• Proceedings of the Computational Structural Engineering Institute Conference
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• 2010.04a
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• pp.546-549
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• 2010

현대사회에서 점차 경량콘크리트의 활용도에 대한 관심이 높아지고 있으나 이에 관한 연구실적은 아직까지 미비하다. 경량콘크리트는 그 특성상 가벼운 자중과 높은 에너지 흡수성을 가지고 있다는 점에서 방호벽에 적용 가능한 재료로 볼 수 있다. 이에 본 연구에서는 이러한 점을 고려하여 경량 방호벽에 대한 컴퓨터 시뮬레이션을 통한 경량콘크리트 방호벽의 거동해석을 수행하였으며, 이를 위해 미세역학기반 경량콘크리트 모델을 상용 유한요소 프로그램인 ABAQUS에 적용하여 경량콘크리트 압축공시체에 관한 해석을 선 수행하였다. 이를 통해 도출된 손상변수를 통하여 실제 방호벽에 대한 정적 하중 시뮬레이션을 수행하였다.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.24 no.1
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• pp.69-78
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• 2011

In this study, an optimization method using multi-objective genetic algorithm(MOGA) has been proposed to develop a fuzzy control algorithm that can effectively control a smart tuned mass damper(TMD). A 76-story benchmark building subjected to wind load was selected as an example structure. The smart TMD consists of 100kN MR damper and the natural period of the smart TMD was tuned to the first mode natural period of the example structure. Damping force of MR damper is controlled to reduce the wind-induced responses of the example structure by a fuzzy logic controller. Two input variables of the fuzzy logic controller are the acceleration of 75th floor and the displacement of the smart TMD and the output variable is the command voltage sent to MR damper. Multi-objective genetic algorithm(NSGA-II) was used for optimization of the fuzzy logic controller and the acceleration of 75th story and the displacement of the smart TMD were used as objective function. After optimization, a series of fuzzy logic controllers which could appropriately reduce both wind responses of the building and smart TMD were obtained. Based on numerical results, it has been shown that the control performance of the smart TMD is much better than that of the passive TMD and it is even better than that of the sample active TMD in some cases.

• Proceedings of the Computational Structural Engineering Institute Conference
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• 2000.04b
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• pp.365-370
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• 2000

A sliding mode fuzzy control (SMFC) algorithm is applied to design a controller for a benchmark problem on a wind- excited building. The structure is a 76-story concrete office tower with a height of 306 meters, hence the wind resistance characteristics are very important for the serviceability as well as the safety. A control system with an active tuned mass damper is assumed to be installed on the top floor. Since the structural acceleration is measured only at ,limited number of locations without measurement of the wind force, the structure of the conventional continuous sliding mode control may have the feed-back loop only. So, an adaptive least mean squares (LMS) filter is employed in the SMFC algorithm to generate a fictitious feed-forward loop. The adaptive LMS filter is designed based on the information of the stochastic characteristics of the wind velocity along the structure. A numerical study is carried out. and the performance of the present SMFC with the ,adaptive LMS filter is investigated in comparison with those of' other control, of algorithms such as linear quadratic Gaussian control, frequency domain optimal control, quadratic stability control, continuous sliding mode control, and H/sub ∞///sub μ/, control, which were reported by other researchers. The effectiveness of the adaptive LMS filter is also examined. The results indicate that the present algorithm is very efficient .

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2009.04a
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• pp.652-653
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• 2009

In this study, flow-induced vibration (FIV) analyses have been conducted for a 3D compressor blade model. Advanced computational analysis system based on computational fluid dynamics (CFD) and computational structural dynamics (CSD) has been developed in order to investigate detailed dynamic responses of designed compressor blades. Fluid domains are modeled using the computational grid system with local grid deforming and remeshing techniques. Reynolds-averaged Navier-Stokes equations with $\kappa-\varepsilon$ turbulence model are solved for unsteady flow problems of the rotating compressor model. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of the 3D compressor blade for fluid-structure interaction (FSI) problems. Detailed dynamic responses and instantaneous pressure contours on the blade surfaces considering flow-separation effects are presented to show the multi-physical phenomenon of the rotating compressor blade.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.19 no.6
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• pp.551-559
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• 2009

In this study, flow-induced vibration(FIV) analyses have been conducted for a 3D compressor blade model. Advanced computational analysis system based on computational fluid dynamics(CFD) and computational structural dynamics(CSD) has been developed in order to investigate detailed dynamic responses of designed compressor blades. Fluid domains are modeled using the computational grid system with local grid deforming and remeshing techniques. Reynolds-averaged Navier-Stokes equations with $\kappa-\epsilon$ turbulence model are solved for unsteady flow problems of the rotating compressor model. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of the 3D compressor blade for fluid-structure interaction(FSI) problems. Detailed dynamic responses and instantaneous pressure contours on the blade surfaces considering flow-separation effects are presented to show the multi-physical phenomenon of the rotating compressor blade.

• Computational Structural Engineering
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• v.11 no.1
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• pp.171-178
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• 1998

The added viscoelastic dampers increase damping and stiffness of buildings and results in so called non-classical or non-proportional damping problem. In this system the eigenvectors of the undamped system may not diagonalize the damping matrix, and the system is generally analyzed by converting the equation of motion into a 2n first order state-space form. As this approach is complex and time-consuming compared to the classically damped problem, the system is often analyzed by neglecting the off-diagonal terms in the damping matrix. In this paper the theoretical background of the approximate approach is studied, and the vibration characteristics of a three-story shear building with a viscoelastic damper are investigated using the exact and approximate method. It is found that the approximate method may produce good result when the additional damping is small, but as the damping increases the error also increase.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.17 no.2
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• pp.161-169
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• 2004

This paper deals with system identification of a three-story building model with active mass damper (MID) for the controller design. Observer Kalman filter identification (OKID) technique is applied to find the relationship between the experimental results of the input and output. The inputs to the building model with MID are ground accelerations and motor command signal, which are, respectively, simulated earthquake and equivalent control force. The outputs are each floor acceleration and MID acceleration. The MID controller is designed based on the experimentally identified building system. Finally it is shown that experimental results agree accurately with simulated results.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.111-114
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• 2010

MOV(Main Oxidizer shut-off Valves) control the combustion of launch vehicle systems by the supply and the isolation of liquid oxygen to a main combustion chamber in launch vehicle systems. Moreover, the MOV should secure a constant flow rate of liquid oxygen for combustion instability in the steady operational state. To modify the middle flange and rip of inlet valve design by Computer Aided Structural Analysis for improvement of EM core functions. In result, it has been verified to improve performance of EM by tests.

• Computational Structural Engineering
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• v.10 no.2
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• pp.203-211
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• 1997

In the design of tall building system, the wind loading can be more dominant factor than earthquake loading, and thus, it is important to check the stability and human comfort against wind. Experimental wind tunnel test is usually performed to predict wind behavior of a tall building, however, the test is not cost-effective in the preliminary stage for various structural models of tall building systems. In this regard, the study is focused on the numerical wind analysis of the tall building with and without tuned mass dampers based on the three dimensional model of wind loads and building behavior. As a numerical result, an asymmetrical 102-story tall building is presented to show the results of root mean squares of build responses with and without tuned mass dampers.

• Computational Structural Engineering
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• v.11 no.3
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• pp.173-185
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• 1998

본 연구에서는 자동차엔진 및 트랜스미션 성능시험을 위한 다이나모 베드구조물을 분석하고 설계하였다. 해석상에 고려된 베드구조물은 Ⅰ형강 구조물, 보강된 박스구조물 그리고 블록구조물로 제작되었으며, 시험을 위한 엔진 및 트랜스미션은 베드상판에 장착된다. 엔진구동시 회전에 의한 진동이 발생된다. 공진을 피하기 위해 베드구조는 충분한 구조적 일체성을 가져야 한다. 본 연구에서는 베드 구조물의 응력, 변위 그리고 자유진동해석이 ANSYS Code를 이용한 유한요소해석이 수행되었다. Ⅰ형강 구조형 베드 구조물에서 최대 응력은 23.2MPa에서 90.3MPa까지 나타났으며, 최대 처짐은 0.25㎜에서 0.92㎜까지 나타났다. 박스 구조형 베드 구조물에서 최대 응력은 0.028MPa에서 0.259MPa까지 나타났으며, 최대 처짐은 0.031㎜에서 0.413㎜까지 나타났다. 그리고 박스구조형 베드 구조물에서 최대 처짐은 0.92MPa에서 2.15MPa까지 나타났으며, 최대 처짐은 1.1㎜에서 2.7㎜까지 나타났다. 모든 구조물이 응력과 처짐 값에서 매우 안정적인 범위 내에서 발생됨을 볼 수 있었다. 구조진동해석에서 Ⅰ형강 베드구조물의 고유진동수는 112.03㎐에서 141.66㎐까지의 범위에 발생되었다. 박스 구조형 베드구조물에서의 고유진동수는 396.93㎐에서 755.11㎐까지의 범위에서 발생되었다. 마지막으로 블록구조형 베드구조물에서는 266.51㎐에서 244.67㎐까지의 고유진동수를 찾을 수 있었다. 모든 구조물에서 베드구조물의 무게증가에 따른 기본진동수는 증가된다. 베드시스템의 지지기초시스템은 2자유도계 시스템으로 설계되었으며, 다양한 질량변화 및 스프링상수 변화에 따른 진동해석을 수행하였다. 질량비가 증가될수록 고유진동수는 크게 감소되며, 스프링상수가 증가될수록 고유진동수는 감소된다.