• 제목/요약/키워드: Cross-plane flow

검색결과 79건 처리시간 0.025초

단순변형율 조건 하의 회전하는 가변단면 $90^{\circ}$ 곡덕트 내 내향 난류유동 측정 (Measurement of Inward Turbulent Flows Subject to Plane Rate of Strain in a Rotating 90 Deg. Curved Duct of Variable Cross-Section)

  • 김동철;최영돈
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집B
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    • pp.765-770
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    • 2000
  • Hot-wire measurements are reported on the developing turbulent flows subject to plane rate of strain in a rotating $90^{\circ}$ dog bend. The cross-section of the bend varies from $100mm{\times}50mm$ rectangular shape at the bend inlet gradually to the $50mm{\times}100mm$ shape at the bend outlet with remaining a constant area. Data signals from the rotating test section are transmitted through a slip ring to the personal computer which is located at the outside of the rotating disc. 3-dimensional velocity and 6 Reynolds stress components were calculated from the equations which correlate the fluctuating and mean voltage values measured with rotating a slant type hot-wire into 6 orientations. The effects of Coriolis and centrifugal forces on the mean motions and turbulence structures are investigated with respect to rotational speed.

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단순변형률 조건 하의 회전하는 가변단면 $90^{\circ}$ 곡덕트내 외향 난류유동 측정 (Measurement of Outward Turbulent Flows Subject to Plane Rate of Strain in a Rotating 90 Deg. Curved Duct of Variable Cross-Section)

  • 오창민;최영돈
    • 대한기계학회논문집B
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    • 제24권5호
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    • pp.623-631
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    • 2000
  • Hot-wire measurements were carried out on the developing turbulent flows subject to plane rate of strain in a rotating curved duct. The cross-section of the curved duct varies from 100mm${\times}$50mm rectangular shape at the bend inlet gradually to the 50mm${\times}$100mm rectangular shape at the bend outlet. Experimental setup consists of the test section of $90^{\circ}$ curved duct, rotating disc of 1.95m diameter, Ag-Ni precision slip ring, automatic traversing mechanism, variable speed motor, centrifugal blower, orifice flowmeter and hot-wire anemometer. Data signals from the rotating curved duct are transmitted through the slip ring to the computer which is located at the outside of the rotating disc. 3-dimensional velocity and 6 Reynold stresses components were obtained from the fluctuating and mean voltage measured by the slant type hot-wire probe rotating into 6 orientations. We investigate the effects of Coriolis and centrifugal forces on the turbulence structure.

기울어진 정방형 실린더에 작용하는 유체력 (Flow past a Square Cylinder with an Angle of Attack)

  • 윤동혁;양경수;최춘범
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회B
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    • pp.2754-2758
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    • 2008
  • Numerical investigation has been carried out for laminar flow ($Re{\leq}150$) past a square cylinder in cross freestream with an angle of attack. This study would be the first step towards understanding flow-induced forces on cylindrical structures under a strong gust of wind from the viewpoint of wind hazards. Collecting all the numerical results obtained, we propose contour diagrams of drag/lift coefficients and Strouhal number (St) on an Re-Angle plane.

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3차원 교차 주름판 내 유동의 불안정성 및 자활 진동 (Instability and Self-Sustained Oscillation of the Flow between Three-Dimensionally Cross-corrugated Plates)

  • 이승엽;최영돈
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.679-682
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    • 2002
  • Energy dissipations in a general PHE flow are the compounded effects of the piled corrugate geometries and its wall pressure and temperature distributions. In addition, although the exchangers are substantial pieces of engineering equipment, they are composed of a very large number of nominally identical and small geometrical elements. In the present numerical study, the three-dimensionally complicated energy dissipation fields and those wall-shape-induced flow destabilization are investigated in the cross-corrugated passages, which result in high energy transports with comparatively low pressure drop. We revealed the critical conditions as $Re=157.3 for the wall-shape-induced flow destabilization in a general PHE element by initial value method, or shooting method, and compare its value to that of analytical solution of plane Poiseille flow, two-dimensional grooved flow and so on. We also observed the detailed variation of flow field and energy transportation with changes in time and flow variables such as Reynolds number. Lastly, we considered the flow natural frequency, or Strouhal number, with variation of hydrodynamic conditions for the best use of active control, such as forced mass flow rate pulsative flow, to enhance energy transportation.

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직사각형 단면을 갖는 $90^{\circ}C$ 급곡관 내의 3차원 난류유동에 관한 실험적 연구 (Experimental Study of Three-Dimensional Turbulent Flow in a $90^{\circ}C$ Rectanglar Cross Sectional Strongly Curved Duct)

  • 맹주성;류명석;양시영;장용준
    • 대한기계학회논문집
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    • 제15권1호
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    • pp.262-273
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    • 1991
  • 본 연구에서는 벽면에서의 압력은 압력측정 정치를 제작하여 측정하였으며 평 균유동 및 난류량들은 열선 유속계(hot wire system)을 사용하여 측정하였다.

폐색으로 인한 흙/부직포 시스템의 투수능 저하 모델 (Permeability Reduction Model of Soil-Geotextile System Induced by Clogging)

  • 이인모;김주현
    • 한국지반공학회논문집
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    • 제16권4호
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    • pp.107-116
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    • 2000
  • 흙 필터를 대신한 토목섬유의 사용량이 점차 증가하고 있다. 따라서 흙과 결합된 복합체계에 대한 메카니즘 연구가 활발히 진행되고는 있지만 이러한 복합체의 거동은 흙과 사용 필터재의 상호작용으로 인한 여러 가지 영향 인자들 때문에 실제의 필터 설계는 경험적인 방법에 의존하고 있다. 본 연구에서는 흙/부직포 시스템에서 세립자 이동에 의한 폐색 현상을 규명하고자 하였다. 국내의 대표적인 풍화잔적토 지반에 속하는 서울의 신내동과 포이동 지역의 흘을 시료로 이용한 본 실험은 필터재 내에서의 흐름방향에 따라 수평흐름과 수직흐름으로 나누어 실내 시험을 실시하였다. 필터재로서는 현장에서 배수재로 광범위하게 쓰이는 토목섬유를 사용하였다. 흙 모체와 필터가 결합된 복합체의 적합성 여부를 필터재의 흐름에 따라 비교, 분석하고 기존에 제안된 폐색 방지 기준을 적용하여 보았다. 이러한 실험결과를 토대로 하여 수평 흐름시 발생하는 공간적 투수 계수 변화를 예측할 수 있는 모델을 제안하고 실내에서 실시한 모형실험과 이론적 모델예측의 비교를 통하여 투수능 저하 현상의 시각적, 공간적 변화 양상을 파악하였다.

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원심압축기 회전차 내부의 3차원 유동해석 (Calculation of 3-Dimensional Flow Through an Impeller of Centrifugal Compressor)

  • 강신형;최영석
    • 대한기계학회논문집
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    • 제19권10호
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    • pp.2617-2629
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    • 1995
  • The flow through a centrifugal compressor rotor was calculated using the quasi-3-dimensional and fully 3-dimensional Navier-Stokes solution methods. The calculated results, obtained during the development of the computer codes for both methods are discussed. In the inviscid quasi 3-dimensional analysis, stream function formulation was used for the blade to blade (B-B) plane calculations, and the streamline curvature method was used for the meridional (H-S) plane calculations. In the viscous 3-dimensional flow analysis, a control volume method based on a general rotating curvilinear coordinate system was used to solve the time-averaged Navier-Stokes equations, and a standard k-.epsilon. model was used to obtain eddy viscosity. The quasi-3-dimensional analysis reasonably predicts the pressure distributions and requires much less computation time in the region where viscous effects are not strong; however, it fails to predict velocity field and loss mechanism through the impeller passage. The viscous 3-dimensional flow analysis shows reasonable pressure distributions and typical jet-wake flow field through the impeller passage. Secondary flow and total pressure distributions on cross-sectional planes explain the loss mechanisms through the impeller.

Wind tunnel study of plume dispersion with varying source emission configurations

  • Wittwer, Adrian R.;Loredo-Souza, Acir M.;Schettini, Edith B. Camano;Castro, Hugo G.
    • Wind and Structures
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    • 제27권6호
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    • pp.417-430
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    • 2018
  • The concentration fields in the proximities of a local gas emission source are experimentally analyzed in several combinations of wind incidences and source emissions. These conditions are determined by the plume buoyancy, emission velocity and incident flow wind speed. Concentration measurements are performed by an aspirating probe in a boundary layer wind tunnel. The analysis included the mean concentration values and the intensity of concentration fluctuations in a neutral atmospheric boundary layer flow. Different configurations are tested: an isolated stack in a homogeneous terrain and a stack with a bluff body in close proximity, located windward and leeward from the emission source. The experimental mean concentration values are contrasted with Gaussian profiles and the dilution factor is analyzed with respect to the empirical curves of the minimum dilution. Finally, a study on the plume intermittency is performed in a cross-sectional plane near the emission source. It is possible to highlight the following observations: a) plume vertical asymmetry in the case of an isolated emission source, b) significant differences in the dispersion process related to the relative location of the emission source and bluff body effects, and c) different probabilistic behavior of the concentration fluctuation data in a cross-sectional measurement plane inside the plume.

Flow Visualization of Flowfield Structures around an Aerospike Nozzle using LIF and PSP

  • NIIMI Tomohide;MORI Hideo;TANIGUCHI Mashio
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2004년도 Proceedings of 2004 Korea-Japan Joint Seminar on Particle Image Velocimetry
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    • pp.75-80
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    • 2004
  • Aerospike nozzles have been expected to be used for an engine of a reusable space shuttle to respond to growing demand for rocket-launching and its cost reduction. In this study, the flow field structures in any cross sections around clustered linear aerospike nozzles are visualized and analyzed, using laser induced fluorescence (LIF) of nitrogen monoxide seeded in the carrier gas of nitrogen. Since flow field structures are affected mainly by pressure ratio, the clustered linear aerospike nozzle is set inside a vacuum chamber to carry out the experiments in the wide range of pressure ratios from 75 to 200. Flow fields are visualized in several cross-sections, demonstrating the complicated three-dimensional flow field structures. Pressure sensitive paint (PSP) of PtTFPP bound by poly- IBM -co-TFEM is also applied to measurement of the complicated pressure distribution on the spike surface, and to verification of contribution of a truncation plane to the thrust. Finally, to examine the effect of the sidewalls attached to the aerospike nozzle, the flow fields around the nozzle with the sidewalls are compared with those without sidewalls.

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Numerical study of fluid behavior on protruding shapes within the inlet part of pressurized membrane module using computational fluid dynamics

  • Choi, Changkyoo;Lee, Chulmin;Park, No-Suk;Kim, In S.
    • Environmental Engineering Research
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    • 제25권4호
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    • pp.498-505
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    • 2020
  • This study analyzes the velocity and pressure incurred by protruding shapes installed within the inlet part of a pressurized membrane module during operation to determine the fluid flow distribution. In this paper, to find the flow distribution within a module, it investigates the velocity and pressure values at cross-sectional and outlet planes, and 9 sections classified on outlet plane using computational fluid dynamics. From the Reynolds number (Re), the fluid flow was estimated to be turbulent when the Re exceeded 4,000. In the vertical cross-sectional plane, shape 4 and 6 (round-type protrusion) showed the relatively high velocity of 0.535 m/s and 0.558 m/s, respectively, indicating a uniform flow distribution. From the velocity and pressure at the outlet, shape 4 also displayed a relatively uniform fluid velocity and pressure, indicating that fluid from the inlet rapidly and uniformly reached the outlet, however, from detailed data of velocity, pressure and flowrate obtained from 9 sections at the outlet, shape 6 revealed the low standard deviations for each section. Therefore, shape 6 was deemed to induce the ideal flow, since it maintained a uniform pressure, velocity and flowrate distribution.