• Title/Summary/Keyword: Swirl Flows

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Prediction of strongly swirling turbulent flow downstream of an abrupt pipe expansion (원관내 급확대부 하류의 강선회난류에 관한 수치해석)

  • Kim, K.Y.;Chang, Y.S.
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.9 no.1
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    • pp.23-32
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    • 1997
  • Swirling turbulent flows downstream of an abrupt axisymmetric expansion in a pipe are analyzed numerically by a second-order turbulence closure. Predictions for the flows without swirl and with strong swirl are obtained. The governing differential equations are discretized by finite volume approach. The results show that the on-axis recirculation induced by the strong swirl is correctly reproduced. The predictions for mean velocity components and turbulent normal stresses agree well with experimental data far downstream of expansion, but show large discrepancies in wall-bounded recirculation zone.

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Centerline Turbulent Characteristics of an Axisymmetric Flow with the Swirl (소용돌이 성분이 있는 축대칭유동의 중심난류 특성)

  • 남경덕;한용운
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.10
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    • pp.2724-2737
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    • 1994
  • The swirl effect on an axisymmetric turbulence has been investigated along its centerline by the hot wire anemometry. Flow facility to generate and conrol the swirl has been built by using the rotating honeycomb and grid. For the case of internal flows, as the strength of the swirl increases the flow tends to be locally isotropic by modifying the radial and the rotational components mainly. In comparison with those of the plain free jet, the decay of the centerline turbulences seems to be delayed substantially even with a slight swirl component.

LES OF TURBULENT PREMIXED COMBUSTION FLAME AND LES APPLICATION FOR THE INDUSTRIAL COMBUSTOR DEVELOPMENT (난류 예혼합연소 화염의 LES 및 산업용 연소기 개발을 위한 LES 응용 해석 기술)

  • Park, Nam-Seob;Ryu, Jong-Hyuk
    • 한국전산유체공학회:학술대회논문집
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    • 2010.05a
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    • pp.437-441
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    • 2010
  • LES results of turbulent premixed combustion flows are introduced by using the dynamic sub-grid scale model based on G-equation describing the flame front propagation. The turbulent premixed combustion flows around bluff body and over backward facing step are analyzed to validate present formation. LES of swirling partially premixed combustion flame is also performed to conform the predictive capabilities of LES model and to prompt our understanding for the combustion flows over double cone swirl burner combustor by using CFD-ACE+ commercial code.

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Three-Dimensional Flow Analysis for Estimation of Measuring Error oi Orifice Flowmeter due to Swirling Flow (선회로 인한 오리피스 유량계의 계량오차 예측을 위한 삼차원 유동해석)

  • Kim Hong-Min;Kim Kwang-Yong;Her Jae-Young;Ha Young-Chul
    • Proceedings of the KSME Conference
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    • 2002.08a
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    • pp.79-82
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    • 2002
  • Three-dimensional pipe flows with elbows and tees for few different pipe fittings are calculated to estimate the effect of swirling flow on measuring accuracy of orifice flow meter. It is evaluated how the pressure difference across the orifice is dependent on the length of upstream straight pipe in a branch and how swirl intensity, swirl angel and axial velocity distribution affect the measuring error of orifice flowmeter. From the results, it is found that, regardless of flow rate specified in this calculation, the effect of the straight pipe length can be neglected for the lengths larger than thirty diameters although there still remain significant swirl at the orifice

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Effects of a Swirling and Recirculating Flow on the Combustion Characteristics in Non- Premixed Flat Flames

  • Jeong, Yong-Ki;Jeon, Chung-Hwan;Chang, Young-June
    • Journal of Mechanical Science and Technology
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    • v.18 no.3
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    • pp.499-512
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    • 2004
  • The effects of swirl intensity on non-reacting and reacting flow characteristics in a flat flame burner (FFB) with four types of swirlers were investigated. Experiments using the PIV method were conducted for several flow conditions with four swirl numbers of 0, 0.26, 0.6 and 1.24 in non-reacting flow. The results show that the strong swirling flow causes a recirculation, which has the toroidal structures, and spreads above the burner exit plane. Reacting flow characteristics such as temperature and the NO concentrations were also investigated in comparison with non-reacting flow characteristics. The mean flame temperature was measured as the function of radial distance, and the results show that the strong swirl intensity causes the mean temperature distributions to be uniform. However the mean temperature distributions at the swirl number of 0 show the typical distribution of long flames. NO concentration measurements show that the central toroidal recirculation zone caused by the strong swirl intensity results in much greater reduction in NO emissions, compared to the non-swirl condition. For classification into the flame structure interiorly, the turbulence Reynolds number and the Damkohler number have been examined at each condition. The interrelation between reacting and non-reacting flows shows that flame structures with swirl intensity belong to a wrinkled laminar-flame regime.

The Effects of Various Swirl Flows on Pulverized Petroleum Coke Combustion (미분 석유코크스연소기에서 스월강도변화가 연소과정에 미치는 영향)

  • Cha, Chun Loon;Lee, Ho Yeon;Hwang, Sang Soon
    • 한국연소학회:학술대회논문집
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    • 2014.11a
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    • pp.297-299
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    • 2014
  • Petroleum coke has high heating value and low price. Due to the steadily increasing demand for heavy oil processing, the production volume of petroleum coke tends to be expanded. The high availability and low price of petroleum coke have been strongly considered as candidate fuel for power generation facilities. However the high carbon content, high sulfur content and nitrogen content of petroleum fuel are known to produce relatively large quantity of CO2, high NOx and SO2 emission. In this work, a series of numerical simulations have been carried out in order to investigate the effects of swirl flow intensity on combustion furnace, which is most important operating condition. Results show that the temperature distribution was spatially uniform at about 1600K but high temperature region are located quite differently depending on swirl number. In addition, numerical temperature data was compared with experimental temperature data and its temperature difference shows less than 10%. On the other hand, discrepancy between numerical and experimental emission data were slightly large with necessities of improved emission model.

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A Review on Swirling Flow by Using Flow Visualization Techniques in the Circular Tubes (원형관 내에서 유동가시화 기법을 이용한 선회유동에 관한 연구고찰)

  • Chang, Tae-Hyun;Doh, Deog-Hee;Lee, Kwoon-Soo
    • Journal of the Korean Society of Visualization
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    • v.8 no.3
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    • pp.12-21
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    • 2010
  • Swirling flows are found in very wide range of applications, for examples, cyclone separators, spraying machines, heat exchangers and jet pumps, ect. Relatively, little work has been done on the swirl flow using flow visualization techniques. This study deals with many visualization techniques to study on swirling flow. These techniques are related to oil films methods, smoke, dye liquids, liquid crystal, stroboscope light, smoke wire, white light, naphthalene sublimation, LDV(lase doppler Velocimetry) and PIV(particle image velocimetry). The present work has handled single, annular, carved tube, swirl expansion and swirl wake using several visualization methods in the vertical and horizontal circular tube.

The Effect of Swirl Flow on Combustion Characteristics in a Marine Diesel Engine (박용 디젤기관에서 스월유동이 연소특성에 미치는 영향)

  • 김병현;박권하;이상수;성낙원
    • Journal of Advanced Marine Engineering and Technology
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    • v.24 no.2
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    • pp.38-49
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    • 2000
  • A diesel engine has been studied for many years to improve fuel economy and to reduce emissions as important factors governing the emission performance of diesel engines. This study addresses to swirl effects on combustion characteristics in a large diesel engine. The transport equations of flows and chemical reactions are given for fully compressible fluid. The simulations have been done for compression and expansion strokes and the results are given at several crank angles which are the angles at just before injection start, TDC, ATDC 90 and just before exhaust valve open. The results show that the strength of the swirl flow makes many effects on burning fuel and forming emissions.

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Combustion and Emission Characteristics in CNG Engine with SCV (SCV를 장착한 CNG 엔진의 연소 및 배출가스 특성)

  • 김진영;박원옥;공태원;하종률
    • Transactions of the Korean Society of Automotive Engineers
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    • v.11 no.3
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    • pp.1-6
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    • 2003
  • Natural gas is one of the promising alternative fuels because of the abundant deposits and the cleanness of emission gas. CNG has a lot of merits except lower burning speed has a slow disadvantage. One way to overcome the disadvantage is to raise a turbulence intensity. We give various intake for changing turbulence intensity in the cylinder by three kinds of swirl control valve with a way to raise a turbulence intensity. In the present study, a $1.8\ell$ conventional gasoline engine is modified to use a CNG as a fuel instead of gasoline. We try to virify combustion and emission characteristics in each engine parameters. Parameters of experimentation are equivalence ratio, spark timing and intake flow change. The results of this study are as swirl flows. In the case of adding swirl flow, burning speed and torque are increased. But NOx and THC concentration are increased a little respectively.

Analysis of Combustion Flow of LNG-Fueled Gas Turbine Swirl Burner (LNG 연료를 이용한 가스 터빈 연소기의 연소유동 해석)

  • Kim, Tae-Ho;Kang, Ki-Ha;Choi, Jeong-Yeol;Kim, Sung-Chul
    • Journal of the Korean Society of Combustion
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    • v.13 no.3
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    • pp.33-40
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    • 2008
  • Two- and Three- dimensional numerical simulations are carried out to understand the combustion characteristics of LNG-fueled gas turbine combustor for power generation using imported and domestic natural gases. Reacting flow characteristics of the swirl stabilized natural gas combustor were understood from the numerical results with the flow conditions selected from the gas turbine operation data. The thermal influences of different natural gases were very small and the fuel composition and flow rate were considered to be tuned well. The flow structures of the recirculation and combustion region was understood from the comparison of the two- and three-dimensional results. The complexity of the three-dimensional swirl flows inside the gas turbine combustor with multiple swirlers was understood those resulting from the interactions of the stage and pilot burners.

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