• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2002년도 봄 학술발표회 논문집
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• pp.489-496
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• 2002

The lateral buckling of a laminated composite beam is studied. A general analytical model applicable to the lateral buckling of a composite beam subjected to various types of loadings is derived. This model is based on the classical lamination theory, and accounts for the material coupling for arbitrary laminate stacking sequence configuration and various boundary conditions. The effects of the location of applied loading on the buckling capacity are also included in the analysis. A displace-based one-dimensional finite element model is developed to predict critical loads and corresponding buckling modes for a thin-walled composite beam with arbitrary boundary conditions. Numerical results are obtained for thin-walled composites under central point load, uniformly distributed load, and pure bending with angle-ply and laminates. The effects of fiber orientation location of applied load, and types of loads on the critical buckling loads are parametrically studied.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.867-869
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• 2004

A smart blade conception has been proposed by the authors. With stretching-twisting coupling effect, the blade is twisted by centrifugal load or ambient temperature change. In this paper, the blades, made by three kinds of anti-symmetric laminates, are investigated by rotational tests. The results show the angle of smart blade tips increases in proportion to the 2nd power of a rotating speed and is well in agreement with the numerical results by FEM.

• Structural Engineering and Mechanics
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• 제25권6호
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• pp.637-652
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• 2007

This paper presents stacking sequence optimization of laminated angle-ply cylindrical panel based on natural frequency. Finite element method (FEM) is used to obtain the vibration characteristic of an anisotropic panel using the first order shear deformation theory(FSDT) and genetic algorithm (GA) is used to obtain the optimal stacking sequence of the layers. Cylindrical panel has finite length and arbitrary boundary conditions. The thicknesses of the layers are assumed constant and their angles are specified as design variables. The effect of the number of plies and boundary conditions in the fitness function is considered. Numerical examples are presented for four, six and eight layered anisotropic cylindrical panels.

• Structural Engineering and Mechanics
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• 제77권2호
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• pp.245-259
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• 2021

In this research, the influence of the laminate stacking sequence on thermal stress distribution in symmetric composite plates with a quasi-square cutout subjected to uniform heat flux is examined analytically using the complex variable technique. The analytical solution is obtained based on the thermo-elastic theory and the Lekhnitskii's method. Furthermore, by employing a suitable mapping function, the solution of symmetric laminates containing a circular cutout is extended to the quasi-square cutout. The effect of important parameters including the stacking sequence of laminates, the angular position, the bluntness, the aspect ratio of cutout, the flux angle and the composite material are examined on the thermal stress distribution. It is found out that the circular shape for cutout may not necessarily be the optimum geometry for all stacking sequences. The finite element analysis results are used to validate the analytical solution.

• Structural Engineering and Mechanics
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• 제88권3호
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• pp.201-208
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• 2023

In this work, the effect of the correction fibers direction on the efficiency of repairing damaged composite plates was highlighted. The composite plates studied in this work consist of eight layers of graphite/epoxy, while the patch used in this repair consists of four layers of the same type. The results obtained in this work, whether with regard to the experimental or analytical side, showed that the fibers orientation affects the repair efficiency, so the closer the angle of fibers inclination is to the tensile strength direction, the performance of the composite material is ideal. Hence, we conclude that the composite materials with longitudinal fibers (Parallel to tensile strength) is the most powerful and efficient material in performance.

• Journal of Mechanical Science and Technology
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• 제18권1호
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• pp.65-73
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• 2004

Composites are a material class for which nondestructive material property characterization is as important as flaw detection. Laminates of fiber reinforced composites often possess strong in-plane elastic anisotropy attributable to the specific fiber orientation and layup sequence when waves are propagating in the thickness direction of composite laminates. So the layup orientation greatly influences its properties in a composite laminate. It could result in the part being .ejected and discarded if the layup orientation of a ply is misaligned. A nondestructive technique would be very beneficial, which could be used to test the part after curing and requires less time than the optical test. Therefore a ply-by-ply vector decomposition model has been developed, simplified, and implemented for composite laminates fabricated from unidirectional plies. This model decomposes the transmission of a linearly polarized ultrasound wave into orthogonal components through each ply of a laminate. Also in order to develop these methods into practical inspection tools, motorized system have been developed for different measurement modalities for acquiring ultrasonic signals as a function of in-plane angle. It is found that high probability shows between the model and tests developed in characterizing cured layups of the laminates.

• 한국진공학회지
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• 제16권2호
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• pp.79-90
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• 2007

저에너지 초고속 표면 처기 이온원, 4개의 마그네트론 스퍼터 캐소드가 부착된 300 mm 폭 다목적 연성 기판 제작을 위한 부피 800 L 용량의 진공 웹코터 원형 (prototype) 장비를 설계 제작하였고, 무접착제 2층 연성 동박 적층 필림을 제작하여 성능을 평가하였다. 2 개의 터보 펌프 및 폴리콜드를 장착한 비코팅 부분인 상실부와 각각 1개씩의 터보 펌프를 사용한 표면 처리 및 코팅 부분인 하실부의 진공 배기 특성을 측정하였다. 패러데이 컵을 사용하여 대면적 이온원의 이온 전류 밀도 및 균일도를 측정하고, 스퍼터 캐소드의 자기장 분포 및 타겟 사용 효율을 조사하였다. 진공 웹코터의 성능 및 각 구성 요소의 특성 조사를 위하여 연성 기판으로는 폴리이미드 (Kapton-E) $38{\mu}m$을 사용하여 여러 가지 가스 이온에 대한표면 처리 조건에 따른 증류수의 접촉각 변화와 화학 성분의 변화를 x-선 분광학을 사용하여 조사하였다. 고밀도 2층 연성 동박 적층 필림 기판을 스퍼터-전기 도금법으로 제작하기 위하여 스퍼터 타겟으로는 Ni-Cr 및 Cu 금속을 사용하여, 각각의 증착율을 직류 전력의 변화 및 롤의 속도에 따라 조사하였고, 전기 도금으로 $9{mu}m$ 까지 동박 적층 필림을 제작한 후 접착력 및 내열성, 내화학성을 측정하여 소형 진공 웹 코터의 특성을 조사하였다.

• 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.

• Steel and Composite Structures
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• 제25권1호
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• pp.105-116
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• 2017

This paper presents the dynamic stability study of laminated composite plates with different force combinations and aspect ratios. Optimum non-diverging stacking is obtained for certain loading combination and aspect ratio. In addition, the stability force is maximized for a definite operating frequency. A dynamic version of the principle of virtual work for laminated composites is used to obtain force-frequency relation. Since dynamic stiffness governs the divergence or flutter, an efficient optimization method is necessary for the response functional and the relevant constraints. In this way, a model based on the ant colony optimization (ACO) algorithm is proposed to search for the proper stacking. The ACO algorithm is used since it treats with large number of dynamic stability parameters. Governing equations are formulated using classic laminate theory (CLT) and von-Karman plate technique. Load-frequency relations are explicitly obtained for fundamental and secondary flutter modes of simply supported composite plate with arbitrary aspect ratio, stacking and boundary load, which are used in optimization process. Obtained results are compared with the finite element method results for validity and accuracy convince. Results revealed that the optimum stacking with stable dynamic response and maximum critical load is in angle-ply mode with almost near-unidirectional fiber orientations for fundamental flutter mode. In addition, short plates behave better than long plates in combined axial-shear load case regarding stable oscillation. The interaction of uniaxial and shear forces intensifies the instability in long plates than short ones which needs low-angle layup orientations to provide required dynamic stiffness. However, a combination of angle-ply and cross-ply stacking with a near-square aspect ratio is appropriate for the composite plate regarding secondary flutter mode.

• 수산해양기술연구
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• 제21권1호
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• pp.75-81
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• 1985

직교이방향 이층 유리섬유 강화 Epoxy 수지를 사용하여 인장축에 대해 섬유방향이 0$^{\circ}$, 15$^{\circ}$, 25$^{\circ}$ 및 45$^{\circ}$인 시료로 인장시험 및 전기절연 강도시험을 통하여 얻은 결과는 다음과 같다. 1) 섬유방향이 인장축에 대해 0$^{\circ}$에서 45$^{\circ}$로 증가함에 따라 항복응력 및 파단응력은 감소하는 경향이고 특히 0$^{\circ}$와 15$^{\circ}$ 사이에서 급격한 변화율을 보인다. 2) 파단시 변화율은 인장방향에 대한 섬유방향이 45$^{\circ}$인 경우 최대치를 나타냈고 15$^{\circ}$~45$^{\circ}$ 범위에서 급격한 변화율을 보인다. 3)섬유의 방향이 동일할 경우 인장력을 많이 받은 시료일수록 최대절연강도 값은 낮아졌고 인장방향과 섬유방향의 교각이 증가할수록 최대절연강도 값을 나타내는 압축응력의 값은 낮은 점으로 이동하는 경향을 보였다. 4) 기계적 특성과 같이 섬유방향이 45$^{\circ}$인 경우의 시료가 가장 나쁜 전기적 절연강도 특성을 나타냈다.