• Title/Summary/Keyword: numerical oscillation

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A comparative study of galloping cable and torsional oscillations in suspension bridge (갤럽핑 케이블과 현수교의 뒤틀린 진동에 관한 비교 연구)

  • Hyeyoung Oh
    • Journal of the Korea Computer Industry Society
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    • v.5 no.3
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    • pp.355-362
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    • 2004
  • This paper presents the common and different results between the galloping cable and torsional oscillations in suspension bridge. Numerical results of the galloping cable and torsional oscillations in suspension bridge are presented by using the second-order Runge Kutta method under the initial conditions. This paper shows that large amplitude solution can coexist with the small amplitude one as the frequency and amplitude of the oscillation change. The differences in symmetry and transient effects are presented.

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UNSTEADY SUPERSONIC INLET DIFFUSER FLOWS WITH SINUSOIDAL PRESSURE OSCILLATIONS

  • Jong Yun Oh
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1996.11a
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    • pp.107-116
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    • 1996
  • Numerical simulations have been conducted to characterize unsteady flow structures in an axisymmetric supersonic inlet diffuser with sinusoidal pressure oscillations at the diffuser exit. The formulation is based on the unsteady Navier-Stokes equations and turbulence closure is achieved using a two-layer model with a too-Reynolds-number scheme for the near-wall treatment. The governing equations are formulated in an integral form, and are discretized by the four-stage Runge-Kutta scheme for temporal terms and the Harten-Yee upwind TVD scheme for convective terms. Results indicated that the inlet shock characteristics are significantly modified by acoustic oscillations originating from the combustor. The characteristics of shock/boundarv-layer interactions (such as the size of separation bubble, terminal shock shape, and vorticity intensity) are also greatly iufluenced by the shock oscillation due to acoustic waves.

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Evaluation of torsional natural frequencies for non-tubular bonded joints

  • Pugno, Nicola;Ruotolo, Romualdo
    • Structural Engineering and Mechanics
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    • v.13 no.1
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    • pp.91-101
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    • 2002
  • During the last several years, research activity on non-tubular bonded joints has concentrated on the effects of normal stress, bending moments and shear. Nevertheless, in certain situations, the structure may be subjected to twisting moments, so that the evaluation of its dynamic behaviour to torsional vibrations becomes of great importance even though evaluations of such loading conditions is entirely lacking in the literature. The aim of this article is to show that torsional natural frequencies of the non-tubular joint can be evaluated by determining the roots of a determinantal equation, derived by taking advantage of some analytical results obtained in a previous paper dealing with the analysis of the state of stress in the adhesive. Numerical results related to clamped-free and clamped-clamped joints complete the article.

Effect of Pressure on Acoustic Pressure Response and NO Formation in Diluted Hydrogen-Air Diffusion Flames (희석된 수소-공기 확산 화염에서 음향파 응답과 NO 생성에 미치는 압력의 영향)

  • Sohn, Chae-Hoon;Chung, Suk-Ho
    • 한국연소학회:학술대회논문집
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    • 1999.10a
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    • pp.11-20
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    • 1999
  • Acoustic pressure response and NO formation of hydrogen-air diffusion flames at various pressures are numerically studied by employing counterflow diffusion flame as a model flame let in turbulent flames in combustion chambers. The numerical results show that extinction strain rate increases linearly with pressure and then decreases, and increases again at high pressures. Thus, flames are classified into three pressure regimes. Such non-monotonic behavior is caused by the change in chemical kinetic behavior as pressure rises. Acoustic pressure response in each regime is investigated based on the Rayleigh criterion. At low pressures, pressure-rise causes the increase in flame temperature and chain branching/recombination reaction rates, resulting in increased heat release. Therefore, amplification in pressure oscillation is predicted. Similar phenomena are predicted at high pressures. At moderate pressures, weak amplification is predicted. Emission index of NO shows similar behaviors as to the peak-temperature variation with pressure.

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Numerical Modelling of Weak Oscillation Phenomena in RF Repeaters (RF중계기 미세발진현상의 수치적 모델링)

  • Lee Hak-Yong;Song Seung-Joon;Lee Hong-Bae
    • 한국정보통신설비학회:학술대회논문집
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    • 2002.08a
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    • pp.43-45
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    • 2002
  • 이동통신 무선망 설계 시에는 전파강도가 부족하여 발생하는 부분적인 음영지역을 해결하기 위해서 기지국 신호를 재증폭하는 중계기를 이용하게 된다. 이러한 중계기는 입출력 안테나 사이에 충분한 격리도를 확보하지 않으면 증폭된 출력신호가 입력단으로 유입되어 시스템 발진현상이 발생하게 된다. 격리도에 따라 신호의 신호대잡음비를 저하시키는 수준의 미세발진이 발생하거나 출력증폭기의 한계점에 도달시키는 완전발진이 발생 된다. 기지국에 입력된 신호를 복조하여 신호의 상태에 따라 단말기 출력을 증가시키도록 제어하는 상황에서 이러한 중계기의 발진현상은 시스템 성능의 현저한 저하를 가져오게 된다. 본 논문에서는 실험적으로 발견된 중계기 발진현상을 수학적 모델링을 통하여 중계기의 특성 및 입출력 안테나 사이의 격리도와 미세발진현상과의 관계를 규명한다. 아울러 실험결과와의 비교분석을 통하여 본 논문에서 제시한 모델링의 타당성을 증명한다.

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Active Random Noise Control using Adaptive Learning Rate Neural Networks

  • Sasaki, Minoru;Kuribayashi, Takumi;Ito, Satoshi
    • 제어로봇시스템학회:학술대회논문집
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    • 2005.06a
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    • pp.941-946
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    • 2005
  • In this paper an active random noise control using adaptive learning rate neural networks is presented. The adaptive learning rate strategy increases the learning rate by a small constant if the current partial derivative of the objective function with respect to the weight and the exponential average of the previous derivatives have the same sign, otherwise the learning rate is decreased by a proportion of its value. The use of an adaptive learning rate attempts to keep the learning step size as large as possible without leading to oscillation. It is expected that a cost function minimize rapidly and training time is decreased. Numerical simulations and experiments of active random noise control with the transfer function of the error path will be performed, to validate the convergence properties of the adaptive learning rate Neural Networks. Control results show that adaptive learning rate Neural Networks control structure can outperform linear controllers and conventional neural network controller for the active random noise control.

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Dry friction losses in axially loaded cables

  • Huang, Xiaolun;Vinogradov, Oleg G.
    • Structural Engineering and Mechanics
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    • v.4 no.3
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    • pp.330-344
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    • 1996
  • A model of a cable comprising interacting wires with dry friction forces at the interfaces is subjected to a quasi-static cyclic loading. The first cycle of this process, comprising of axial loading, unloading and reloading is investigated analytically. Explicit load-elongation relationships are obtained for all of the above phases of the cycle. An expression for the hysteretic losses is also obtained in an explicit form. It is shown that losses are proportional to the third power of the amplitude of the oscillating axial force, and are in inverse proportion to the interwire friction forces. The results obtained are used to introduce a model of a cable as a solid rod with an equivalent stiffness and damping properties of the rod material. It is shown that the stiffness of the equivalent rod is weakly nonlinear, whereas the viscous damping coefficient is proportional to the amplitude of the oscillation. Some numerical results illustrating the effect of cable parameters on the losses are given.

Numerical Study for Mixing Characteristics of an Oscillating Micro-stirrer (미소진동교반기의 혼합특성에 대한 수치적 연구)

  • Kim, Yong-Dae;Maeng, Joo-Sung
    • 유체기계공업학회:학술대회논문집
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    • 2006.08a
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    • pp.309-312
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    • 2006
  • Effective mixing is an important problem in microfluidics for chemical and biomechanical applications. In this study, the influences of the Reynolds number and the oscillating frequency on mixing characteristics of micro-stirrer are studied in a microchannel with single stirrer. The influence of fluid inertial effects in an active mixer is first discussed. It is found that the stirring effects by stirrer oscillation are promptly attenuated at low Reynolds number, which makes greatly difficult the rapid mixing. As the inertial effects are increased, the chaotic advection is generated and then developed. The mixing phase is finally developed some mushroom shaped structure. And the mixing efficiency is also studied as a function of the oscillating frequency. We found that the mixing efficiency does not always increase with higher oscillating frequency of stirrer. Consequently, we found the functional relation between the optimal frequency of a stirrer and the Reynolds number.

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Wet etching charicteristics of InP in InP/InGaAs HBTs and their fabrication (InP의 습식식각특성과 InP/lnGaAs HBT의 제작)

  • 김강대;박재홍;김용규;황성범;송정근
    • Proceedings of the IEEK Conference
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    • 2002.06b
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    • pp.77-80
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    • 2002
  • In this paper, InP-based HBTs have been optimally designed by numerical simulation and fabricated by the self-aligned process. The structure of HBT was designed in terms of the current gain*f$_{max}$ for the base and f$_{T}$*f$_{max}$ for the collector. The designed structure produced the current gain of about 50 and the cutoff frequency and the maximum oscillation frequency of 87GHz and 2940Hz respectively. In addition, we present a study of the vertical and lateral etching of InP with the mask sides parallel to the principal crystallographic axes, [0101 and (001). This etching characteristics arc used to fabricate self-aligned HBT structures with reduced parasitic effects.s.s.s.

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NUMERICAL STUDY OF MODULATED TAYLOR-COUETTE FLOW (진동하는 Taylor-Couette 유동에 대한 수치적 연구)

  • Kang, Chang-Woo;Yang, Kyung-Soo;Mutabazi, Innocent
    • Journal of computational fluids engineering
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    • v.15 no.4
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    • pp.32-39
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    • 2010
  • In this study, we consider Taylor-Couette flow with the outer cylinder at rest and the inner one oscillating with a mean angular velocity. Varying the mean angular velocity, amplitude and frequency of the oscillation, we investigate the characteristics of modulated Taylor vortices. At a constant mean angular velocity, Taylor vortices intensify as the amplitude increases and frequency decreases. The axial wavenumber is calculated by spectral analysis. When the frequency varies, the axial wavenumber does not change at a constant mean angular velocity and amplitude. But, the axial wavenumber increases, as the mean angular velocity increases.