• 제목/요약/키워드: Quasi-Steady Model

검색결과 118건 처리시간 0.026초

유동 모드 댐퍼에서의 Herschel-Bulkley 모델의 유용한 해법 (Useful Guide to Solve Herschel-Bulkley Model in a Flow Mode Damper)

  • 이덕영;박성태
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2003년도 추계학술대회논문집
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    • pp.784-787
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    • 2003
  • Electrorheological(ER) and magnetorheological(MR) fluid-based dampers are typically analyzed using Bingham-plastic shear model under quasi-steady fully developed flow conditions. A Herschel-Bulkley constitutive shear flow relationship is that the linear shear stress vs. strain rate behavior of Bingham model is replaced by a shear stress that is assumed to be proportional to a power law of shear rate. This power is called the flow behavior index. Depending on the value of the flow behavior index number, varying degrees of post-yield shear thickening or thinning behavior can be analyzed. But it is not practical to analyze the damping force in a flow mode damper using Herschel-Bulkley model because it is needed to solve a polynomial equation. A useful guide is suggested to analyze the damping force in a damper using the Herschel-Bulkley model.

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현장에서 운전중인 터보냉동기의 성능 측정과 전력 소비량 예측 (Field Performance Test and Prediction of Power Consumption of a Centrifugal Chiller)

  • 장영수;신영기;김영일;백영진
    • 대한기계학회논문집B
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    • 제25권12호
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    • pp.1730-1738
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    • 2001
  • This paper presents an overview of testing and analyzing field performance of a centrifugal chiller which has a rated capacity of 200 RT(703 kW). Field data of a chiller installed in the cleanroom research building of KIST has been collected far performance analysis. The operating data included start-up, shut-down, and quasi-static state where cooling capacity and compressor power consumption varied cyclically. It was found that the steady-state thermodynamic model could be applied to relate the cooling capacity and COP under quasi-static conditions. The results led to finding the required cooling load pattern and a possible energy saving method. This study provides a method of evaluating performance of a large capacity centrifugal chiller in which field test is necessary.

낙동강 하류의 유사특성과 낙동강하구둑 준설효과에 관한 수치모의 연구 (Numerical Modeling for Sedimentation Characteristics of the Lower Nakong River and Sediment Dredging Effects at the Nakdong River Estuary Barrage)

  • 지운;;박상길;김병달
    • 대한토목학회논문집
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    • 제28권4B호
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    • pp.405-411
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    • 2008
  • 낙동강하구둑은 하구둑 상류로의 염수침입을 방지하여 지속적인 용수를 공급하기 위해 1987년에 건설되었으며 이후 매년 하구둑 상류 접근수로에 퇴적되는 유사를 제거하기 위해 준설 작업이 수행되어져 왔다. 준설작업뿐만 아니라 산업 및 주거 시설의 개발사업 등의 하천 환경 변화로 인해 하구둑 상류에서의 유사 이송 및 하상 특성은 꾸준히 변화되어 왔으나 하구둑이 건설된 이 후 유사이송 및 하상변동에 대한 현장 모니터링 및 연구는 활발히 수행되지 못하였다. 이에 본 논문은 낙동강 하류의 대상구간에 대해 현장 측정 자료 및 과거 자료들을 최대한 활용하여 낙동강하류에서의 하상변동 및 계절별 유사농도 등의 변화를 분석하였으며 검증된 기초자료들과 준정상류 모형을 이용하여 하구둑 상류에 시행되고 있는 준설작업의 수행 여부에 따른 홍수 발생시 수위 변화에 대해서 수치모의를 실시함으로써 낙동강하구둑에서의 준설효과를 분석하였다.

Modeling of rain-wind induced vibrations

  • Peil, Udo;Nahrath, Niklas
    • Wind and Structures
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    • 제6권1호
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    • pp.41-52
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    • 2003
  • Rain-wind induced vibrations of cables are a challenging problem in the design of cable-stayed bridges. The precise excitation mechanism of the complex interaction between structure, wind and rain is still unknown. A theoretical model that is able to accurately simulate the observed phenomena is not available. This paper presents a mathematical model describing rain-wind induced vibrations as movement-induced vibrations using the quasi-steady strip theory. Both, the vibrations of the cable and the movement of the water rivulet on the cable surface can be described by the model including all geometrical and physical nonlinearities. The analysis using the stability and bifurcation theory shows that the model is capable of simulating the basic phenomena of the vibrations, such as dependence of wind velocity and cable damping. The results agree well with field data and wind tunnel tests. An extensive experimental study is currently performed to calibrate the parameters of the model.

오리피스 링이 부착된 원관내 주기적인 난류운동에 대한 수치해석 (Numerical Study of Periodic Turbulent Flow for a Pipe with an Orifice Ring)

  • 맹주성;양시영;서현철
    • 대한기계학회논문집
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    • 제17권9호
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    • pp.2294-2303
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    • 1993
  • This paper investigated the characteristics of the turbulent incompressible flow past the orifice ring in an axi-symmetric pipe. The flow field was the turbulent pulsatile flow for Reynolds number of $2{\times}10^{5}$ which was defined based on the maximum velocity and the pipe diameter at the inlet, with oscillating frequence $(f_{os})=1/4{\pi}$ which was considered as quasi-steady state frequence. In the present investigation, finite analytic method was used to solve the governing equations in Navier Stokes and turbulent transport formulations. Particularly at high Reynolds number and low oscillation frequency, the effects of orifice ring on the flow were numerically investigated. The separation zone behind the orifice ring during the acceleration phase was found to be decreased. However, during the deceleration phase, the separation behind the orifice ring for pulsatile flow continuously grow to a size even larger than that in steady flow. The pressure drop in steady flow was found to be constant and always positive while for pulsatile flow the pressure drop change with time. And large turbulent kinetic energy, dissipation rate were found to be located in the region where the flow passes through the orifics ring. The maximum turbulent kinetic energy, generally occurs along the shear layer where the velocity gradient is large.

Time domain flutter analysis of the Great Belt East Bridge

  • Briseghella, Lamberto;Franchetti, Paolo;Secchi, Stefano
    • Wind and Structures
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    • 제5권6호
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    • pp.479-492
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    • 2002
  • A finite element aerodynamic model that can be used to analyse flutter instability of long span bridges in the time domain is presented. This approach adopts a simplified quasi-steady formulation of the wind forces neglecting the vortex shedding effects. The governing equations used are effective only for reduced velocities $V^*$ sufficiently great: this is generally acceptable for long-span suspension bridges and, then, the dependence of the wind forces expressions of the flutter derivatives can be neglected. The procedure describes the mechanical response in an accurate way, taking into account the non-linear geometry effects (large displacements and large strains) and considering also the compressed locked coil strands instability. The time-dependence of the inertia force due to fluid structure interaction is not considered. The numerical examples are performed on the three-dimensional finite element model of the Great Belt East Bridge (DK). A mode frequency analysis is carried out to validate the model and the results show good agreement with the experimental measurements of the full bridge aeroelastic model in the wind tunnel tests. Significant parameters affecting bridge response are introduced and accurately investigated.

Proposed large-scale modelling of the transient features of a downburst outflow

  • Lin, W.E.;Orf, L.G.;Savory, E.;Novacco, C.
    • Wind and Structures
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    • 제10권4호
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    • pp.315-346
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    • 2007
  • A preceding companion article introduced the slot jet approach for large-scale quasi-steady modelling of a downburst outflow. This article extends the approach to model the time-dependent features of the outflow. A two-dimensional slot jet with an actuated gate produces a gust with a dominant roll vortex. Two designs for the gate mechanism are investigated. Hot-wire anemometry velocity histories and profiles are presented. As well, a three-dimensional, subcloud numerical model is used to approximate the downdraft microphysics, and to compute stationary and translating outflows at high resolution. The evolution of the horizontal and vertical velocity components is examined. Comparison of the present experimental and numerical results with field observations is encouraging.

공냉식 수직평판형 흡수기의 흡수과정에 대한 근사해법 (Approximate Solution of Absorption Process in an Air-Cooled Vertical Plate Absorber)

  • 정은수
    • 설비공학논문집
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    • 제6권4호
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    • pp.453-462
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    • 1994
  • An unsteady quasi one-dimensional model of momentum, heat and mass transfer in a falling film of a vertical plate absorber which is cooled by air was developed using the integral method. Energy conservation of the absorber wall is considered in the model. The model can predict absorption rate, film thickness and mean velocity as well as concentration and temperature profiles. Predictions of steady state temperature and concentration profiles for LiBr/water system for constant wall temperature condition are in good agreement with the two-dimensional finite difference method solutions. Effects of operating conditions, such as convective heat transfer coefficient between the cooling air and the absorber wall, cooling air temperature and film thickness at inlet, on absorption rate of water vapor into LiBr/water solution were shown.

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Water-Entry Induced Cavity Pressure

  • Lee, Min-Hyung
    • Journal of Mechanical Science and Technology
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    • 제14권5호
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    • pp.562-568
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    • 2000
  • The pressure in a water-entry induced cavity, is analyzed up to the closed cavity (bubble). Water-entry is a highly transient phenomenon, and the evolution of the water-entry cavity must be explained by considering the entry speed, shape of the solid body, atmosphere pressure, and cavity pressure as the primary variables. This work is an extension of the cavity dynamics model recently reported by Lee (l997a). To extend the model for a wide range of entry speeds the cavity pressure is calculated from a one-dimensional quasi-steady flow model. The estimation of the cavity pressure allows us to explain the experimentally observed surface closure phenomena at low entry speeds. Predictions for the time of surface closure are compared with the published experimental data.

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실시간 공력모델을 이용한 비행 시뮬레이션 연구 (Study of Flight Simulation using Real-Time Aerodynamic Model)

  • 이창호;박영민;최형식
    • 항공우주시스템공학회지
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    • 제9권4호
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    • pp.49-54
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    • 2015
  • Accurate aerodynamic data is required for the flight simulation or control logic design of aircraft. The aerodynamic look-up table has been used widely to provide aerodynamic forces and moments for given flight conditions. In this paper, we replace the aerodynamic look-up table with real-time aerodynamic model which calculates aerodynamic forces and moments of quasi-steady flow directly for given flight conditions and control surface deflections. Flight simulations are conducted for the low-speed small UAV using real-time aerodynamic model, and responses of the UAV are predicted successfully for inputs of control surfaces.