• 한국초전도ㆍ저온공학회논문지
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• 제9권2호
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• pp.7-10
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• 2007

Persistent mode HTS pancake coil has been fabricated using a coated conductor by a "wind-and-flip" method. A coated conductor with the length of 1.2 meters was divided at the center along the length. The sliced coated conductor was wound on a pair of bobbins with a diameter of around 4 cm and two pancake coils connected superconductively without a resistive joint were prepared. By flipping one of the pancake coils, the magnetic field generated by each coil is to be aligned to the same direction and generate meaningful magnetic field while the magnetic fields of two spit coils are canceled without flipping. Permanent current was induced by flowing current to the coil immersed in liquid nitrogen pool using a power supply. A magnetic field of 48.8 Gauss was generated when 20 A of current was flowing in the pancake coils. The "Wind and flip" method can be applied for the fabrication of a long solenoid magnet by winding a sliced coated conductor on a cylindrical bobbin. It is also introduced that the construction of multiple sets of pancake (or solenoid) coils is possible by a "wind-and-flip" method using a wide coated conductor.

• 한국초전도학회:학술대회논문집
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• 한국초전도학회 2006년도 High Temperature Superconductivity Vol.XVI
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• pp.87-87
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• 2006

• 한국초전도학회:학술대회논문집
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• 한국초전도학회 2009년도 Korea Superconductivity Society Meeting 2009
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• pp.120-120
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• 2009

• 한국초전도ㆍ저온공학회논문지
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• 제15권4호
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• pp.44-47
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• 2013

We had proposed a winding method so called "Wind-and-Flip", which enables a persistent current operation of an HTS pancake coil without any electrical joint. In order to improve the magnetic field drift characteristics, a prototype HTS coil with the technique was fabricated, and tested under various temperatures. Because the coil doesn't have any electric terminals for current leads, an HTS background magnet was used to induce the persistent current in the coil by field cooling process. A conduction cooling system with a GM cryocooler was prepared to keep the operating temperatures of the prototype coil much below the 77 K. We investigated the magnetic field drift characteristics under the various operating temperatures by measuring the center magnetic field with a cryogenic Hall sensor. The persistent current mode operation at 20 ~ 50K showed a strong possibility of the winding technique for the application such as MRI or NMR.

• 한국초전도학회:학술대회논문집
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• 한국초전도학회 2007년도 High Temperature Superconductivity Vol.XVII
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• pp.93-93
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• 2007

• Wind and Structures
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• 제30권5호
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• pp.451-463
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• 2020

Two-dimensional numerical simulations are conducted at a low Reynolds number Re = 100 to investigate the near wake of three identical circular cylinders that are arranged in an equilateral triangular configuration. The incident angle of the three-cylinder configuration with respect to incoming flow is varied from θ = 0° to 60°, while the spacing between adjacent cylinders (L) covers a wide range of L/D = 1.25-7.0, where D is diameter of the cylinder. Typical flow structures in the near wake of the three-cylinder configuration are identified, including a single Karman vortex street, bistable flip-flopping near wake, anti-phase and/or in-phase vortex shedding, shear layer reattachment, and vortex impingement, depending on the configuration (L/D, θ). The behavior of Strouhal number (St) is discussed in detail, echoing the distinct structures of near wake. Furthermore, fluid forces on the individual cylinders are examined, which, though highly depending on (L/D, θ), exhibit a close correlation to the near wake behavior.

• Wind and Structures
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• 제29권1호
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• pp.1-13
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• 2019

A numerical investigation on forces and flow around three square cylinders in side-by-side arrangement is conducted at a Reynolds number Re = 150 with the cylinder center-to-center spacing ratio L/W = 1.1 ~ 9.0, where W is the cylinder side width. The flowat this Re is assumed to be two-dimensional, incompressible, and Newtonian. The flow simulation is conducted by using ANSYS-Fluent. The flow around the three side-by-side cylinders entails some novel flow physics, involving the interaction between the gap and free-stream side flows as well as that between the two gap flows. An increase in L/W from 1.1 to 9.0 leads to five distinct flow regimes, viz., base-bleed flow (L/W < 1.4), flip-flopping flow (1.4 < L/W < 2.1), symmetrically biased beat flow (2.1 < L/W < 2.6), non-biased beat flow (2.6 < L/W < 7.25) and weak interaction flow (7.25 < L/W < 9.0). The gap flow behaviors, time-averaged and fluctuating fluid forces, time-averaged pressure, recirculation bubble, formation length, and wake width in each flow regime are discussed in detail.

• 한국항공우주학회지
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• 제46권9호
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• pp.752-759
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• 2018

본 논문에서는 비선형 모델 시뮬레이션을 통해 저속 회전 중인 유도포탄의 비행 모습을 확인하고 외란으로써 여러 가지 방향과 크기의 돌풍을 작용하여 유도포탄의 비행 안정성을 분석한 방법과 결과를 소개한다. 돌풍은 3m/s, 7m/s, 10m/s, 15m/s 네 가지의 속력을 가지고 26가지의 방향에서 탄도 정점 부근부터 작용하도록 설정하였다. 초당 1회전 및 3회전으로 회전하는 경우에 대해 총 208회의 시뮬레이션을 수행한 결과를 분석하였다. 초당 3회전으로 회전할 때는 탄체가 전복되지 않았지만, 초당 1회전으로 회전할 때는 7m/s 이상의 돌풍이 작용할 때 비행 후반부에 탄체가 전복되는 경우가 발견되었다. 탄체 비행 방향 반대쪽으로 작용하여 비행 방향 대기속도를 증가하는 돌풍은 해로운 영향을 주지 않았다. 탄체 전복은 모두 탄체가 하강하는 후반부에 발생하였으며, 탄도 정점 부근에서는 자세가 크게 진동하거나 탄체가 전복되지 않았다.

• 대한기계학회논문집B
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• 제22권6호
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• pp.860-873
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• 1998

In a low speed open-type wind tunnel, a group of parallel wakes downstream of two dimensional grid model consisting of several circular cylinders were experimentally investigated to study the response of the wake flows to the acoustic excitation, in hoping to promote the understanding of the underlying mechanism behind the gross flow change due to artificial excitation. In the unexcited wake flows, the development of the individual wakes behind cylinders was almost uniform for the ratio of the spacing to the cylinder diameter of s/d.geq.1.5. For smaller s/d, however, the jet streams issued through the gaps between the cylinders became biased in one side and the cylinders had wakes of different sizes. At s/d=1.25, the gap flow directions change in time, leading to unstable wake patterns. Further reduction in s/d made this unstable flip-flopping of the jets stable. The most effective excitation frequency was found to be in the Strouhal number range of St=0.5-0.6. This frequency was related to the vortex shedding. At s/d=1.75, the excitation frequency was 2 or 4 times the vortex shedding frequency. When the flow was excited at this frequency, the vortex sheddings were energized, and pairings between neighboring vortices were generated. Also, the merging process between individual wakes was accelerated. The unstable and unbalanced wake patterns at s/d=2.15 were made stable and balanced. The unstable and unbalanced wake patterns at s/d=2.15 were made stable and balanced. For smaller spacing of s/d .leq,1.0, the acoustic excitation became less effective in controlling the flow.

• 한국구조물진단유지관리공학회 논문집
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• 제26권2호
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• pp.28-36
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• 2022

매립지 위에 건설되는 항만시설물은 바람(태풍), 파랑, 선박과의 충돌 등 극한 외부 하중에 노출되기 때문에 구조물의 안전성 및 사용성을 주기적으로 평가하는 것이 중요하다. 본 논문에서는 항만 계류시설에 설치된 방충설비의 유지관리를 위하여 비전 및 딥러닝 기반의 방충설비 세분화(segmentation) 시스템을 개발하였다. 방충설비 세분화를 위하여 인코더-디코더 형식과 인간 시각체계의 편심 기능에서 영감을 얻은 수용 영역 블록(Receptive field block) 기반의 합성곱 모듈을 DenseNet 형식으로 개선하는 딥러닝 네트워크를 제안하였다. 네트워크 훈련을 위해 BP형, V형, 원통형, 타이어형 등 다양한 형태의 방충설비 영상을 수집하였으며, 탄성 변형, 좌우 반전, 색상 변환 및 기하학적 변환을 통해 영상을 증강시킨 다음 제안한 딥러닝 네트워크를 학습하였다. 기존의 세분화 모델인 VGG16-Unet과 비교하여 제안한 모델의 세분화 성능을 검증하였으며, 그 결과 본 시스템이 IoU 84%, 조화평균 90% 이상으로 정밀하게 실시간으로 세분화할 수 있음을 확인하였다. 제안한 방충설비 세분화 시스템의 현장적용 가능성을 검증하기 위하여 국내 항만 시설물에서 촬영된 영상을 기반으로 학습을 수행하였으며, 그 결과 기존 세분화 모델과 비교하였을 때 우수한 성능을 보이며 정밀하게 방충설비를 감지하는 것을 확인하였다.