• 제목/요약/키워드: nonlinear vibration response

검색결과 373건 처리시간 0.028초

강도한계 이선형 단자유도 시스템의 비탄성 변위비 (Inelastic Displacement Ratio for Strength-limited Bilinear SDF Systems)

  • 한상환;이태섭;석승욱
    • 한국지진공학회논문집
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    • 제14권4호
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    • pp.23-28
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    • 2010
  • 본 연구는 철골 모멘트 골조의 이력거동을 잘 나타내는 강도한계 이선형 단자유도 시스템에 대하여 지반조건, 후탄성 기울기, 감쇠비, 항복강도 저감계수, 고유주기 등의 변화가 비탄성변위비에 미치는 영향을 분석하였다. NEHRP의 기준에 따라 B(보통암지반), C(매우 조밀한 토사지반), D(단단한 토사지반)의 지반조건에 해당하는 총 240개의 지진 가속도에 대하여 비선형 시간이력 해석을 수행하였다. 본 연구에서는 비탄성 거동 하에서 P-$\Delta$ 효과를 반영할 수 있도록 음강성비를 -0.1 에서 -0.5까지 고려하였다. 비선형 회귀분석을 통하여 감쇠비 2%, 5%, 10%, 20%에 대한 강도한계 이선형 모델의 비탄성 변위비와 로그표준편차식을 제안하였다.

Influence of lateral motion of cable stays on cable-stayed bridges

  • Wang, P.H.;Liu, M.Y.;Huang, Y.T.;Lin, L.C.
    • Structural Engineering and Mechanics
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    • 제34권6호
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    • pp.719-738
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    • 2010
  • The aim of this paper concerns with the nonlinear analysis of cable-stayed bridges including the vibration effect of cable stays. Two models for the cable stay system are built up in the study. One is the OECS (one element cable system) model in which one single element per cable stay is used and the other is MECS (multi-elements cable system) model, where multi-elements per cable stay are used. A finite element computation procedure has been set up for the nonlinear analysis of such kind of structures. For shape finding of the cable-stayed bridge with MECS model, an efficient computation procedure is presented by using the two-loop iteration method (equilibrium iteration and shape iteration) with help of the catenary function method to discretize each single cable stay. After the convergent initial shape of the bridge is found, further analysis can then be performed. The structural behaviors of cable-stayed bridges influenced by the cable lateral motion will be examined here detailedly, such as the static deflection, the natural frequencies and modes, and the dynamic responses induced by seismic loading. The results show that the MECS model offers the real shape of cable stays in the initial shape, and all the natural frequencies and modes of the bridge including global modes and local modes. The global mode of the bridge consists of coupled girder, tower and cable stays motion and is a coupled mode, while the local mode exhibits only the motion of cable stays and is uncoupled with girder and tower. The OECS model can only offers global mode of tower and girder without any motion of cable stays, because each cable stay is represented by a single straight cable (or truss) element. In the nonlinear seismic analysis, only the MECS model can offer the lateral displacement response of cable stays and the axial force variation in cable stays. The responses of towers and girders of the bridge determined by both OECS- and MECS-models have no great difference.

고층 철근콘크리트 건축구조모델의 지진응답에 대한 해석적 모사 (Analytical Simulation of the Seismic Response of a High-Rise RC Building Model)

  • 이한선;이정재;정동욱
    • 한국지진공학회논문집
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    • 제12권5호
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    • pp.1-10
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    • 2008
  • Taft N21E 지진파를 사용하여 1:12 축소된 모델로 여러번의 진동대 실험을 저층부 2개층에 비틀림과 연층을 가지는 17층 고층 철근콘크리트 건물에 대해 지진 거동을 조사하기 위해 수행했었다. 이 거동의 주요 특징은 (1) 연약 골조가 거대한 비탄성 변형을 받은 후 변형이나 비틀림에서 비틀림 모드까지 현저한 진동의 갑작스런 변화, (2) 이러한 모드 변화에 따른 비틀림 강성의 갑작스런 증가, (3) 비틀림 모드에서 월의 요곡(warping) 거동, 그리고 (4) 진동대 거동의 반대 방향에만 생기는 전도모멘트 양상을 보여주었다. 본 연구에서는 이러한 성과를 Perform3D라는 비선형 해석 프로그램을 사용하여 위 특성을 모사하기 위해 노력하였다. 이 소프트웨어에서 가용한 비선형 모델과 함께 그의 장점과 단점을 해석 및 실험 결과의 비교를 통해 제시하였다.

The effect of composite-elastomer isolation system on the seismic response of liquid-storage tanks: Part I

  • Shahrjerdi, A.;Bayat, M.
    • Earthquakes and Structures
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    • 제15권5호
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    • pp.513-528
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    • 2018
  • A typical viable technique to decrease the seismic response of liquid storage tanks is to isolate them at the base. Base-isolation systems are an efficient and feasible solution to reduce the vulnerability of structures in high seismic risk zones. Nevertheless, when liquid storage tanks are under long-period shaking, the base-isolation systems could have different impacts. These kinds of earthquakes can damage the tanks readily. Hence, the seismic behaviour and vibration of cylindrical liquid storage tanks, subjected to earthquakes, is of paramount importance, and it is investigated in this paper. The Finite Element Method is used to evaluate seismic response in addition to the reduction of excessive liquid sloshing in the tank when subjected to the long-period ground motion. The non-linear stress-strain behaviour pertaining to polymers and rubbers is implemented while non-linear contact elements are employed to describe the 3-D surface-to-surface contact. Therefore, Nonlinear Procedures are used to investigate the fluid-structure interactions (FSI) between liquid and the tank wall while there is incompressible liquid. Part I, examines the effect of the flexibility of the isolation system and the tank aspect ratio (height to radius) on the tank wall radial displacements of the tank wall and the liquid sloshing heights. Maximum stress and base shear force for various aspect ratios and different base-isolators, which are subjected to three seismic conditions, will be discussed in Part II. It is shown that the composite-base isolator is much more effective than other isolators due to its high flexibility and strength combined. Moreover, the base isolators may decrease the maximum level pertaining to radial displacement.

Three-dimensional dynamics of vortex-induced vibration of a pipe with internal flow in the subcritical and supercritical regimes

  • Duan, Jinlong;Chen, Ke;You, Yunxiang;Wang, Renfeng;Li, Jinlong
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제10권6호
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    • pp.692-710
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    • 2018
  • The Three-dimensional (3-D) dynamical behaviors of a fluid-conveying pipe subjected to vortex-induced vibration are investigated with different internal flow velocity ${\nu}$. The values of the internal flow velocity are considered in both subcritical and supercritical regimes. During the study, the 3-D nonlinear equations are discretized by the Galerkin method and solved by a fourth-order Runge-Kutta method. The results indicate that for a constant internal flow velocity ${\nu}$ in the subcritical regime, the peak Cross-flow (CF) amplitude increases firstly and then decrease accompanied by amplitude jumps with the increase of the external reduced velocity. While two response bands are observed in the In-line (IL) direction. For the dynamics in the lock-in condition, 3-D periodic, quasi-periodic and chaotic vibrations are observed. A variety of CF and IL responses can be detected for different modes with the increase of ${\nu}$. For the cases studied in the supercritical regime, the dynamics shows a great diversity with that in the subcritical regime. Various dynamical responses, which include 3-D periodic, quasi-periodic as well as chaotic motions, are found while both CF and IL responses are coupled while ${\nu}$ is beyond the critical value. Besides, the responses corresponding to different couples of ${\mu}_1$ and ${\mu}_2$ are obviously distinct from each other.

난류 경계층 모델을 고려한 AGARD 445.6 날개의 플러터 해석 및 실험결과 비교 (Comparison Study of Viscous Flutter Boundary for the AGARD 445.6 Wing Using Different Turbulent Boundary Layer Models)

  • 김요한;김동현;김동만;김수현
    • 한국군사과학기술학회지
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    • 제12권6호
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    • pp.704-710
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    • 2009
  • In this study, a comparison study of flutter analysis for the AGARD 445.6 wing with wind turnnel test data has been conducted in the subsonic, transonic and supersonic flow regions. Nonlinear aeroelastic using FSIPRO3D which is a generalized user-friendly fluid-structure analyses have been conducted for a 3D wing configuration considering shockwave and turbulent viscosity effects. The developed fluid-structure coupled analysis system is applied for aeroelastic computations combining computational structure dynamics(CSD), finite element method(FEM) and computations fluid dynamics(CFD) in the time domain. MSC/NASTRAN is used for the vibration analysis of a wing model, and then the result is applied to the FSIPRO3D module. the results for dynamic aeroelastic response using different turbulent models are presented for several Mach numbers. Calculated flutter boundary are compared with the wind-tunnel experimental and the results show very good agreements.

Simplified procedure for seismic analysis of base-isolated structures

  • Serror, Mohammed H.;El-Gazzar, Sherif O.;Mourad, Sherif A.
    • Earthquakes and Structures
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    • 제8권5호
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    • pp.1091-1111
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    • 2015
  • Base isolation is an effective method for protecting structures against earthquake hazard. It elongates the period of vibration and introduces supplemental damping to the structural system. The stiffness, damping and displacement are coupled forcing the code seismic design procedure to be unnecessarily complicated. In addition, the force reduction factor -a key parameter in the design procedurehas not been well addressed by seismic design codes at the high levels of damping due to the pronounced difference between pseudo and actual accelerations. In this study, a comparison has been conducted to evaluate eight different methods, in the literature, for calculating the force reduction factor due to damping. Accordingly, a simplified seismic analysis procedure has been proposed based on the well documented N2 method. Comprehensive analysis has been performed for base-isolated structure models for direct application and verification of the proposed procedure. The results have been compared with those of the European code EC8, the nonlinear time history analysis and investigations in the literature, where good agreement has been reported. In addition, a discussion has been elaborated for the resulted response of the base-isolated structure models with respect to the dynamic characteristics of the base isolation system.

유압 인버터 엘리베이터를 위한 부하 보상 및 속도 제어기 (Load compensation and Speed Controller for Hydraulic Inverter-fed Elevator)

  • 한상수
    • 전자공학회논문지
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    • 제51권2호
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    • pp.163-167
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    • 2014
  • 유압 인버터 엘리베이터의 비선형성과 유압 펌프의 누유량으로 인한 진동 및 속도 편차를 줄이기 위한 부하 보상 및 속도 제어기를 제안하였다. 부하보상 제어기는 PI제어기로 구성하였으며 속도제어기는 PID 제어기를 이용하여 구성하였다. 제어기 제어 변수 이득은 시스템 전달함수의 주파수 응답 방법을 이용하였다. 제안한 제어기의 효용성은 실험을 통해 입증하였고 실험 결과 제안한 제어기는 부하 변동에 강인하고 비선형인 유압 엘리베이터 시스템에 안정하고 좋은 속도 및 가속도 응답 특성을 갖는다.

Performance evaluation of smart prefabricated concrete elements

  • Zonta, Daniele;Pozzi, Matteo;Bursi, Oreste S.
    • Smart Structures and Systems
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    • 제3권4호
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    • pp.475-494
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    • 2007
  • This paper deals with the development of an innovative distributed construction system based on smart prefabricated concrete elements for the real-time condition assessment of civil infrastructure. So far, two reduced-scale prototypes have been produced, each consisting of a $0.2{\times}0.3{\times}5.6$ m RC beam specifically designed for permanent instrumentation with 8 long-gauge Fiber Optic Sensors (FOS) at the lower edge. The sensing system is Fiber Bragg Grating (FBG)-based and can measure finite displacements both static and dynamic with a sample frequency of 625 Hz per channel. The performance of the system underwent validation in the laboratory. The scope of the experiment was to correlate changes in the dynamic response of the beams with different damage scenarios, using a direct modal strain approach. Each specimen was dynamically characterized in the undamaged state and in various damage conditions, simulating different cracking levels and recurrent deterioration scenarios, including cover spalling and corrosion of the reinforcement. The location and the extent of damage are evaluated by calculating damage indices which take account of changes in frequency and in strain-mode-shapes. The outcomes of the experiment demonstrate how the damage distribution detected by the system is fully compatible with the damage extent appraised by inspection.

3-블레이드 회전익 항공기에서 기하학적 정밀 보의 공탄성 모델을 이용한 무베어링 로터의 자이로스코픽 세차 진동 제어

  • 임병욱;김용세;신상준
    • EDISON SW 활용 경진대회 논문집
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    • 제6회(2017년)
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    • pp.270-281
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    • 2017
  • 본 논문에서는 헬리콥터 블레이드에서 발생하는 자이로스코픽 세차 진동에 대해 연구하고, 능동 제어기 설계를 통하여 진동 저감 시뮬레이션을 수행한다. 이를 위해, 헬리콥터의 전진 비행시 동역학적 응답을 외팔보 조건을 갖는 회전익의 해석이 가능한 EDISON의 기하학적 정밀 보 구조동역학 프로그램을 이용하여 구조 해석을 진행하고 이를 단순 공기력 모델과 연성하여 공탄성 해석을 수행하였다. 실시간 구조 응답을 구하기 위해 EDISON 프로그램 해석 결과를 비선형 수식으로 모델링하는 기법과 트림해석에는 Newton-Raphson 기법 등이 사용되었다.

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