• 제목/요약/키워드: Oscillation criterion

검색결과 35건 처리시간 0.022초

수소/공기 대향류 확산화염의 비선형 음향파 응답특성에 관한 연구 (Nonlinear Acoustic-Pressure Responses of H2/Air Counterflow Diffusion Flames)

  • 김홍집;정석호;손채훈
    • 대한기계학회논문집B
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    • 제27권8호
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    • pp.1158-1164
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    • 2003
  • Steady-state structure and acoustic-pressure responses of $H_2$/Air counterflow diffusion flames are studied numerically with a detailed chemistry in view of acoustic instability. The Rayleigh criterion is adopted to judge acoustic amplification or attenuation from flame responses. Steady-state flame structures are first investigated and flame responses to various acoustic-pressure oscillations are numerically calculated in near-equilibrium and near-extinction regimes. The acoustic responses of $H_2$/Air flame show that the responses in near-extinction regime always contribute to acoustic amplification regardless of acoustic-oscillation frequency Flames near extinction condition are sensitive to pressure perturbation and thereby peculiar nonlinear responses occur, which could be a possible mechanism in generating the threshold phenomena observed in combustion chamber of propulsion systems.

Hybrid RANS/LES 방법을 이용한 이음속 공동 유동의 수치적 모사 (Hybrid RANS/LES Simulation of Subsonic Cavity Flow)

  • 장경식;박승오;최석기
    • 한국전산유체공학회지
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    • 제9권2호
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    • pp.23-29
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    • 2004
  • A numerical simulation of an incompressible cavity flow is conducted using the hybrid turbulence model. The model adopted is a modified type of DES using k- ε two-equation model. Cavity geometry and flow condition are based on Cattafesta's experiment. Computational results are compared with the results of Cattafesta's experiment. The simulation successfully predicts the oscillatory features and the Strouhal number of the oscillation compares very favorably with that of the dominant mode of experimental data. Vorticity contours obtained from the simulation data are consistent with the smoke visualization of the Cattafesta's experiment. The coherent structures of cavity flow are also investigated using Q criterion.

발진 이론에 근거한 유도결합형 방전광원의 안정기 설계에 관한 연구 (A Study on the Ballast Design of a Inductively Coupled Plasma Light Source based on Oscillation Theory)

  • 김철진;임연찬
    • 전기학회논문지
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    • 제58권6호
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    • pp.1110-1115
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    • 2009
  • We studied on the design of electrical parameters for ICP(Inductively Coupled Plasma) light sources which can be effective to improve the electrical power efficiency of it. These parameters were derivated from Barkhausen theory about the oscillating condition of a ballaster. The relationships of $f-I_p$ and f-n were calculated theoretically and then these relationships were compared with the measured results about $I_p$ and power depending to a discharge length(l) of ICP light source. Finally, we can see that a specific range of induced current depending to a discharge length would be necessary to minimize the change of magnetization inductance and driving frequency at driving.

Aeroelastic analysis of bridges using FEM and moving grids

  • Selvam, R. Panneer;Govindaswamy, S.;Bosch, Harold
    • Wind and Structures
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    • 제5권2_3_4호
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    • pp.257-266
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    • 2002
  • In the recent years flow around bridges are investigated using computer modeling. Selvam (1998), Selvam and Bosch (1999), Frandsen and McRobie (1999) used finite element procedures. Larsen and Walther (1997) used discrete vorticity procedure. The aeroelastic instability is a major criterion to be checked for long span bridges. If the wind speed experienced by a bridge is greater than the critical wind speed for flutter, then the bridge fails due to aeroelastic instability. Larsen and Walther (1997) computed the critical velocity for flutter using discrete vortex method similar to wind tunnel procedures. In this work, the critical velocity for flutter will be calculated directly (free oscillation procedure) similar to the approaches reported by Selvam et al. (1998). It is expected that the computational time required to compute the critical velocity using this approach may be much shorter than the traditional approach. The computed critical flutter velocity of 69 m/s is in reasonable comparison with wind tunnel measurement. The no flutter and flutter conditions are illustrated using the bridge response in time.

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

  • 손채훈;정석호
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 1999년도 제19회 KOSCO SYMPOSIUM 논문집
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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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유전 알고리즘을 이용한 전력시스템 안정화 장치의 최적 파라미터 선정 (Optimal Parameter Selection of Power System Stabilizer using Genetic Algorithm)

  • 정형환;왕용필;정동일;정문규
    • 대한전기학회논문지:전력기술부문A
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    • 제48권6호
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    • pp.683-691
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    • 1999
  • In this paper, it is suggested that the selection method of optimal parameter of power system stabilizer(PSS) with robustness in low frequency oscillation for power system using Real Variable Elitism Genetc Algorithm(RVEGA). The optimal parameters were selected in the case of power system stabilizer with one lead compensator, and two lead compensator. Also, the frequency responses characteristic of PSS, the system eigenvalues criterion and the dynamic characteristic were considered in the normal load and the heavy load, which proved usefulness of RVEGA compare with Yu's compensator design theory.

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분산전원을 고려한 적응적 재폐로 기법 (An Adaptive Reclosing Technique Considering the Distributed Generation)

  • 서훈철;김철환;여상민
    • 전기학회논문지
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    • 제56권2호
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    • pp.227-232
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    • 2007
  • The autoreclosing is applied to power system for maintaining system stability and continuity of supply. Developments on distributed generation(DG) grows significantly by environmental issues and economical issues. If the DG is connected to distribution system, the DG influences the technical aspects such as power quality, protection and stability. It causes the challenges to protection, especially to reclosing. In order to achieve reliability and safety of the distribution system, the rules and guidelines suggest that the DG units should be rapidly disconnected from the network before the reclosing. If the DG is disconnected whenever the fault occurs, it cannot be utilized effectively. This paper presents the adaptive reclosing algorithm considering the DG. The algorithm consists of angle oscillation's judgment, EEEAC(Emergency Expanded Equal-Area Criterion), calculation of optimal reclosing time and re-connection algorithm. The simulation is implemented for the DG technology by using EMTP MODELS. The simulation results show that the transient stability is maintained and the DG is protected against disturbance.

플랩핑 에어포일에 대한 비틀림 유연성의 영향 (Effects of Torsional Flexibility on a Flapping Airfoil)

  • 조문성;배재성;김학봉;김우진
    • 한국항공우주학회지
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    • 제36권12호
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    • pp.1146-1151
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    • 2008
  • 본 연구에서는 플래핑 운동하는 에어포일에 대한 비틀림 유연성의 영향을 조사하였다. 비틀림 유연성이 있는 에어포일의 공기력은 2차원 비정상 와류 패널 방법을 이용하여 계산하였다. 플래핑 에어포일의 공탄성 해석을 위해 2차원의 typical section 모델이 사용되었다. 주요한 파라미터로서 비틀림 유연성과 가진주파수가 고려되었다. 인 무거운 에어포일 조건에서는 주파수비가 0.75 부근에서 추력 최대점이 발견되었다. 이 추력치를 경계로 두 가지 다른 운동이 관찰되었으며, 하나는 관성 지배 운동(inertia driven deformation motion)이고, 다른 하나는 진동 지배 운동(oscillation driven deformation motion)이다. 또한, 최대 추력 상태에서는 비틀림 유연성과 가진주파수에 관계없이 위상각이 85도를 유지하였다.

Galloping of steepled main cables in long-span suspension bridges during construction

  • An, Yonghui;Wang, Chaoqun;Li, Shengli;Wang, Dongwei
    • Wind and Structures
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    • 제23권6호
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    • pp.595-613
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    • 2016
  • Large amplitude oscillation of steepled main cables usually presents during construction of a long-span bridge. To study this phenomenon, six typical main cables with different cross sections during construction are investigated. Two main foci have been conducted. Firstly, aerodynamic coefficients of a main cable are obtained and compared through simulation and wind tunnel test: (1) to ensure the simulation accuracy, influences of the numerical model's grid size, and the jaggy edges of main cable's cross section on main cable's aerodynamic coefficients are investigated; (2) aerodynamic coefficients of main cables at different wind attack angles are obtained based on the wind tunnel test in which the experimental model is made by rigid plastic using the 3D Printing Technology; (3) then numerical results are compared with wind tunnel test results, and they are in good agreement. Secondly, aerodynamic coefficients of the six main cables at different wind attack angles are obtained through numerical simulation. Then Den Hartog criterion is used to analyze the transverse galloping of main cables during construction. Results show all the six main cables may undergo galloping, which may be an important reason for the large amplitude oscillation of steepled main cables during construction. The flow structures around the main cables indicate that the characteristic of the airflow trajectory over a steepled main cable may play an important role in the galloping generation. Engineers should take some effective measures to control this harmful phenomenon due to the big possibility of the onset of galloping during the construction period.

해상 NB-IoT 서비스를 위한 ICS RF 중계기 (ICS RF Repeater for Marine NB-IoT Service)

  • 조신호;이성렬
    • 한국항행학회논문지
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    • 제25권5호
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    • pp.390-396
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    • 2021
  • 본 연구에서는 해양수산부가 2016년 실행 계획을 발표한 전자어구 실명제를 실현할 수 있는 어구 자동식별 모니터링 시스템에서 통신 거리를 늘릴 수 있는 해상 중계기 설계와 제작에 대해 보고한다. 해상 중계기는 중계기를 구성하는 서비스 안테나와 링크 안테나 사이의 되먹임 신호에 의한 발진을 제거할 수 있는 ICS (interference cancellation system) 방식의 RF 중계기로 설계 제작하였다. ICS RF 중계기 설계에 있어 링크 안테나와 서비스 안테나 간 이격을 30 dB 확보하였다. 시험을 통한 검증 결과 ICS RF 중계기의 출력 신호 일부가 입력으로 되먹임되는 신호 레벨이 중계기 이득보다 15 dB 이상 낮을 때 발진에 의해 발생하는 EVM(error vector magnitude)이 성능 기준인 6%보다 낮게 얻어지는 것을 확인하였다. 본 연구를 통해 개발된 ICS RF 중계기를 어구 자동식별 모니터링 시스템 등의 해상 IoT 네트워크에 적용하면 서비스 영역이 늘어날 것으로 기대된다.