• KSCE Journal of Civil and Environmental Engineering Research
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• v.14 no.6
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• pp.1281-1288
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• 1994

Beams curved in plan are often designed with the circular curved member system including warping effects. In this study, the curved bridges are idealized as the circular curved member system with singly symmetric cross sections and simply supported ends. Displacement fields of them to satisfy the boundary conditions are expanded by Fourier series and the governing equation of natural frequencies of them is derived. The distributions of the characteristics of natural frequencies of them are shown according to the variations of relevant parameters-angle of intersection, curvature, and parameter of symmetry of cross section which can represent the properties of the curved bridges. A parametric study is conducted to investigate the effect of relevant parameters on natural frequencies.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2004.11a
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• pp.709-712
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• 2004

A study of the coupled flexural-torsional vibrations of thin-walled beams with monosymmetric cross-section is presented. The governing differential equations for free vibration of such beams are solved numerically to obtain natural frequencies and their corresponding mode shapes. The beam model is based on the Bernoulli-Euler beam theory and the effect of warping is taken into consideration. Numerical results are given for two specific examples of beams with free-free, clamped-free, hinged-hinged, clamped-hinged and clamped-clamped end constraints both including and excluding the effect of warping stiffness. The effect of warping stiffness on the natural frequencies and mode shapes is discussed and it is concluded that substantial error can be incurred if the effect is ignored.

• Magazine of the Korea Concrete Institute
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• v.9 no.2
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• pp.99-108
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• 1997

Many studies on the second-order analysis of reinforced concrete columns have been dealt for symmetric sections under uniaxial loading. However, actual columns are practically subjected to hiaxial loading. In order to more accurately predict the behavior of concrete columns under biaxial loading. the interaction between bending moments of major and minor axes should be considered. In this paper, a stiffness matrix of columns under biaxial loadings was derived and a numerical method was proposed. Numerical analyses, based on the proposed method. were performed to predict behavior of concrete columns with square and rectangular sections under various loading conditions. The analytical results were compared to those using the moment magnifier method in ACI code. It was found that the ultimate strength of concrete rectangular columns, fhr some cases of' biaxial loading conditions. calculated by the moment magnifier method was larger than the values based on the proposed method and therefore. may be ovet.'stimated.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.26 no.1A
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• pp.99-106
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• 2006

Due to single symmetry of cross section, T-shaped members are likely to buckle in a flexural-torsional mode when they are subjected to axial compression. Therefore, the flexural-torsional buckling can be regarded as a governing mode of global buckling. An experimental program has been carried out to investigate the flexural-torsional buckling behavior of pultruded T-shaped members. Two types of pultruded members were tested in the experiment, and they were made of either E-glass/vinylester or E-glass/polyester. Lay-up and thickness of reinforcing layers, volume fractions of each constituents in layers, mechanical properties were experimentally determined. Two sets of knife edge fixure were used to simulate simple support condition for flexure and twisting, and the lateral displacements and the angle of twist were measured using three potentiometers. Every specimen buckled in a flexural-torsional mode, and most of the specimens showed post-buckling strength.

• Geophysics and Geophysical Exploration
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• v.25 no.1
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• pp.38-43
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• 2022

In case axial symmetrical bodies with varying cross sections such as volcanic conduits and unexploded ordnance (UXO), it is efficient to approximate them by adding the response of thin disks perpendicular to the axis of symmetry. To compute the vector magnetic and magnetic gradient tensor respones by such bodies, it is necessary to derive an analytical expression of the circular disk. Therefore, in this study, we drive closed-form expressions of the vector magnetic and magnetic gradient tensor due to a circular disk. First, the vector magnetic field is obtained from the existing gravity gradient tensor using Poisson's relation where the gravity gradient tensor due to the same disk with a constant density can be transformed into a magnetic field. Then, the magnetic gradient tensor is derived by differentiating the vector magnetic field with respect to the cylindrical coordinates converted from the Cartesian coordinate system. Finally, both the vector magnetic and magnetic gradient tensors are derived using Lipschitz-Hankel type integrals based on the axial symmetry of the circular disk.

• Geophysics and Geophysical Exploration
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• v.26 no.1
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• pp.1-7
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• 2023

This study derives the expressions of vector gravity and gravity gradient tensor due to an elliptical cylinder. The vector gravity for an arbitrary three-dimensional (3D) body is obtained by differentiating the gravitational potential, including the triple integral, according to the shape of the body in each axis direction. The vector gravity of the 3D body with axial symmetry is integrated along the axial direction and reduced to a double integral. The complex Green's theorem using complex conjugates subsequently converts the double integral into a one-dimensional (1D) closed-line integral. Finally, the vector gravity due to the elliptical cylinder is derived using 1D numerical integration by parameterizing a boundary of the elliptical cross-section as a closed line. Similarly, the gravity gradient tensor due to the elliptical cylinder is second-order differentiated from the gravitational potential, including the triple integral, and integrated along the vertical axis direction reducing it to a double integral. Consequently, all the components of the gravity gradient tensor due to an elliptical cylinder are derived using complex Green's theorem as used in the case of vector gravity.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.13 no.1
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• pp.65-74
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• 1993

The buckling load of a blade stiffened laminated composite plate having midplane symmetry is maximized for a given total weight. The thicknesses of the layers and the width and height of the stiffener are taken as the design variables. Buckling analysis is carried out using a finite element method. The optimization problem is solved using an IMSL subroutine. Due to the highly nonlinear nature of the optimality equations, several local optimum solutions are found. Various combinations of fiber orientation for the laminate layers and the blade stiffener are investigated to examine their relative efficiency. Out of several cases examined, the best design was produced from the combination of ($0^{\circ}Beam/0^{\circ}/90^{\circ}$)s.

• Proceedings of the Mineralogical Society of Korea Conference
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• 2003.05a
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• pp.84-85
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• 2003

소백산육괴의 동부에 분포하는 영양-울진지역의 선캠브리아기 변성암류는 평해층, 기성층, 원남층, 평해화강편마암, 하다우백질화강편마암 등으로 구성되어 있다(김옥준 외, 1963). 그러나, 최근 김남훈 외(2001, 2002)은 야외조사연구와 암석학적 및 지구화학적 연구를 통하여 주로 변성화산암류로 기재되었던 기성층은 변성화산암류가 아니라 평해층과 원남층에서 산출되는 화강암질편마암과 각섬암 기원의 변성암류가 연성전단변형을 받아 형성된 압쇄암 내지 초압쇄암으로 되어 있고, 기존의 기성층은 변성화산암류와 같이 성분상으로 구분되는 별개의 층이 아닌 구조적으로 만들어진 연성전단대의 중심부일 가능성을 시사한 바가 있다. 본 연구는 연성전단대의 연장성 및 연성전단대 형성과 관련된 지구조운동의 특성을 파악하고, 중첩된 변형구조들의 선후관계로부터 영양-울진지역 선캠브리아기 변성암류에 대한 변형작용사를 규명하기 위해 기성층의 분포지를 중심으로 이 지역 선캠브리아기 변성암류에 대한 상세한 야외지질조사를 실시하였다. 그 결과, 예천(북후면-평은면)지역을 통과하여 봉화 부근에서 동북동-서남서 방향이 동-서 방향으로 전환하여 장군봉지역까지 연장되는 것으로 알려져 있는 우수 주향 이동성 예천전단대(KIGAM, 1995; 강지훈 외 1997; 강지훈, 2000; 강지훈과 김형식, 2000)는 영양-울진지역까지 연장됨이 확인된다. 또한, 영양-울진지역의 선캠브리아기 변성암류에는 연성전단변형 이전에 적어도 한 번의 습곡작용과 이후에 적어도 두 번의 습곡작용이 인지된다. 각 변형단계별 특징적인 구조요소를 요약하면 다음과 같다. D1 변형: 편마면 내지 편리(S0)가 습곡되어 형성된 F1 습곡은 동-서 방향의 준 수평적인 습곡축을 갖는 뿌리 없는 등사습곡 형태로 인지된다. 양 날개부의 S0 엽리는 F1 습곡축면(S1)으로 완전히 전위된 하나의 엽리(S0-1)로 나타나고, S0-1 엽리는 이 지역의 광역엽리로 인지된다. S0-1 광역엽리는 구성암류의 대상 분포 방향과 유사한 서북서 주향에 북쪽으로 중각 경사하는 집중된 방향성을 보이며 분산되어 나타난다. D2 변형: 변형구조로는 신장선구조, 압쇄구조면, 비대칭습곡 등으로 인지된다. 신장선구조는 S0-1 엽리면상에서 주로 신장된 석영(집합체)과 장석(집합체)들의 정향배열에 의해 정의되고, S0-1 엽리의 주향 방향으로 저각으로 침강하는 집중된 방향성을 보이며 분산되어 나타난다. 신장선구조에 평행하고 S0-1 엽리에 수직한 단면에서는 상부-동쪽-이동의 우수주향 이동성 연성 전단운동감각을 지시하는 구조요소들이 다량 관찰된다. 연성전단변형에 의해 형성된 압쇄구조면은 전단엽리와 압쇄엽리에 각각 해당하는 C면과 S면 등이 인지된다. 전단엽리 C면은 S0-1 광역엽리와 거의 일치하고, 압쇄엽리 S면은 F2 비대칭습곡의 축면엽리와 거의 일치한다. S0-1 엽리를 습곡시키는 F2 비대칭습곡은 S0-1 엽리를 전단면으로 하여 상부-동쪽-이동 전단운동에 의해 형성된 밀착습곡 형태로 인지된다. F2 습곡축은 북동 방향으로 중각 내지 저각 침강하고 F1 습곡축과는 65$^{\circ}$-75$^{\circ}$ 범위의 사이각을 이룬다. F2 습곡축면은 동북동 주향에 북쪽으로 중각으로 경사하고 F1 습곡축면과는 20$^{\circ}$-40$^{\circ}$ 범위의 사이각을 이룬다. D3 변형. S0-1 엽리와 압쇄구조면 등을 습곡시키는 F3 습곡은 준 수평적인 습곡축과 습곡축면을 갖는 개방 횡와습곡의 형태로 인지된다. D4 변형: F4 습곡은 비대칭 공역성 킹크습곡, 공역성 충상단층에 수반되어 나타나는 드래그습곡, 대칭 개방 직림습곡 등의 다양한 습곡 형태로 인지된다. 이들 F4 습곡의 축면엽리는 일반적으로 동-서 주향에 남쪽과 북쪽으로 경사한다. 그 경사각은 비대칭 공역성 킹크습곡(저각), 드래그습곡(중각), 대칭 개방 직립습곡(고각) 순으로 고각을 이룬다. F4 습곡축은 동쪽과 서쪽으로 저각 침강하는 집중된 방향성을 보인다. 공역성 충상단층은 동-서 주향에 남쪽과 북쪽으로 경사하는 단층면과 상부가 북쪽과 남쪽으로 충상하는 운동상을 보인다. 드래그습곡의 축면엽리는 이러한 공역성 충상단층운동의 전단압축방향에 수직으로 발달한다. 이러한 D4 변형구조는 남-북 방향의 압축 지구조 환경하에서 형성된 것으로 고찰된다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.35 no.12
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• pp.1273-1283
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• 2011

A 3-dimensional unsteady numerical analysis has been performed to evaluate the aerodynamic characteristics of a Giromill. Generally, the structure of a Giromill is simple and therefore easy to develop. In addition, the high solidity of the Gironmill helps improve the self-starting capacity at a low tip speed ratio (TSR). However, contrary to the Darrieus wind turbine which has a TSR of 4-7, a Giromill has a low TSR of 1-3. In this study, the aerodynamic characteristics of the Giromill are investigated using computational fluid dynamics (CFD). Three straight-bladed wings are used, and the solidity of the Giromill is 0.75. In contrast to a Darrieus wind turbine having low solidity, the Giromill shows a sudden decrease in the aerodynamic performance because of the interference between the wings and an increase in the drag on the wings in the downstream direction where wind flow is significantly reduced. Consequently, the aerodynamic performance decreased at a TSR value lower than 2.4.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.39 no.1
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• pp.55-62
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• 2015

The electromagnetic force induced by an intense electric current pulse, which generates an electromagnetic field around the metal jet originating from a shaped charge, can disperse and scatter the high-speed metal jet. An electric device consisting of an RLC circuit applies an intense electric current pulse that flows in the circuit while the metal jet passes between two electrodes. In this study, the metal jet formation was simulated using the ALE technique in 2-D, and a 3-D finite element model was mapped using 2-D simulation results to induce the electric current directly. The deformed shapes of the metal jet and the electromagnetic force were calculated using a finite element analysis by inducing the electric current directly, and the major parameters of the intense electric current pulse for breaking up the metal jet were examined.