• 제목/요약/키워드: Flow separation

검색결과 1,794건 처리시간 0.024초

수평 T형 증발관내 2상류의 유량분배 및 압력강하 특성 (Characteristics of T-phase flow distribution and pressure drop in a horizontal T-type evaporator tube)

  • 박종훈;조금남;조홍기
    • 설비공학논문집
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    • 제11권5호
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    • pp.658-668
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    • 1999
  • The objective of the present study is to investigate the effect of experimental parameters on the hydrodynamic characteristics in a horizontal tee-type evaporator using R-22. The experimental apparatus consisted of an unheated tee-type test section, a liquid-vapor separator, a preheated, mass flow meters, a plate heat exchanger, pump, and other measurement devices. The experimental parameters were mass flux(500 and 600kg/$m^2$s), inlet quality(0.1~0.3) and separation ratio(0.3~0.7). Absolute pressure at the inlet of the test section was 0.652 MPa. The branch-to-inlet inner diameter ratio was 0.61. Pressure gradient at the branch section was larger than that at the run section at the same separation ratio. Pressure drop per unit length increased at the run section and decreased at the branch section as the separation ratio increased. Pressure drop predicted by the separated flow model agreed with experimental data within -35 to +16%. Generally, predicted values showed similar trend with the data. Mass flow ratio of vapor refrigerant was affected by the inlet quality more than the mass flux.

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3D 프린팅을 적용한 미니 하이드로 싸이클론 분리기의 질량유량을 통한 분리효율 해석 및 평가 (Analysis and Evaluation of Separation Efficiency on Mass Flow of Mini Hydro Cyclone Separator Manufactured by 3D Printing)

  • 이형욱;이여울;이명원;권제영;강명창
    • 한국기계가공학회지
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    • 제20권7호
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    • pp.89-96
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    • 2021
  • In this study, a mini hydro cyclone was designed and manufactured to achieve an inlet flow rate of 2 L/min in the experiment, which was conducted using alumina powder with a specific gravity of 3.97. This hydro cyclone was studied for using in steam and water analysis system (SWAS) of thermal power plant and was manufactured by 3D printing. Numerical analysis was performed with Solidworks Flow Simulation, utilizing the reynolds stress method (RSM) of fluid multiphase flow analysis models. Experimental and numerical analysis were performed under the three conditions of inlet velocity 2.0, 4.0, and 6.0 m/s. The separation efficiency was over 80% at all inlet velocity conditions. At the inlet velocity 4m/s, the separation efficiency was the best, and it was confirmed that the efficiency was more than 90%.

A Computational Study on the Unsteady Lateral Loads in a Rocket Nozzle

  • ;김희동
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년도 제30회 춘계학술대회논문집
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    • pp.289-292
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    • 2008
  • Highly over-expanded nozzle of the rocket engines will be excited by non-axial forces due to flow separation at sea level operations. Since rocket engines are designed to produce axial thrust to power the vehicle, non-axial static and/or dynamic forces are not desirable. Several engine failures were attributed to the side loads. Present work investigate the unsteady flow in an over-expanded rocket nozzle in order to estimate side load during a shutdown/starting. Numerical computations has been carried out with density based solver on multi-block structured grid. Present solver is explicit in time and unsteady time step is calculated using dual time step approach. AUSMDV is considered as a numerical scheme for the flux calculations. One equation Spalart-Allmaras turbulence model is selected. Results presented here is for two nozzle pressure ratio i.e. 100 and 20. At 100 NPR, restricted shock separation (RSS) pattern is observed while, 20 NPR shows free shock separation (FSS) pattern. Side load is observed during the transition of separation pattern at different NPR.

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정상 해석 기반의 데이터베이스를 이용한 TST 비행체의 분리 궤도 예측 (PREDICTION OF SEPARATION TRAJECTORY FOR TSTO LAUNCH VEHICLE USING DATABASE BASED ON STEADY STATE ANALYSIS)

  • 조재현;안상준;권오준
    • 한국전산유체공학회지
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    • 제19권2호
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    • pp.86-92
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    • 2014
  • In this paper, prediction of separation trajectory for Two-stage-To-Orbit space launch vehicle has been numerically simulated by using an aerodynamic database based on steady state analysis. Aerodynamic database were obtained for matrix of longitudinal and vertical positions. The steady flow simulations around the launch vehicle have been made by using a 3-D RANS flow solver based on unstructured meshes. For this purpose, a vertex-centered finite-volume method was adopted to discretize inviscid and viscous fluxes. Roe's finite difference splitting was utilized to discretize the inviscid fluxes, and the viscous fluxes were computed based on central differencing. To validate this flow solver, calculations were made for the wind-tunnel experiment model of the LGBB TSTO vehicle configuration on steady state conditions. Aerodynamic database was constructed by using flow simulations based on test matrix from the wind-tunnel experiment. ANN(Artificial Neural Network) was applied to construct interpolation function among aerodynamic variables. Separation trajectory for TSTO launch vehicle was predicted from 6-DOF equation of motion based on the interpolated function. The result of present separation trajectory calculation was compared with the trajectory using experimental database. The predicted results for the separation trajectory shows fair agreement with reference[4] solution.

INVESTIGATION ON CRITERION OF SHOCK-INDUCED SEPARATION IN SUPERSONIC FLOWS

  • Heuy-Dong KIM
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 1995년도 제5회 학술강연회논문집
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    • pp.69-83
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    • 1995
  • A great number of experimental data indicating shock-induced separation(SIS) in internal or external supersonic flows were reviewed to make clear the mechanism of SIS and to present the criterion of turbulent boundary layer separation. The interesting conclusions were obtained for the considerably wide range of flow geometries that the incipient separation is almost independent of the flow geometries, and that it is relatively unaffected by changes in gas specific heat, and boundary layer Reynolds number, Furthermore, the pressure rise necessary to separate boundary layer in external flows was found to be applicable to SIS in overexpanded propulsion nozzles. This is due to the fact that the SIS phenomenon caused by the interaction between shock waves and turbulent boundary layers is processed through a supersonic deceleration. This is, the SIS in almost all of interacting flow fields is governed by the concept of free interaction, and criterion of SIS is only a Function of upstream Mach number.

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우오수분리벽을 이용한 합류식 하수관거와 분류식 우수관거의 월류수 제어효과 비교 (Comparison of Pollutant Control in Combined Sewer Overflows and Separated Sewer Overflows using the Separation Wall)

  • 임봉수;김도영;이광춘
    • 한국물환경학회지
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    • 제23권4호
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    • pp.458-466
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    • 2007
  • This study is to evaluate control effects of separation wall by surveying water quality and sewer overflows during dry and wet periods in combined sewer and separated sewer systems. Ravine water from the combined Seokgyo outfall with the separation wall was separated about four times larger than sewage flow during dry periods. The water quality of the combined Seokgyo outfall with separation wall during dry periods is flow weighed average BOD 61 mg/L, the combined Cheonseokgyo outfall without the separation wall is average BOD 71 mg/L, and the separated Pyeongsong center outfall is average BOD 41 mg/L. The BOD concentration in separated outfall form about 57% of the combined outfall, and this means the separated outfall (i.e. storm sewer) is polluted by inflow of sewage. The overflow load of the separated outfall is ten times higher than the combined outfall and its overflow load per rainfall is three times than combined outfall during the wet periods. Therefore, the control plan of overflow load is required in storm sewer. The control effects of the overflow load increased 79% by setting the separation wall in the combined sewer, and showed 27% increase without the separation wall in separated sewer, but forecasted over 80% increase of effects if the separation wall was set.

수직분사 막냉각구멍 내부에서의 3차원 유동특성 (Three-dimensional flow within a film-cooling hole normally oriented to the main flow)

  • 이상우;주성국
    • 대한기계학회논문집B
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    • 제21권9호
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    • pp.1185-1197
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    • 1997
  • Three-dimensional flow within a film-cooling hole, which is normally oriented to the main flow, has been measured by using a straight five-hole probe for the blowing ratios of 1.0 and 2.0. The length-to-diameter ratio of the injection hole is fixed to be 1.0 throughout the whole experiments. The result shows that the secondary flow within the hole is strongly affected by the main flow and flow separation at the hole inlet. The higher blowing ratio provides less influence of the main flow on the injectant flow. The three-dimensional flow at the hole exit is considerably altered due to the strong interaction between the injectant and main flow. The aerodynamic loss produced inside the injection hole is mainly attributed to the inlet flow separation.

다공성 매질의 내부유동에 관한 섭동해석 (Perturbation Analysis of Stokes Flow in Porous Medium)

  • 성관제
    • 한국물환경학회지
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    • 제21권4호
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    • pp.393-397
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    • 2005
  • In this study, flow in a porous medium is analyzed using a computer-extended perturbation series solution. The flow is modelled as a creeping flow in a periodically constricted channel. The channel walls have a sinusoidally varying width and the flow is analyzed in terms of its vorticity and stream functions in the Stokes flow regime. The perturbation series in terms of a small parameter, average width to length ratio, is extended with a computer resulting in purely asymptotic series and Pade summation is used to obtain final results. Resulting flow shows flow separations in the widening section and immobile zones in the widest section of the flow regime with reattachment in the narrowing section. Analysis of the flow separation phenomena resulted in a correlation between the two geometric parameters of the channel walls to predict the onset of flow separation in the Stokes flow regime.

초음속 비행환경 조건에서의 슈라우드 분리시험 연구 (Experimental Investigation for the Shroud Separation in the Supersonic Flow)

  • 김정영;이동민
    • 한국항공우주학회지
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    • 제45권7호
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    • pp.539-549
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    • 2017
  • 본 논문에서는 마하 3의 초음속 유동 환경에서의 슈라우드 분리 특성 연구를 위한 시험을 수행하였다. 시험은 분리 구조물의 시험이 가능한 수직 자유 젯 풍동에서 이루어졌다. 분리시험용 슈라우드는 시험 목적과 시험 환경에 맞게 소형화한 축소형 모델을 사용하였으며 외부 유동의 하중을 고려해 잠금/전개장치를 설계하였다. 고속카메라를 활용해 슈라우드가 전개되는 동안 슈라우드에서 생성되는 충격파 변화 양상과 슈라우드 전개/분리 거동을 기록하였다. 또 첨두부 동체 표면에는 압력센서를 적용해 슈라우드가 전개되는 동안 첨두부 표면에 작용하는 비정상 압력을 계측하였다. 시험자료 분석 결과, 슈라우드 분리기술 연구에 필요한 슈라우드 분리 영상 및 첨두부 비정상 압력 자료를 획득하였다. 아울러 외부 유동의 온도와 방향 조건에 따른 슈라우드 분리 거동과 충격파 변화 양상 그리고 첨두부 표면 압력 변화 특성을 확인하였다.

화학적 수문곡선 분리기법을 이용한 낙동강 최상류 유역 기저유출량 산정 (Base Flow Estimation in Uppermost Nakdong River Watersheds Using Chemical Hydrological Curve Separation Technique)

  • 김령은;이옥정;최정현;원정은;김상단
    • 한국물환경학회지
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    • 제36권6호
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    • pp.489-499
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    • 2020
  • Effective science-based management of the basin water resources requires an understanding of the characteristics of the streams, such as the baseflow discharge. In this study, the base flow was estimated in the two watersheds with the least artificial factors among the Nakdong River watersheds, as determined using the chemical hydrograph separation technique. The 16-year (2004-2019) discontinuous observed stream flow and electrical conductivity data in the Total Maximum Daily Load (TMDL) monitoring network were extended to continuous daily data using the TANK model and the 7-parameter log-linear model combined with the minimum variance unbiased estimator. The annual base flows at the upper Namgang Dam basin and the upper Nakdong River basin were both analyzed to be about 56% of the total annual flow. The monthly base flow ratio showed a high monthly deviation, as it was found to be higher than 0.9 in the dry season and about 0.46 in the rainy season. This is in line with the prevailing common sense notion that in winter, most of the stream flow is base flow, due to the characteristics of the dry season winter in Korea. It is expected that the chemical-based hydrological separation technique involving TANK and the 7-parameter log-linear models used in this study can help quantify the base flow required for systematic watershed water environment management.