• Title/Summary/Keyword: oscillating flow

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Blood Flow in an Aortic Bifurcation Model: Pulsed Doppler Ultrasound and Laser Doppler Anemometry Studies (대동맥분기에서의 혈액유동: 맥도플러초음파 및 레이저도플러계측기를 사용한 연구)

  • Kim, Young-H.
    • Proceedings of the KOSOMBE Conference
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    • v.1992 no.11
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    • pp.43-46
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    • 1992
  • $\underline{In\;vitro}$ velocity measurements were made using both the pulsed Doppler ultrasound (PDU) machine and laser Doppler anemometer (LDA) system in order to investigate the flow characteristics near the aortic bifurcation. Velocities measured from the PDU machine was in good agreement with those from the LDA. The flow in the daughter branches was three-dimensional with a secondary flow. The oscillating wall shear stress with this secondary fluid motion is well correlated with the localization of the atherosclerosis.

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Numerical Simulation of Irregular Airflow in OWC Wave Generation System Considering Sea Water Exchange (해수교환을 고려한 진동수주형 파력발전구조물에서 불규칙공기흐름에 관한 수치해석)

  • Lee, Kwang Ho;Park, Jung Hyun;Cho, Sung;Kim, Do Sam
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.25 no.3
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    • pp.128-137
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    • 2013
  • Due to the global warming and air pollution, interest in renewable energies has increased in recent years. In particular, the crisis of the depletion of fossil energy resources in the near future has accelerated the renewable energy technologies. Among the renewable energy resources, oceans covering almost three-fourths of earth's surface have an enormous amount of energy. For this reason, various approaches have been made to harness the tremendous energy potential. In order to achieve two purposes: to improve harbor water quality and to use wave energy, this study proposed a sea water exchange structure applying an Oscillating Water Column (OWC) wave generation system that utilizes the air flow velocity induced by the vertical motion of water column in the air chamber as a driving force of turbine. In particular, the airflow velocity in the air chamber was estimated from the time variations of water surface profile computed by using 3D-NIT model based on the 3-dimensional irregular numerical wave tank. The relationship of the frequency spectrums between the computed airflow velocities and the incident waves was analyzed. This study also discussed the characteristics of frequency spectrums in the air chamber according to the presence of the structure, wave deformations by the structure, and the power of the water and air flows were also investigated. It is found that the phase difference exists in the time series data of water level fluctuations and air flow in the air chamber and the air flow power is superior to the fluid flow power.

A Two-Dimensional Study of Transonic Flow Characteristics in Steam Control Valve for Power Plant

  • Yonezawa, Koichi;Terachi, Yoshinori;Nakajima, Toru;Tsujimoto, Yoshinobu;Tezuka, Kenichi;Mori, Michitsugu;Morita, Ryo;Inada, Fumio
    • International Journal of Fluid Machinery and Systems
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    • v.3 no.1
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    • pp.58-66
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    • 2010
  • A steam control valve is used to control the flow from the steam generator to the steam turbine in thermal and nuclear power plants. During startup and shutdown of the plant, the steam control valve is operated under a partial flow conditions. In such conditions, the valve opening is small and the pressure deference across the valve is large. As a result, the flow downstream of the valve is composed of separated unsteady transonic jets. Such flow patterns often cause undesirable large unsteady fluid force on the valve head and downstream pipe system. In the present study, various flow patterns are investigated in order to understand the characteristics of the unsteady flow around the valve. Experiments are carried out with simplified two-dimensional valve models. Two-dimensional unsteady flow simulations are conducted in order to understand the experimental results in detail. Scale effects on the flow characteristics are also examined. Results show three types of oscillating flow pattern and three types of static flow patterns.

Variation of Eigenvalues of the Multi-span Fuel Rod due to Periodic Flow Disturbance by the Flow Mixer (혼합날개의 주기적 유동교란에 따른 다점지지 연료봉의 고유치변화)

  • Lee, Kang-Hee;Woo, Ho-Kil
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.20 no.3
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    • pp.215-222
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    • 2010
  • Long and slender body, like a fuel rod, oscillating in axial flow can be unstabilized even by the small cross flow which can be activated by the flow mixer or turbulent generator. It is important to include these effects of flow disturbance in dynamic stability analysis of nuclear fuel rod. This work shows how eigen frequency of a multi-span fuel rod can be changed by the swirl flow, which is discretely generated by a flow mixer. By solving a state-space form of the eigenvalue equation for a multi-span fuel rod system, the critical velocity at which a fuel rod becomes unstable was calculated. Based on the simulation results, we evaluated how stability of a multi-spanned nuclear fuel rod with mixing vanes can be affected by the coolant flow in an operating reactor core.

THE COMPUTATION OF UNSTEADY FLOWS AROUND THREE DIMENSIONAL WINGS ON DYNAMICALLY DEFORMING MESH (변형격자계를 이용한 3차원 날개 주변의 비정상 유동 해석)

  • Yoo, Il-Yong;Lee, Seung-Soo
    • 한국전산유체공학회:학술대회논문집
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    • 2009.11a
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    • pp.34-37
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    • 2009
  • Deforming mesh should be used when bodies are deforming or moving relative to each other due to the presence of aerodynamic forces and moments. Also, the flow solver for such a flow problem should satisfy the geometric conservation law to ensure the accuracy of the solutions. In this paper, a RANS(Reynolds Averaged Navier-Stokes) solver including automatic mesh capability using TFI(Transfinite Interpolation) method and GCL is developed and applied to flows induced by oscillating wings with given frequencies. The computations are performed both on deforming meshes and on rigid meshes. The computational results are compared with experimental data, which shows a good agreement.

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THE COMPUTATION OF UNSTEADY FLOWS AROUND THREE DIMENSIONAL WINGS ON DYNAMICALLY DEFORMING MESH (변형격자계를 이용한 3차원 날개 주변의 비정상 유동 해석)

  • Yoo, Il-Yong;Lee, Byung-Kwon;Lee, Seung-Soo
    • Journal of computational fluids engineering
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    • v.15 no.1
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    • pp.37-45
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    • 2010
  • Deforming mesh should be used when bodies are deforming or moving relative to each other due to the presence of aerodynamic forces and moments. Also, the flow solver for such a flow problem should satisfy the geometric conservation law to ensure the accuracy of the solutions. In this paper, a RANS(Reynolds Averaged Navier-Stokes) solver including automatic mesh capability using TFI(Transfinite Interpolation) method and GCL is developed and applied to flows induced by oscillating wings with given frequencies. The computations are performed both on deforming meshes and on rigid meshes. The computational results are compared with experimental data, which shows a good agreement.

A Characteristics of Smoke Layer Formation Affected Periodicity of Fire Plumes (Plume의 주기성이 연층형성에 미치는 영향)

  • 한용식;김명배;오광철;신현동
    • Fire Science and Engineering
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    • v.16 no.2
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    • pp.38-42
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    • 2002
  • This experiment is to understand a characteristics of smoke layer formation affected periodicity of fire plumes. The ON-OFF jet was used to constitute the oscillating flow, which was formed by a mixture of nitrogen gas with kerosene particles. The instantaneous images was obtained by digital video camera using laser sheet technique. The results were confirmed that the smoke layer in the near fire source comprise vortices which are formed by impingement from the periodicity of fire plume. The periodic impinging of plumes were thickened the smoke layer and produced the back-flow.

Numerical Analysis of Flow Characteristics in the Wells Turbine for Wave Power Conversion (파력 발전용 웰즈터빈의 유동특성에 관한 수치적 연구)

  • Lee, Hyeong-Gu;Kim, Jeong-Hwan;Lee, Yeon-Won
    • 유체기계공업학회:학술대회논문집
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    • 2000.12a
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    • pp.325-333
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    • 2000
  • The aerodynamics of the Wells turbine has been studied using a 3-dimensional, unstructured mesh flow solver for the Reynolds-averaged Navier-Stokes equations. The basic feature of the Wells turbine is that even though the cyclic airflow produces oscillating axial forces on the airfoil blades, the tangential force on the rotor is always in the same direction. Geometry used to define the 3-dimensional numerical grid is based upon that of an experimental test rig. The 3-dimensional Wells turbine model, consisting of approximate 220,000 cells is tested at four axial flow rates. In the calculations the angle of attack has been varied between $10^{\circ}$ and $30^{\circ}$ of blades. Representative results from each case are presented graphically and analyzed. It is concluded that this method holds much promise for future development of Wells turbines.

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Visualization of the flow between co-rotating disks in shroud with an obstruction (장애물을 포함한 동시회전 디스크 내부의 비정상 유동가시화)

  • 공대위;도덕희;주원구
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2003.05a
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    • pp.1152-1156
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    • 2003
  • Hard disk drives (HDD) in computer are used extensively as data storage capacity. The trend in the computer industry to produce smaller disk drives rotating at higher speeds requires an improved understanding of fluid motion in the space between disks. PIV measurement was used fer the unsteady flow between the center pair of four disks of four times larger than common radius of HDD disk at several rpm in a fixed cylindrical enclosure. The boundary between inner region and outer region is detected using PIV measurement and the number of dominant vortices s determined clearly. Tip vortices generated by an obstruction with actual-like configuration can be found at inner region. Oscillating flow from the obstruction appears at outer region with complex flow pattern.

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Turbulence Generation by Ultrasonically Induced Gaseous Cavitation in the $CO_2$Saturated Water Flow

  • Lee, Seung-Youp;Park, Young-Don
    • Journal of Mechanical Science and Technology
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    • v.17 no.8
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    • pp.1203-1210
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    • 2003
  • Emission of ultrasonic vibration to turbulent flow promotes the turbulence generation due to the resonantly oscillating pressure field and thereby induced cavitation. In addition, ultrasonic vibration is well transmitted through water and not dissipated easily so that the micro-bubbles involved in the fluid induce the gaseous cavitation if the bubbles are resonated with the ultrasonic field. In the present study, we found through LDV measurement that the gaseous cavitation induced by ultrasonic vibration to CO$_2$saturated water flow in the rectangular cross-sectioned straight duct enhances turbulence much more than the case of non-ultrasonic or normal ultrasonic conditions without gaseous cavitation. We also found that the fluctuating velocity component induced by emitting the ultrasonic vibration in normal direction of a rectangular channel flow can be redistributed to stream-wise component by the agitation of gaseous cavitation.