• 한국전산구조공학회논문집
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• 제16권3호
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• pp.251-260
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• 2003

원형단면의 깊은 테이퍼봉과 보의 진동수와 모드형상을 결정하는 3차원 해석방법이 제시되었다. 수학적으로 1차원인 전통적인 봉과 보이론과는 달리, 본 연구에서는 3차원 동탄성방정식을 근간으로 하였다. 반경방향(r), 원주방향(θ), 축방향(z)으로의 변위성분인 u/sup r/, u/sub θ/, u/sub z/를 시간에 대해서는 정현적으로, θ에 대해서는 주기적으로, r과 z방향으로는 다수다항식의 형태로 표현하였다. 봉과 보의 위치(변형률)에너지와 운동에너지를 정식화하고, 고유치문제를 해결하기 위해 Ritz법을 사용하였으며, 진동수의 최소화과정을 통해 엄밀해의 상위경계치의 진동수를 구하였다. 이때 다항식의 차수를 증가시키면 진동수는 엄밀해에 수렴하게 된다. 봉과 보의 하위 5개의 진동수에 대해서 유효숫자 4자리까지의 수렴성 연구가 이루어졌다. 축방향으로 1차 직선적, 2차 및 3차 곡선으로 테이퍼된 9가지 형상의 봉과 보의 수치결과를 3차원 이론을 이용하여 최초로 계산하였다. 또한 선형 테이퍼 보의 예를 통해 3차원 Ritz법과 고전적인 1차원 Euler-Bernoulli 보이론과의 비교가 이루어졌다.

• 한국광학회지
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• 제11권6호
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• pp.411-417
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• 2000

SSC(Spot-size converter)가 집적된 1$1.3\mu{m}$ FP(Fabry-Perot)-LD(Laser Diode)에서 SSC 영역의 광도파로 구조가 단일모드광섬유와의 광결합 효율 및 정렬오차에 미치는 영향에 대해서 3차원 BPM(Beam Propagation Method)를 사용하여 알아보았다. 수지 taper의 경우 광결합효율을 향상하기 위해서는 taper 끝단에 충분한 길이의 직선도파로를 형성하는 것이 중요함을 알수 있었다. 또한 수평 taper 구조에서는 출사단 방향으로 도파로폭이 좁아지는 경우가 넓어지는 경우에 비해 유리하고, 수직 taper에 비해 완만한 도파로 경사가 필요함을 알 수있었다. 단일모드 광섬유와의 광결합 손실 및 정렬오차 허용도의 관점에서 좋은 특성을 주는 SSC 도파로 모양을 제시하였다.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2005년도 춘계 학술발표회 논문집
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• pp.79-86
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• 2005

This paper deals with the static optimal shapes of simple beams which are subjected to a vertical point load. The area and second moment of inertia of the regular polygon cross-section of the tapered beams are determined, which have always same volume and same length for the parabolic taper. The differential equation governing the elastic curve is derived using the small deflection theory and solved numerically. By using the numerical results of deflections, rotations and bending stresses of such beams, the optimal shapes, namely, optimal section ratios, of the beams subjected to a single point load according to variation of load position parameters are determined and presented in the figures. Examples of the static optimal shapes for beams with a single load and multiple loads are reported. The design process of this study can be used directly for the minimum weight design of simple beams.

• Structural Engineering and Mechanics
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• 제27권2호
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• pp.243-257
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• 2007

A numerically efficient superelement is proposed as a low degree of freedom model for dynamic analysis of rotating tapered beams. The element uses a combination of polynomials and trigonometric functions as shape functions in what is also called the Fourier-p approach. Only a single element is needed to obtain good modal frequency prediction with the analysis and assembly time being considerably less than for conventional elements. The superelement also allows an easy incorporation of polynomial variations of mass and stiffness properties typically used to model helicopter and wind turbine blades. Comparable results are obtained using one superelement with only 14 degrees of freedom compared to 50 conventional finite elements with cubic shape functions with a total of 100 degrees of freedom for a rotating cantilever beam. Excellent agreement is also shown with results from the published literature for uniform and tapered beams with cantilever and hinged boundary conditions. The element developed in this work can be used to model rotating beam substructures as a part of complete finite element model of helicopters and wind turbines.

• Structural Engineering and Mechanics
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• 제66권6호
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• pp.737-748
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• 2018

The current study presents a new technique in the framework of the nonlocal elasticity theory for a comprehensive buckling analysis of Euler-Bernoulli nano-beams made up of bidirectional functionally graded material (BDFGM). The mechanical properties are considered by exponential and arbitrary variations for axial and transverse directions, respectively. The various circumstances including tapering, resting on two-parameter elastic foundation, step-wise or continuous variations of axial loading, various shapes of sections with various distribution laws of mechanical properties and various boundary conditions like the multi-span beams are taken into account. As far as we know, for the first time in the current work, the buckling analyses of BDFGM nano-beams are carried out under mentioned circumstances. The critical buckling loads and mode shapes are calculated by using energy method and a new technique based on calculus of variations and collocation method. Fast convergence and excellent agreement with the known data in literature, wherever possible, presents the efficiency of proposed technique. The effects of boundary conditions, material and taper constants, foundation moduli, variable axial compression and small-scale of nano-beam on the buckling loads and mode shapes are investigated. Moreover the analytical solutions, for the simpler cases are provided in appendices.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2011년도 춘계학술대회 논문집
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• pp.149-150
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• 2011

• Smart Structures and Systems
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• 제19권3호
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• pp.309-322
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• 2017

In this paper, the buckling, and free vibration analysis of tapered functionally graded carbon nanotube reinforced composite (FG-CNTRC) micro Reddy beam under longitudinal magnetic field using finite element method (FEM) is investigated. It is noted that the material properties of matrix is considered as Poly methyl methacrylate (PMMA). Using Hamilton's principle, the governing equations of motion are derived by applying a modified strain gradient theory and the rule of mixture approach for micro-composite beam. Micro-composite beam are subjected to longitudinal magnetic field. Then, using the FEM, the critical buckling load, and natural frequency of micro-composite Reddy beam is solved. Also, the influences of various parameters including ${\alpha}$ and ${\beta}$ (the constant coefficients to control the thickness), three material length scale parameters, aspect ratio, different boundary conditions, and various distributions of CNT such as uniform distribution (UD), unsymmetrical functionally graded distribution of CNT (USFG) and symmetrically linear distribution of CNT (SFG) on the critical buckling load and non-dimensional natural frequency are obtained. It can be seen that the non-dimensional natural frequency and critical buckling load decreases with increasing of ${\beta}$ for UD, USFG and SFG micro-composite beam and vice versa for ${\alpha}$. Also, it is shown that at the specified value of ${\alpha}$ and ${\beta}$, the dimensionless natural frequency and critical buckling load for SGT beam is more than for the other state. Moreover, it can be observed from the results that employing magnetic field in longitudinal direction of the micro-composite beam increases the natural frequency and critical buckling load. On the other hands, by increasing the imposed magnetic field significantly increases the stability of the system that can behave as an actuator.

• International Journal of Ocean System Engineering
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• 제2권3호
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• pp.195-199
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• 2012

This paper reports a new analytical method to calculate the planar displacement of structures. The cross-sections were assumed to remain in plane and the deflection curve was evaluated using the curvature values geometrically, despite being solved with differential equations. The deflection curve was parameterized with the arc-length of the curvature values, and was taken as an assembly of chains of circular arcs. Fast and accurate solutions of complex deflections can be obtained easily. This paper includes a comparison of the nonlinear displacements of an elastic tapered cantilever beam with a uniform moment distribution among the proposed analytical method, numerical method of the theory and large deflection FEM solutions.

• Journal of Electrical Engineering and Technology
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• 제8권4호
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• pp.856-862
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• 2013

A cavity-backed two-arm spiral antenna for partial discharge diagnosis is presented. The proposed antenna consists of a two-arm Archimedean spiral, a tapered microstrip balun as spiral antenna feed, and a ring-shaped absorber-loaded cavity. The Archimedean spiral antenna is designed for the operating frequency band of 0.3 GHz to 1.5 GHz and fed by the tapered microstrip balun. The cavity is utilized to transform the bidirectional beam into a unidirectional beam, thereby enhancing gain. The ring-shaped absorber is stacked in the cavity to reduce the reflected waves from the cavity wall. The proposed antenna is designed and simulated using CST Microwave Studio. A prototype of the proposed antenna is likewise fabricated and tested. The measured radiation patterns are directional to the positive z-axis, and the measured peak gain is 8.13 dBi at a frequency of 1.1 GHz.

• Structural Engineering and Mechanics
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• 제23권2호
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• pp.209-216
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• 2006