• 제목/요약/키워드: complex modes

검색결과 402건 처리시간 0.022초

2차원 유체-구조물-지반계의 지진응답해석 (Earthquake Response Analysis for 2-D Fluid-Structure-Soil Systems)

  • 윤정방;장수혁;김재민
    • 한국해양공학회:학술대회논문집
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    • 한국해양공학회 2001년도 추계학술대회 논문집
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    • pp.132-137
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    • 2001
  • This paper presents a method of seismic analysis for a 2-D fluid-structure-soil interaction systems. With this method, the fluid can be modeled by spurious free 4-node displacement-based fluid elements which use rotational penalty and mass projection technique in conjunction with the one point reduced integration scheme to remove the spurious zero energy modes. The structure and the near-field soil are discretized by the standard 2-D finite elements, while the unbounded far-field soil is represented by the dynamic infinite elements in the frequency domain. Since this method directly models the fluid-structure-soil interaction systems, it can be applied to the dynamic analysis of a 2-D liquid storage structure with complex geometry. Finally, results of seismic analyses are presented for a spent fuel storage tank embedded in a layered half-space and a massive concrete dam on a layered half-space.

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투입노력 양에 기반한 소프트웨어 유지보수 비용산정 모형 (A Software Maintenance Cost Estimation Model based on Real Maintenance Efforts)

  • 정은주;유천수
    • Journal of Information Technology Applications and Management
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    • 제19권2호
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    • pp.181-196
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    • 2012
  • The cost of software maintenance occupies about two thirds in the software lifecycle. However, it is not easy to estimate the cost of software maintenance because of various viewpoints about software maintenance, unclear estimation methods, and complex procedures. Until now, the cost estimation model has used compensation factors for software characteristic and environment on the basis of program size. Especially, most of existing models use maintenance rate of total software cost as a main variable. This paper suggests the software maintenance cost estimation model that uses the result of calculating real maintenance efforts. In this paper, we classify functional maintenance and non-functional maintenance as software maintenance activity type. For functional maintenance, present function point of target software is needed to evaluate. The suggested maintenance cost evaluation model is applied to a software case in public sector. This paper discusses some differences between our model and other modes.

운동방정식을 기저로 한 스튜워트 플랫폼 운동장치의 제어시스템 설계 및 슬라이딩 모드제어 (Model-Based Control System Design and Sliding Mode Control of Stewart Platform Manipulator)

  • 이종원;김낙인
    • 대한기계학회논문집A
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    • 제23권6호
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    • pp.903-911
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    • 1999
  • A high speed tracking control system for 6-6 Stewart platform manipulator is designed for performing the model based joint-axis sliding mode control. Because of the complex dynamics and kinematics of the Stewart platform manipulator, two computer systems, consisting of a PC and a DSP, are adopted, so that real time tasks are run in synchronous and asynchronous modes. It is experimentally proven that the proposed control system makes the convenience in implementation of model based tracking control, so that it can achieve effective tracking control under relatively high speed and additional payload conditions.

Efficient Aerodynamic Computation of a Wing Model Considering Body Effect for the Aeroelastic Application

  • Lee, Seung-Jun;Im, Dong-Kyun;Lee, In
    • International Journal of Aeronautical and Space Sciences
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    • 제10권1호
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    • pp.14-19
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    • 2009
  • The typical aeroelastic analysis for a complex configuration such as a complete aircraft was done using the aerodynamic results of the wing and the structural modes of a complete aircraft; that is, the aerodynamics of a wing of a complete aircraft is assumed to be not much influenced by the body shape. Nevertheless, the body shape can cause a distortion of aerodynamic pressure on the wing surface and it is necessary to investigate the body effect in flutter analysis. In this reseasrch, MGM inverse design method is applied to include the body effect of a wing-body model which disturbs the pressure distribution on the wing surface.

소형내연기관축계의 비틀림진동댐퍼에 관한 연구 제1보 최적점성.고무탄성댐퍼의 개발 (A Study on the Torsional Vibration Damper of the Small Internal Combustion Engine Driving System(Part I) - Development of the Optimum Viscous-Rubber Damper-)

  • 전효중;김유종;김의간;김동혁
    • Journal of Advanced Marine Engineering and Technology
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    • 제15권2호
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    • pp.44-52
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    • 1991
  • The crankshaft system of engine is a complex vibratory object and its vibration modes are consisted of torsional, axial and their coupled vibration. Among them, the torsional vibration causes engine noise as well as serious fatigue faillures of crankshaft. If the troules of noises and crankshaft strength are forecasted by torsional vibration calculation in the design atage of crankshaft, the torsional damper is adopted as the final countermeasure. In this paper, some computer program to calculate crankshaft torsional vibration of engine are developed and with developed programs, an efficient rubber-viscous damper for automobile and with developed programs, an efficient rubber-viscous damper for automobile engine is designed and manufactured, and then it is fitted on the actual automobile engine to confirm its calculated efficiency. By comparing the measured result (with damper and without damper) with the calculated one, the reliability of developed computer programs and the performances of manufactured damper are confirmed.

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지능판의 진동제어를 위한 수동구속감쇠의 위치 설정 (Placement of passive Constrained Layer Damping for Vibration Control of Smart Plate)

  • 강영규;김찬묵
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 추계학술대회논문집
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    • pp.12-16
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    • 2002
  • Dynamic characteristics of smart laminated composite plates with passive constrained layer damping have been investigated to design structure with maximum possible damping capacity. The equations of motion are derived for flexural vibrations of symmetrical, multi-layer laminated plates. The damping ratio and modal damping of the first bending and torsional modes are calculated by means of iterative complex eigensolution method. The structural damping index(SDI) is introduced to determine the optimum placement of viscoelastic patch. This paper addresses a design strategy of laminated composite plate under vibrations.

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회전자유도 보간에 의한 모드합성법 (Modal Synthesis Method Using Interpolated Rotational DOF)

  • 장경진;지태한;박영필
    • 소음진동
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    • 제5권4호
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    • pp.503-514
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    • 1995
  • In the case of performing experimental modal analysis(EMA) and finite- element analysis(EFA) for a whole structure of automotive body that is composed of many complex parts, a trouble may arise from the calculation time, the capacity of memory in computers and the experimental conditions, etc. In this paper, for the vibrational analysis of automotive body model, the efficient modal synthesis method by means of dividing the whole structure into two parts and performing EMA and FEA for each part is studied. In addition, the method based on Lagrange interpolation is proposed for approximating rotational degrees-of-freedom information and linking FEA with EMA. In result, by measuring translational degrees-of-freedom information of only few points and adopting only few modes, the linking method based on Lagrange interpolation turned out to be efficient and accurate in the low frequency range.

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Power System Nonlinearity Modal Interaction by the Normal Forms of Vector Fields

  • Zhang, Jing;Wen, J.Y.;Cheng, S.J.
    • Journal of Electrical Engineering and Technology
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    • 제3권1호
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    • pp.8-13
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    • 2008
  • Because of the robust nonlinear characteristics appearing in today's modern power system, a strong interaction exists between the angle stability and the voltage stability, which were conventionally studied insularly. However, as the power system is a complex unified system, angle instability always happens in conjunction with voltage instability. The authors propose a novel method to analyze this type of stability problem. In the proposed method, the theory of normal forms of vector fields is utilized to treat the auxiliary dynamic system. By use of this method, the interaction between response modes caused by the nonlinearity of the power system can be analyzed. Consequently, the eigenvalue analysis method is extended to cope with performance analysis of the power system with heavy nonlinearity. The effectiveness of the proposed methodology is verified on a 3-bus power system.

Parametric study on equivalent damping ratio of different composite structural building systems

  • Farghaly, Ahmed Abdelraheem
    • Steel and Composite Structures
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    • 제14권4호
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    • pp.349-365
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    • 2013
  • Structures consisting of concrete and steel parts, which are irregular in damping ratios are investigated. This investigation is a code-based seismic design of such structures. Several practical difficulties encountered, due to inherent differences in the nature of dynamic response of each part, and the different damping ratios of the two parts. These structures are irregular in damping ratios and have complex modes of vibration so that their analysis cannot be handled with the readily available commercial software. Therefore, this work aims to provide simple yet sufficiently accurate constant values of equivalent damping ratios applied to the whole structure for handling the damping irregularity of such structures. The results show that the equivalent damping ratio changes with the height of the building and the kind of the structural system, but it is constant for all accelerations values. Thus, available software SAP2000 applied for seismic analysis, design and the provisions of existing seismic codes. Finally, evaluation of different kinds of structural system used in this research to find the most energy dissipating one found by finding the best value of quality coefficient.

마찰재 접촉강성에 따른 디스크 브레이크 진동모드 형상화 (Mode Shape Variation of Disc Brake with Respect to Contact Stiffness Variation)

  • 강재영
    • 한국자동차공학회논문집
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    • 제18권3호
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    • pp.127-132
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    • 2010
  • Eigensolutions associated with self-excited vibration of disc brake system can be obtained by complex eigenvalue analysis. The eigenvalue sensitivity to change in contact stiffness can be used to demonstrate stability criteria and eigenvalue veering. Dynamic instability on eigenvalue loci with respect to the variation of contact stiffness is found to be related to mode interaction between two adjacent modes. This modal interaction can be effectively shown by mode shape visualization. This paper presents the methodology to construct the mode shape of disc brake system where a disc and two brake pads are coupled with contact stiffness.