권4호
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• pp.58-68
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• 1988

$[0^{\circ}]_{8T},\;[90^{\circ}]_{8T},\;[+45^{\circ}]_{8T}$의 단축방향과 $[{\pm}15^{\circ}]_{2S},\;[{\pm}30^{\circ}]_{2S},\;[{\pm}45^{\circ}]2_{2S},\;[{\pm}60^{\circ}]_{2S},\;[{\pm}75^{\circ}]_{2S}$ Angle Ply 그리고 $0^{\circ},\;{\pm}45^{\circ},\;90^{\circ}$로 조합된 다방향 복합적층판의 기계적 성질에 대하여 스트레인 게이지를 이용하여 측정 수록하였다. 메트릭스의 특성이 잘 나타나는 $[10^{\circ}]$ Off-Axis와 $[{\pm}45^{\circ}]$ Angle Ply를 이용하여 전단탄성계수를 측정하였다. 복합재료 인장시험시 발생하는 Acoustic Emission 특성과 파괴거동을 비교 검토하고, 이것을 통하여 Acoustic Emission법의 유용성과 파손 메카니즘을 규명하고자 하였다.

• Structural Engineering and Mechanics
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• 제2권4호
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• pp.359-367
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• 1994

The stability behaviour of symmetrically laminated rectangular composite plates with loaded ends clamped and unloaded edges simply-supported, and subjected to uniform in-plane compression is investigated. A numerical and experimental investigation is presented in this contribution. The stacking sequence of the laminated glass/epoxy composite plates is symmetric about the middle surface and consists of 8-ply [0, 90, +45, -45]s lamination. Numerical predictions were obtained through the use of the finite element method. The above plates were modelled with 8-noded isoparametric layered shell elements. The effect of the input parameters such as the degree and forms of prescribed initial imperfection and the incremental step size required for incremental loading, on the convergence of the solution is thoroughly examined. Experimental results are presented for 10 test panels. All test panels were made from glass/epoxy unidirectional prepregs and have aspect ratio of 5.088. The laminate thicknesses were found to vary from 1.054 mm to 1.066 mm. Comparison of experimental data with predicted results show good correlation and give confidence in the finite element model.

• 대한기계학회논문집A
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• 제26권3호
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• pp.553-559
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• 2002

Carbon-fiber which has very small radial dimension makes us difficult to measure it's properties. So in this paper, we suggest a simple method to measure the thermal conductivity of a carbon-fiber's and carbon-fiber-reinforced-plastics(CFRP) laminates. The thermal conductivity of CFRP laminates was measured experimentally at the same time analytically. The experimental model is based on the one-dimensional analysis of fin sample because CFRP laminates has a thin geometric configuration. The analytical model to measure the thermal conductivity of carbon-fiber is expressed by use of mean-field model which is based on Eshelby's elliptical inclusion problem. Therefore the thermal conductivity of angle-ply laminates can be computed by use of effective longitudinal and transverse thermal conductivities of unidirectional composite of the constituents.

• 비파괴검사학회지
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• 제35권3호
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• pp.206-214
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• 2015

In this study, low-velocity impact damage (LVID) in glass fiber reinforced plastic (GFRP) was investigated using pulse thermography (PT) and lock-in thermography (LIT) techniques. The main objective of this study was to evaluate the detection performance of each technique for LVID in GFRP. Unidirectional and cross-ply GFRPs were prepared with four energy levels using a drop weight impact machine and they were inspected from the impact side, which may be common in actual service conditions. When the impacted side was used for both inspection and thermal loading, results showed that the suggested techniques were able to identify the LVID which is barely visible to the naked eye. However, they also include limitations that depend on the GFRP thickness at the location of the delamination produced by the lowest impact energy of five joule.

• 한국안전학회지
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• 제27권6호
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• pp.20-25
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• 2012

Currently, the most important purpose in designing automobile is environment-friendly and safety performance aspect. CFRP(Carbon Fiber Reinforced Plastics) of the advanced composite materials as structure materials for vehicles, has a wide application in lightweight structural materials of air planes, ships and automobiles because of high strength and stiffness. In this study, experimental investigations are carried out for CFRP single and double hat shaped section member in order to study the effect of various stacking condition. They were cured by heating to the appropriate curing temperature($130^{\circ}C$) by means of a heater at the vacuum bag of the autoclave. The stacking conditions were selected to investigate the effect of the interface numbers. The CFRP single and double hat shaped section members which manufactured from unidirectional prepreg sheets were made of 8ply. The static collapse tests performed and the collapse mode and energy absorption capability were analyzed according to interface number.

• Advances in aircraft and spacecraft science
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• 제10권4호
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• pp.347-368
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• 2023

In the first part of this study, a numerical simulation model was developed using the mechanical APDL software to validate the results of the 3D-elastisity theory on the laminated sandwich plate developed by Panago. The numerical simulation model showed a good agreement to the results of Pagano's theory in terms of deflection, normal stresses, and shear stresses. In the second part of this study, the developed numerical simulation model was used to define different plates dimensions and fibers layup orientations to examine the load response in terms of deflection and stresses. Further analysis was implemented on the natural frequencies of laminated xxx plates of the plates. The layup configurations include Unidirectional (UD), Cross-Ply (CP), Quasi-Isotropic (QI), the linear bio-inspired known as Linear-Helicoidal (LH), and the nonlinear bio-inspired known as Fibonacci-Helicoidal (FH). The following numerical simulation model can be used for the design and study of novel, sophisticated bio-inspired composite structures in a variety of configurations subjected to sinusoidal or constant loads.

• 대한기계학회논문집A
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• 제41권10호
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• pp.983-989
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• 2017

본 논문에서는 첨단복합재의 볼트단일접합 베어링강도에 대한 시험적 평가 결과를 수록하였다. 볼트단일접합 시험은 stabilized 접합과 unstabilized 접합에 대하여 수행하였다. Stabilized 접합은 접합부 면외회전을 제한하는 접합이다. Unstabilized 접합은 면외변위를 제한하지 않는 접합이다. 볼트 단일접합에서 적층판의 베어링강도 값은 적층판 내 적층각 $0^{\circ}$, $+45^{\circ}$, $-45^{\circ}$ 및 $90^{\circ}$ 비율에 영향이 없음을 보여준다. 볼트접합부 면외거동의 영향으로 unstabilized 볼트 단일접합 베어링 강도값이 stabilized 볼트 단일접합 베어링 강도값 보다 작음을 보여주고 있다. 본 논문에 사용된 복합재료는 $177^{\circ}C(350^{\circ}F)$에서 경화되는 Carbon/Epoxy UD Tape 프리프레그이다. 표준각 $0^{\circ}$, $+45^{\circ}$, $-45^{\circ}$ 및 $90^{\circ}$ 층으로 적층된 8종류의 적층판에서 총 112개 볼트단일접합 시험시편을 구성하였다. Stabilized 접합과 unstabilized 접합의 시험방법은 ASTM-D-5961M 규정을 사용하였다.