• 제목/요약/키워드: Flow level

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금정산 풍하측 저고도의 강풍 현상 (On the Low Level Strong Wind Occurring at the Downwind Side of the Kumjeong Mountain.)

  • 임상진;서광수
    • 한국환경과학회지
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    • 제5권6호
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    • pp.713-718
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    • 1996
  • We identified two characteristic turbulent flow cases, weakening and strengthening, which appear at the downwind side. Observations were made two times, Dec. 2-3. 1995 and Feb. 13-14. 1996 at Pusan National University site located downwind side of Kumjeong mountain. Meteorological observation system, tethersonde, was adopted to present observation. In the case of the west wind which blows perpendicular to Sanghak mountain located westward from the site, the wind speed highly increased in exponential with height. Therefore, the low level wind speed was so weak just like Taylor(1988)'s review. While the wind speed was intensified at 200-400m layer when the northwest wind blows from the continental Siberian high. We suppose 기 is because of the strong vertical convergence of flow between the surface inversion layer and the upper one, and also the horizontal convergence along the saddle and valley between the two mountains, Kumjeong and Sanghak-because of Bernoulli's effect. The inversion layer existed at surface-l00m and 500-600m level and the strong wind existed at about 200-400m layer.

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컴퓨터 프로그램을 이용한 엔진오일 내 공기함량 변화가 엔진윤활시스템에 미치는 영향 연구 (A Study on Effects of Oil Aeration Level on Engine Lubrication System by using Computer Program)

  • 전상명;박영환;장시열
    • Tribology and Lubricants
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    • 제17권3호
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    • pp.198-208
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    • 2001
  • A Parametric study based on a computer analysis of the lubrication system of a four-cylinder gasoline engine is illustrated. Through the parametric study, the effects of various aeration levels on the change of oil flow rate and pressure are investigated. Also, at high oil temperature and low engine speed, the effect of oil aeration level on oil flow characteristics in lubrication system is investigated. The illustrated results may give to designers the guide lines of oil aeration level for the safe design of engine lubrication systems in terms of minimum pressure at crank oil bore.

2차원 채널유동에서의 액적 변형에 대한 수치해석적 연구 (STUDY ON THE DEFORMATION OF DROPLETS IN A TWO-DIMENSIONAL CHANNEL FLOW)

  • 정성록;조명환;최형권;유정열
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.6-9
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    • 2011
  • In this study, the two-phase incompressible flow in two-dimensional channel considering the effect of surface tension is simulated using an improved level-set method. Quadratic element is used for solving the continuity and Navier-Stokes equations to avoid using an additional pressure equation, and Crank-Nicholson scheme and linear element are used for solving the advection equation of the level set function. Direct approach method using geometric information is implemented instead of the hyperbolic-type partial differential equation for the reinitializing the level set function. The benchmark test case considers various arrays of defomable droplets under different flow conditions in straight channel. The deformation and migration of the droplets are computed and the results are compared very well with the existing studies.

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Analysis of Viscous Free Surface Flow around a Ship by a Level-set Method

  • Park, Il-Ryong;Chun, Ho-Hwan
    • Journal of Ship and Ocean Technology
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    • 제6권2호
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    • pp.37-50
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    • 2002
  • In the present numerical simulation of viscous free surface flow around a ship, two-fluids in-compressible Reynolds-averaged Navier-Stokes equations with the standard $\textsc{k}-\varepsilon$turbulence model are discretized on a regular grid by using a finite volume method. A local level-set method is introduced for capturing the free surface movement and the influence of the viscous layer and dynamic boundary condition of the free surface are implicitly considered. Partial differential equations in the level-set method are discretized with second order ENO scheme and explicit Euler scheme in the space and time integration, respectively. The computational results for the Series-60 model with $C_B=0.6$ show a good agreement with the experimental data, but more validation studies for commercial complicated hull forms are necessary.

15만 파운드급 테스트 셀을 이용한 엔진성능 시험기술 (Aircraft Engine Performance Test Technologies by 150K lbf Thrust Test Cell)

  • 김우철;김철;김상백
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.180-187
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    • 2017
  • 항공기 엔진 지상 성능시험을 위한 15만 파운드 급 Test 설비를 구축하기 위해 Test Cell Type, Cell Flow, Cell Bypass Ratio, Approach Velocity, Cell Depression, Front Cell Distortion, Noise 및 Vibration 등의 주요 설계 목표를 설정 하였고, 설비 완공 후 최종 성능검사를 통해 목표 값을 충족하는 성능 데이터를 획득할 수 있었다.

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Modeling and Simulation for Level & Flow Control System Using Microcontroller

  • Unhavanich, Sumalee;Dumawipata, Teerasilapa;Tangsrirat, Worapong
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.86.5-86
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    • 2001
  • This work describes a design and implementation of the level & flow rate control system by using a single-chip microcontroller. The proposed model system is designed based on the use of the single-chip microcontroller 8031 with the EPROM emulator for programming the computer software. The microcontroller reaches the input level and flow signals from the level sensor and the turbine flowmeter, respectively, via the signal conditioning circuits and A/D converters in order to calculate the control signal. Moreover, the status of the process variable can easily be set up and controlled by program monitoring through the emulator, and can be graphically displayed on the computer screen. Experiment results were carried out which can be ...

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Cycle 수준의 Control Flow Description에서 합성 가능한 VHDL 기술로의 변환 방법에 관한 연구 (A Translation Method from Control Flow Descriptions in cycle-accurate level to Synthesizable RTL VHDL Descriptions)

  • 윤창열;장경선
    • 대한전자공학회:학술대회논문집
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    • 대한전자공학회 2003년도 하계종합학술대회 논문집 II
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    • pp.819-822
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    • 2003
  • This paper defines an algorithmic description language in cycle-accurate level which can be used to design hardware components. The proposed language is less complex and more flexible than VHDL language. In that the language includes C-like control flow descriptions and brief timing information(i.e. clock cycle boundaries) indicated by 'wait_edge' statements. We generate RTL VHDL codes from the descriptions. The proposed language requires only 10~30% of the # of lines to describe the same functionality compared with RTL VHDL.

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Gravity Level Dependency of Gas-Liquid Two-Phase Flow

  • Choi, Bu-Hong
    • Journal of Advanced Marine Engineering and Technology
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    • 제27권4호
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    • pp.487-493
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    • 2003
  • More reliable design of thermal transport. Power acquisition and thermal management systems requires the through understanding of the flow hydrodynamic. the differences and similarities between the two-phase flow characteristics of two-Phase flow influenced by the gravity levels. The data of flow Patterns, void fraction, frictional pressure drop associated with their characteristics were obtained at $\mu\textrm{g}$. 1g and 2g. Flow patterns and void fraction data obtained at three gravity levels were compared with each other and previous models and correlations.

개방된 2상 자연순환 회로내의 유동특성에 관한 실험적 연구 (An Experimental Study on the Flow Characteristics Inside an Open Two-Phase Natural Circulation Loop)

  • 경익수;이상용
    • 대한기계학회논문집
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    • 제17권5호
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    • pp.1313-1320
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    • 1993
  • 본 연구에서는 가시화가 가능한 상승부를 가진 개방된2상 자연순환 회로를 설치하여 각 운전 조건에 따른 순환 유동 특성을 살펴보았다. 즉, 가열량 증가에 따 른 상승부에서의 2상 유동 양식의 변화를 관찰하였고 동시에 가열기 입구 과냉 액체의 순환 유속 및 상승부의 기공률(void fraction)을 측정하였다. 또한 가열기 입구 및 출구에 설치된 밸브의 마찰저항, 가열기 입구 액체의 과냉 정도, 그리고 충전수위등이 전반적인 유동특성에 미치는 영향을 연구하였다.

Experimental and Computational Studies on Flow Behavior Around Counter Rotating Blades in a Double-Spindle Deck

  • Chon, Woo-Chong;Amano, Ryoichi S.
    • Journal of Mechanical Science and Technology
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    • 제18권8호
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    • pp.1401-1417
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    • 2004
  • Experimental and computational studies were performed to determine the effects of different blade designs on a flow pattern inside a double-spindle counter rotating mower deck. In the experimental study, two different blade models were tested by measuring air velocities using a forward-scatter LDV system. The velocity measurements were taken at several different azimuth and axial sections inside the deck. The measured velocity distributions clarified the air flow pattern caused by the rotating blades and demonstrated the effects of deck and blade designs. A high-speed video camera and a sound level meter were used for flow visualization and noise level measurement. In the computational works, two-dimensional blade shapes at several arbitrary radial sections have been selected for flow computations around the blade model. For three-dimensional computation applied a non-inertia coordinate system, a flow field around the entire three-dimensional blade shape is used to evaluate flow patterns in order to take radial flow interactions into account. The computational results were compared with the experimental results.