• Steel and Composite Structures
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• 제18권1호
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• pp.135-148
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• 2015

The cutout hole locating at the place of rib-to-diaphragm welded connection is adopted to minimize the restraint, which is caused by the floor-beam web to rib rotation at the support due to the unsymmetrical loads in orthotropic deck. In practice, an inevitable problem is that there is a large number of welding joint's cracks formed at the edge of cutout hole. In this study, a comparative experiment is carried out with two types of cutout hole, the circular arc transition and the vertical transition. The fatigue life estimation of specimens is investigated with the application of the structural hot spot stress approach by finite element analyses. The results are compared with the ones of the fatigue tests which are carried out on these full-scale specimens. Factors affecting the stress range are also studied.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2005년도 춘계 학술발표회 논문집
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• pp.592-600
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• 2005

Ship have cutout inner bottom and girder and floor etc. Ship's structure is used much, and structure strength must be situated, but establish new concept when high stress interacts sometimes fatally the area. There is no big problem usually by aim of weight reduction, a person and change of freight, piping etc.. Because cutout's existence grow up in this place, and elastic buckling strength by load causes large effect in ultimate strength. Therefore, stiffened perforated plate considering buckling strength and ultimate strength is one of important design criteria which must examine when decide structural concept at initial design. Therefore, md, reasonable buckling strength about stiffened perforated plate need to ultimate strength limited design . Calculated ultimate strength varied several web height and cutout's dimension, and thickness in this investigated data. Used program(ANSYS) applied F.E.A code based on finite element method

• Structural Engineering and Mechanics
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• 제52권4호
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• pp.815-827
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• 2014

Buckling optimization of laminated composite plates is significant as they fail because of buckling under in-plane compressive loading. The plate is usually modeled without cutout so that the buckling strength is found analytically using classical laminate plate theory (CLPT). However in real world applications, the composite plates are modeled with cutouts for getting them assembled and to offer the provisions like windows, doors and control system. Finite element analysis (FEA) is used to analyze the buckling strength of the plate with cutouts and it leads to high computational cost when the plate is optimized. In this article, a genetic algorithm based optimization technique is used to optimize the composite plate with cutout. The computational time is highly reduced by replacing FEA with artificial neural network (ANN). The effectiveness of the proposed method is explored with two numerical examples.

• 소음진동
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• 제8권3호
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• pp.467-476
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• 1998

The free vibration analysis and design optimization of the rotating composite cylindrical shells with a rectangular cutout are investigated by theoretical method. The Love's thin shell theory is used to derive the frequency equation. The theoretical results are obtained by application of the energy method employing the Rayleigh-Ritz procedure. The used circumferential vibration modes are trigonometric functions, the axial modes are the beam modal functions chosen to satisfy the prescribed boundary conditions. To check the validity, the theoretical results are compared with experimental, FEM and other theoretical results.

• Steel and Composite Structures
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• 제29권5호
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• pp.681-688
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• 2018

In this paper, buckling load of edge stiffened composite plates is assessed. The effect of stiffener edge size, circular hole, and the fiber orientation angle on buckling behavior of composite plates under uni-axial compressive load is investigated. This paper includes two parts as experimental and numerical studies. L-shape composite plates are manufactured in three different layups. Then the buckling loads are experimentally determined. Subsequently, by using the numerical simulation, the size variation effects of stiffener edge and circular cutout on the plate buckling loads are analyzed in five different layups. The results show that cutout size, stiffener edge height and fiber orientation angle have important effects on buckling load. In addition, there is an optimum height for stiffener edge during different conditions.

• 한국방재학회 논문집
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• 제9권1호
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• pp.41-47
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• 2009

강바닥판의 횡리브 복부판에서는 전단력과 비틀림 모멘트가 작용하는 동시에 종리브의 비틀림으로 인한 면내외 변형이 작용하기 때문에 교차부와 컷아웃부에 응력집중현상이 발생한다. 본 연구는 피로균열 발생사례가 가장 높은 교차부와 컷아웃부에서의 응력집중현상 완화를 통하여 피로성능을 향상시킬 수 있는 구조상세를 개발하기 위하여 수행되었다. 다이아프램의 설치는 교차부와 컷아웃부에서의 응력집중현상 완화효과에 유리한 구조상세이다. 다이아프램의 위치에 대한 응력집중의 양상을 분석하기 위해서 다이아프램 위치를 횡리브 복부판과 일치된 곳으로부터 교축방향으로 이동시켜 가며 그 응답을 수치적으로 분석하였다. 또한 컷아웃폭을 대상으로 매개변수해석을 수행하여 최대응력 감소효과를 분석하였다. 그 결과 다이아프램은 횡리브 복부판과 횡리브 축 방향으로 일치되도록 설치하는 것이 응력집중현상을 완화시켜 구조성능 개선에 유리한 구조상세임을 알 수 있었다. 그러나 어떤 경우에도 다이아프램을 설치하지 않은 경우보다는 설치한 경우가 피로성능에 유리함을 알 수 있었다. 컷아웃폭은 바닥강판으로부터 종리브 바닥판면까지의 거리($y_{gotal}$)에 대한 바닥강판으로부터 컷아웃부의 종리브와 횡리브 교차점까지의 거리($y_i$)의 비($y_i/y_{total}$) 0.85가 되도록 컷아웃폭을 설정하는 경우가 구조성능 개선에 유리한 구조상세임을 알 수 있었다.

• 응용통계연구
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• 제36권2호
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• pp.101-114
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• 2023

데이터 증강 기법은 학습용 데이터셋을 다양한 관점에서 볼 수 있게 해주어 모형의 과적합 문제를 해결하는데 효과적으로 사용되고 있다. 이미지 데이터 증강기법으로 회전, 잘라내기, 좌우대칭, 상하대칭등의 증강 기법 외에도 occlusion 기반 데이터 증강 방법인 Cutmix, Cutout 등이 제안되었다. 음성 데이터에 기반한 모형들에 있어서도, 1D 음성 신호를 2D 스펙트로그램으로 변환한 후, occlusion 기반 데이터 기반 증강기법의 사용이 가능하다. 특히, SpecAugment는 음성 스펙트로그램을 위해 제안된 occlusion 기반 증강 기법이다. 본 연구에서는 위조 음성 탐지 문제에 있어서 사용될 수 있는 데이터 증강기법에 대해 비교 연구해보고자 한다. Fake audio를 탐지하기 위해 개최된 ASVspoof2017과 ASVspoof2019 데이터를 사용하여 음성을 2D 스펙트로그램으로 변경시켜 occlusion 기반 데이터 증강 방식인 Cutout, Cutmix, SpecAugment를 적용한 데이터셋을 훈련 데이터로 하여 CNN 모형을 경량화시킨 LCNN 모형을 훈련시켰다. Cutout, Cutmix, SpecAugment 세 증강 기법 모두 대체적으로 모형의 성능을 향상시켰으나 방법에 따라 오히려 성능을 저하시키거나 성능에 변화가 없을 수도 있었다. ASVspoof2017 에서는 Cutmix, ASVspoof2019 LA 에서는 Mixup, ASVspoof2019 PA 에서는 SpecAugment 가 가장 좋은 성능을 보였다. 또, SpecAugment는 mask의 개수를 늘리는 것이 성능 향상에 도움이 된다. 결론적으로, 상황과 데이터에 따라 적합한 augmentation 기법이 다른 것으로 파악된다.

• Steel and Composite Structures
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• 제36권2호
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• pp.143-161
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• 2020

In nanosized structures as the surface area to the bulk volume ratio increases the classical continuum mechanics approaches fails to investigate the mechanical behavior of such structures. In perforated nanobeam structures, more decrease in the bulk volume is obtained due to perforation process thus nonclassical continuum approaches should be employed for reliable investigation of the mechanical behavior these structures. This article introduces an analytical methodology to investigate the size dependent, surface energy, and perforation impacts on the nonclassical bending behavior of regularly squared cutout nanobeam structures for the first time. To do this, geometrical model for both bulk and surface characteristics is developed for regularly squared perforated nanobeams. Based on the proposed geometrical model, the nonclassical Gurtin-Murdoch surface elasticity model is adopted and modified to incorporate the surface energy effects in perforated nanobeams. To investigate the effect of shear deformation associated with cutout process, both Euler-Bernoulli and Timoshenko beams theories are developed. Mathematical model for perforated nanobeam structure including surface energy effects are derived in comprehensive procedure and nonclassical boundary conditions are presented. Closed forms for the nonclassical bending and rotational displacements are derived for both theories considering all classical and nonclassical kinematics and kinetics boundary conditions. Additionally, both uniformly distributed and concentrated loads are considered. The developed methodology is verified and compared with the available results and an excellent agreement is noticed. Both classical and nonclassical bending profiles for both thin and thick perforated nanobeams are investigated. Numerical results are obtained to illustrate effects of beam filling ratio, the number of hole rows through the cross section, surface material characteristics, beam slenderness ratio as well as the boundary and loading conditions on the non-classical bending behavior of perforated nanobeams in the presence of surface effects. It is found that, the surface residual stress has more significant effect on the bending deflection compared with the corresponding effect of the surface elasticity, Es. The obtained results are supportive for the design, analysis and manufacturing of perforated nanobeams.

• 한국의학물리학회지:의학물리
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• 제13권1호
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• pp.27-31
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• 2002

6MeV 전자선의 output 인자를 결정하기 위해 간편하게 output 인자를 예측하는 수단인 1D(Dimension) 방법을 이용하였으며 그리고 1D 방법으로 결정된 output 인자를 개별적 beam cutout 하에서 직접 측정한 output 인자와 비교하여 1D 방법의 정확성을 분석하였다. 1D 방법은 정방형 field의 한 변과 항상 동일한 한 변을 갖는 사각형 field의 output 인자로서 규정되며, 임의의 사각형 field (X,Y)의 output은 1D output 인자의 곱으로 주어진다. 6MeV 전자선의 대단히 큰 정방형 field의 output은 1D 방법을 사용하면 실제보다 높은 값을 나타내지만 교정인자 CF=C.[(X-10)(Y-10)/$\mid$(X-10)(Y-10)$\mid^{1/2}]$를 적용하면 개별적 cutout하에 직접 측정된 output 인자와 잘 일치하였으며 그 오차 범위는 1% 이내였다.

• Structural Engineering and Mechanics
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• 제61권2호
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• pp.255-266
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• 2017

In this study, self-supporting roofing elements especially convenient for large-span structures such as stadium, airport terminal, mall, coliseum, etc. were examined with respect to critical buckling load. These elements were assumed as laminated composite plates and, variation of free-edge forms, cutout types and lamination configurations were used as design parameters. Based on the architectural feature and structural requirements, the effects of curvilinear free-edge form on critical buckling load were focused on in this research. Within this scope, 14 types of lamination configuration were specified according to various orientation angle, number and thickness of plies with a constant value of total plate thickness. Besides that, 6 different types of cutout and 3 different free-edge forms were determined. By combining all these parameters 294 different critical buckling load analyses were performed by using ANSYS Mechanical software based on finite element method. Effects of those parameters on critical buckling load were evaluated referring to the obtained results. According to the results presented here, it may be concluded that lamination conditions have more significant influence on the critical buckling load values than the other parameters. On the other hand, it is perceived that curvilinear free-edge forms explicitly undergo changings depending on lamination conditions. For future work, existence of delamination might be considered and progression of the defect could be investigated by using non-linear analysis.