• 한국정보과학회논문지:시스템및이론
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• 제29권12호
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• pp.680-686
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• 2002

딥 서브 마이크론 (DSM: deep-submicron) 설계에서는 버스에서 선들 간의 커플링 효과는 크로스톡 지연, 노이즈, 전력 소모와 같은 심각한 문제를 야기 시킨다. 버스 인코딩에 대한 대부분의 이전 연구들은 버스에서의 전력 소모를 최소화하거나 크로스톡 지연을 최소화하는데 초점을 맞추고 있지만 모두를 고려한 방법은 보이지 않는다. 이 논문에서, 우리는 버스에서의 전력 소모 최소화와 크로스톡 지연 방지를 동시에 고려한 새로운 버스 인코딩 알고리즘을 제안하였다. 우리는 이 문제를 공식화하여, 자체 천이와 상호 천이의 가중 합 문제를 풂으로써 해결하였다. 여러 벤치마크 설계를 이용한 실험으로부터 제안한 인코딩 방법을 이용할 경우, 크로스톡 지연을 완전히 제거할 뿐 아니라 이전의 방법들을 사용한 것 보다 최소 15% 이상 적은 전력을 소모하였음을 보았다.

• 조명전기설비학회논문지
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• 제12권4호
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• pp.128-135
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• 1998

돌극형 동기 릴럭턴스 전동기의 고속회전 영역에서, 철손의 영향은 무시할 수 없게 된다. 본 논문에서는 돌 극형 동기 릴럭턴스 전동기에 대하여 고정자 철손이 고정자 내의 둥가 와전류에 의해서 발생한다는 가정 하에서, 둥가 인덕턴스에 직렬로 등가 철손저항이 삽입된 모델을 이용하여 철손을 고려한 전압방정식을 유도하였다. 또, 동작 주파수의 증가에 따른 철손의 변동은 벡터제어계의 제어성능을 악화시키고,d 축과 q 축의 쇄교자속에 서로 간섭하여 벡터제어의 적용을 어렵게 한다. 따라서, d 축과 q 축을 비간섭화 하여 철손저항의 영향을 제거해서 비간섭 토크제어가 가능한 벡터제어법올 제안하였으며, 시뮬레이션올 통하여 이를 확인하였다.

• 한국가스학회지
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• 제7권2호
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• pp.42-47
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• 2003

화학공정산업에서 화재, 폭발, 독성물질 누출의 대형사고로 인한 막대한 인적 물적 손실을 효과적으로 방지하기 위하여 기계적 오류와 연계하여 사람의 행동을 동적으로 제어하는 것이 필요하다. 석유화학공단을 비롯한 에너지산업시설에서의 대형사고는 기계적인 결함과 더불어 사람의 행동과 관련되어 있음에도 불구하고, 대부분의 연구는 시스템의 위험을 감소시키기 위하여 안전장치의 결함과 인간의 행동에 대하여 서로 연계를 지우지 않고 독립적으로 연구를 수행하여 왔다 본 연구에서는 화학공정산업의 안전을 향상시키기 위한 방법을 제시하기 위하여 기계적 고장과 인적오류를 동시에 고려하여 인적오류를 제어하고, 중요한 수행영향인자에 대하여 고찰하였다.

• 한국강구조학회 논문집
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• 제20권4호
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• pp.505-517
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• 2008

휨지배 거동을 나타내는 세장한 이중강판합성벽의 비탄성 거동을 예측하기 위하여 비선형 수치해석 모델이 연구되었다. 수치해석의 편리를 위하여, 제안된 모델은 비교적 단순한 모델을 가지고 비탄성 거동을 근사적으로 예측할 수 있는 거시적 모델로 개발되었다. 휨지배 거동을 나타내는 벽체에 대해서는 다중평행요소 모델이 사용되었으며, 깊은 연결보의 전단거동을 위하여 X형 대각요소 모델이 사용되었다. 각 요소의 주기거동을 예측하기 위하여 콘크리트 및 강판 요소에 대한 간략화된 일축의 주기모델을 제안하였다. 제안된 해석모델은 1자형 및 T형 단일벽과 병렬벽에 적용하였으며, 그 결과는 기존의 실험결과와 비교되었다.

• Structural Engineering and Mechanics
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• 제3권1호
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• pp.91-103
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• 1995

An analysis to determine shear centers for anisotropic elastic thin-walled composite beams, cantilevered and loaded transversely at the free end is presented. The shear center is formulated based on familiar strength of material procedures analogous to those for isotropic beams. These procedures call for a balancing of torsional moments on the cross sectional surface and lead to a condition of zero resultant torsional couple. As a consequence, due the presence of anisotropic coupling, certain non-classical effects are manifested and are illustrated in two example problems. The most distinguishing result is that twisting may occur for composite beams even if shear forces are applied at the shear center. The derived shear center locations do not depend on any specific anisotropic bending theories per se, but only on the values of bending and shear stresses which such theories produce.

• Advances in aircraft and spacecraft science
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• 제4권3호
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• pp.219-235
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• 2017

The large container ships and fast patrol boats are complex marine structures. Therefore, their global mechanical behaviour has long been modeled mostly by refined beam theories. Important issues of cross section warping and bending-torsion coupling have been addressed by introducing special functions in these theories with inherent assumptions and thus compromising their robustness. The 3D solid Finite Element (FE) models, on the other hand, are accurate enough but pose high computational cost. In this work, different marine vessel structures have been analysed using the well-known Carrera Unified Formulation (CUF). According to CUF, the governing equations (and consequently the finite element arrays) are written in terms of fundamental nuclei that do not depend on the problem characteristics and the approximation order. Thus, refined models can be developed in an automatic manner. In the present work, a particular class of 1D CUF models that was initially devised for the analysis of aircraft structures has been employed for the analysis of marine structures. This class, which was called Component-Wise (CW), allows one to model complex 3D features, such as inclined hull walls, floors and girders in the form of components. Realistic ship geometries were used to demonstrate the efficacy of the CUF approach. With the same level of accuracy achieved, 1D CUF beam elements require far less number of Degrees of Freedom (DoFs) compared to a 3D solid FE solution.

• Nuclear Engineering and Technology
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• 제53권6호
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• pp.1893-1908
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• 2021

In light of the importance of helium production in influencing the behaviour of fast reactor fuels, in this work we present a burn-up module with the objective to calculate the production of helium in both in-pile and out-of-pile conditions tracking the evolution of 23 alpha-decaying actinides. This burn-up module relies on average microscopic cross-section look-up tables generated via SERPENT high-fidelity calculations and involves the solution of the system of Bateman equations for the selected set of actinide nuclides. The results of the burn-up module are verified in terms of evolution of actinide and helium concentrations by comparing them with the high-fidelity ones from SERPENT, considering two representative test cases of (U,Pu)O₂ fuel in fast reactor conditions. In addition, a code-to-code comparison is made with the independent state-of-the-art module TUBRNP (implemented in the TRANSURANUS fuel performance code) for the same test cases. The herein presented burn-up module is available in the SCIANTIX code, designed for coupling with fuel performance codes.

• Steel and Composite Structures
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• 제39권2호
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• pp.149-158
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• 2021

In this research paper, the free vibrational response of laminated composite plates is investigated using a non-polynomial refined shear deformation theory (NP-RSDT). The most interesting feature of this theory is the parabolic distribution of transverse shear deformations while ensuring the conditions of nullity of shear stresses at the free surfaces of the plate without requiring the Shear correction factor "Ks". A fourth-nodded isoparametric element with four degrees of freedom per node is employed for laminated composite plates. The numerical analysis of simply supported square anti-symmetric cross-ply and angle-ply laminated plate is carried out using a special discretization based on four-node finite element method which four degrees of freedom per node. Several numerical results are presented to show the effect of the coupling parameters of the plate such as the modulus ratios, the thickness ratio and the plate layers number on adimensional eigen frequencies. All numerical results presented using the current finite element method (FEM) is presented in 3D curve form.

• Elastomers and Composites
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• 제54권3호
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• pp.220-224
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• 2019

Herein, three polymer compounds were manufactured using three polymer combination methods, ethylene-vinyl acetate/ethylene-propylene-diene-copolymer (EPDM), ethylene-vinyl acetate (EVA)/polyethylene-A (PE-A; density: 0.870), and ethylene-vinyl acetate (EVA)/polyethylene-B (PE-B; density: 0.885), for making cable sheath for use in the shipping industry. In this study, EVA, EPDM, PE-A, and PE-B were used as matrix polymers, and EVA-grafted maleic anhydride was used as a coupling agent for compounding with various compounds such as a fire retardant, cross-linking agent, filler, and other additives, besides the plasticizer. ${\Delta}T$, Mooney viscosity, and tensile strength increased in order of EPDM < PE-A < PE-B, the probable reason is due to the different crosslinking effect. The three compounds showed similar results for fire resistance and aging resistance after compounding process, but they showed excellent cold resistance owing to the non-polarity of the polymers and sufficient plasticizer content.

• Steel and Composite Structures
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• 제39권5호
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• pp.543-564
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• 2021

In this study free vibration analysis of a cracked Goland composite wing is investigated. The wing is modelled as a cantilevered beam based on Euler- Bernoulli equations. Also, composite material is modelled based on lamina fiber-reinforced. Edge crack is modelled by additional boundary conditions and local flexibility matrix in crack location, Castigliano's theorem and energy release rate formulation. Governing differential equations are extracted by Hamilton's principle. Using the separation of variables method, general solution in the normalized form for bending and torsion deflection is achieved then expressions for the cross-sectional rotation, the bending moment, the shear force and the torsional moment for the cantilevered beam are obtained. The cracked beam is modelled by separation of beam into two interconnected intact beams. Free vibration analysis of the beam is performed by applying boundary conditions at the fixed end, the free end, continuity conditions in the crack location of the beam and dynamic stiffness matrix determinant. Also, the effects of various parameters such as length and location of crack and fiber angle on natural frequencies and mode shapes are studied. Modal analysis results illustrate that natural frequencies and mode shapes are affected by depth and location of edge crack and coupling parameter.