• Journal of Korean Society of Steel Construction
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• v.14 no.4
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• pp.489-497
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• 2002

Nonlinear behavior and large deformation cannot be analyzed using techniques based on linear theory. Nonetheless, they are emerging as gradually huge and complex structures. In addition, the optimum design of structure is necessary in the development of high-performance computation and numerical methods. as well as stricter design-criterion. Therefore, the structural problems in engineering that are limited to the linear region must be extended to the nonlinear region. Likewise, structural behavior must be accurately analyzed. In turn, this requires considering the expected problems beforehand. Only then can an efficient, economical, and optimized structure be designed. This paper presents the solution of the geometrical nonlinear problem of anisotropic cylindrical shell. The characteristics of the geometrical nonlinear behavior of anisotropic circular cylindrical shells may vary according to several causes. e.g., change of fibers, curvature in the circumferential direction, subtended angle, aspect, etc. Parametric studies were conducted to determine the effect of factors on the large deflection behavior of laminated shells, with interesting observations.

• Journal of the Korean Institute of Telematics and Electronics S
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• v.36S no.7
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• pp.62-70
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• 1999

To achieve precision positioning, working area is required within $5mm{\times}5mm$ and positioning error is allowed within minimum ${\pm}4{\mu}m$. As a general three-layered table takes working range from several centimeters and a few tens of centimeters, it has disadvantages compared with precision positioning table, such as larger working range and rough accuracy. In this paper we design and implement a parallel $XY{\theta}$ table with three linear actuators, where one is on the horizontal direction and the others on the vertical direction on behalf of a degree of $XY{\theta}$ freedom. Finally, the experimental results of precision positioning is showed by using new image processing algorithms with two CCD cameras.

• Computational Structural Engineering
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• v.7 no.4
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• pp.103-111
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• 1994

Based on a variational principle of the consistent shear deformable discrete laminate theory derived in the companion paper Part I, a finite element procedure for the vibration analysis of laminated composite plates is presented. The present formulation takes the in-plane displacements of an arbitrary layer, the rotations of the cross section of each layer and transverse displacement of the plate as the state variables at a nodal point of finite element, resulting in total nodal degree of freedom of 2(n+l) +1 for the n-layered laminate. Thus, it allows to specify displacement boundary conditions of layer stretching and/or rotation of layer cross sections around the plate edge and/or lateral displacement. The developed procedure is applied to the free vibration problem for sandwich-type hybrid laminates composed of layers with drastically different material properties whose elasticity solutions are known. Comparison of analysis results with other FEM solutions showed that the present formulation yields better accuracy.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.49 no.7
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• pp.539-547
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• 2021

Helicopter rotor blade is required to be designed by considering the interacting effects among aerodynamics, flexibility, and controllability. The reverse design allows the structural components to have common characteristics by using the configuration numerics and experimental results. This paper aims to design the composite rotor blade which will feature common characteristics with that of BO-105. The present engineering design procedure is done by dividing the rotor blade into a few sections and composite laminates across the cross section. For each section, variational asymptotic beam sectional analysis (VABS) program is used to evaluate its flapwise, lagwise, and torsion stiffnesses to have discrepancy smaller than certain tolerance. Finally, CAMRAD II is used to predict the stress acting on the rotor blade during the specific flight condition and to check whether the present deign is structurally valid.

• Journal of the Korean Society for Nondestructive Testing
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• v.15 no.2
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• pp.357-363
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• 1995

Disbond size of adhesively bonded single lap and double lap joints CFRP composite specimens has been evaluated using acousto-ultrasonic(AU) technique. Frequency spectra for all specimens were obtained by measuring peak amplitude of the stress wave propagated through the bond-lines. By analyzing these frequency spectra, peak amplitude was found to be proportional to fractional bonding area and to be maxima at the fundamental and the third order higher harmonic frequencies of specimen thickness mode. The disbond size can be evaluated quantitatively and this technique can be applied to real structures if the reference specimens are prepared in advancve.

• Journal of the Earthquake Engineering Society of Korea
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• v.5 no.4
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• pp.97-105
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• 2001

Rubber bearings may exhibit a significant cold temperature effect and some velocity dependency(strain rate effect). Both of these attributes which affect non-linear behavior must be accounted for when accurately modeling the bearings behavior, therefore, an analytical models is proposed to consider the effects of the cold temperature and strain rate on both rubber and lead. From the results of an experimental investigation where the frozen bearings were tested under lateral cyclic loading with constant axial load, a non-linear system identification with least squares procedure was applied to determine the material properties of rubber and lead. It is demonstrated that the proposed analytical model is able to simulate the reversed cyclic loading behavior of elastometric and lead-rubber bearings.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.22 no.3
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• pp.540-544
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• 1998

Compliance calibration method is frequently used to determine $G_IC$ from the DCB composite specimen. However, the method requires at least 4 to 5 fracture test (loading-unloading) records. In this study, $G_IC$ of unidirectional graphite/epoxy DCB composites was determined from the elastic work factor approach which uses a single fracture test record. In order to inspect the validity of the elastic work factor approach, $G_IC$ determined from the elastic work factor approach was compared to that of determined from the compliance calibration method. It was shown that $G_IC$ determined from the elastic work factor approach was comparable to that determined from the compliance calibration method. That is, the elastic work factor approach can be used to determine $G_IC$ of unidirectional graphite/epoxy DCB specimen from a single fracture record.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.14 no.2
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• pp.202-208
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• 2003

In this paper, we proposed a microstrip patch array antenna for DBS reception which had high gain and high tilted angle through mutual coupling driver patch to parasitic patch in H-plane edge and broadside direction in different layers. It was designed and fabricated in 16$\times$8 array by using low cost polyester based copper-clad laminate and foam instead of high cost dielectric substrate. It had gain of 22.9 dBi, beamwidth of 4.6$^{\circ}$, and tilted angle from broadside direction of 43.9$^{\circ}$.

• Journal of Energy Engineering
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• v.8 no.1
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• pp.23-33
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• 1999

용융탄산염 연료전지의 대형화에 관한 기본 기술을 확립하기 위하여 전극의 유효면적이 625 $\textrm{cm}^2$인 단위전지를 20단 적층한 내부 분배형 용융탄산염 연료전지 스택을 제작하고 그 성능을 살펴보았다. 연료로 72% H2/18% CO2/10% H2O를 , 산화제로는 70% air/30% CO2의 혼합 기체를 사용하여 운전한 결과 전류밀도가 150 mA/$\textrm{cm}^2$이고 연료 및 산화제의 이용율이 0.4일 때, 스택 전압이 16.62 V로 1.56 kW의 높은 초기출력을 나타내었다. 스택 내 분리판에서의 온도 분포는 가스 흐름 방향으로 온도가 증가하였으며 스택출력이 높아질수록 가스 배출 부분의 온도가 상승하였다. 스택 내 각 단위전지간의 성능 분포는 균일하지 않았으며, 가스이용율에 따라 그 편차가 증가하였다. 연속 운전 300시간 후부터 스택의 성능이 감소하였으며, 그 원인을 분석한 겨로가 탄소 석출과 부식 생성물에 의한 전기 단락 때문으로 밝혀졌다. 본 연구를 통하여 anode 출구에서의 가스 조성을 분석함으로써 전기 단락에 의한 전압 손실량을 계산하는 기법을 확립하였다. 또한 본 연구에서 얻은 결과를 통하여 향후 스택의 대형화와 장수명화에 대한 대책을 제시하였다.

• Proceedings of the KIEE Conference
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• 2006.10d
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• pp.104-106
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• 2006

Slotless BLDC motor는 Slot과 Teeth가 없으므로 이에 따른 Cogging Torque 및 Torque Ripple이 거의 존재 하지 않으며, 전동기의 무게 또한 감소하게 된다. 또한 권선의 장주(Span)가 짧아 Inductance가 낮기 때문에 고속화가 용이해지며, Slot의 부재는 좀 더 많은 Coil권선을 이용 할 수 있다. 하지만 모터의 구조상 전기장하가 높아짐에 따라 권선의 온도 상승에 대한 보완 등이 필요로 되어 지고 있다. 따라서 본 논문에서는 온도 상승 문제를 해결하기 위해 열 발생과 모터사이의 관계 규명을 전류 밀도 함수로 표시 하였고, 전류 밀도 최소화 설계 방법을 제안하였다. 퍼미언스법에 의한 간략 설계에 의해서 기본 설계를 실시 한 후 FEM을 통한 정밀 해석을 통해서 각각의 민감도를 분석하여 최적의 파라메타를 선정하는 방식을 취하였다. 또한 고속 회전시 발생되는 진동을 저감하기 위해 모터의 길이방향 즉 적층과의 관계를 통하여 진동 저감 설계를 제안하였다.