• 제목/요약/키워드: Wall Jet

검색결과 361건 처리시간 0.033초

충돌 Jet에서 Rod 형상에 따른 유동특성의 PIV 계측에 의한 연구 (A Study on the Flow Characteristics according to the Shapes of Rod on Impinging Jet by PIV Measurement)

  • 나우정;정진도;송민근;이상범;손승우;주은선
    • Journal of Advanced Marine Engineering and Technology
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    • 제28권1호
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    • pp.152-161
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    • 2004
  • The thermal load is a very important problem to be solved in many industrial systems including the electronic equipment. Impinging Jets have been known to provide a large heat transfer rates on surface for many years. The turbulence enhancement of fluid flow is requested for the efficiency elevation of heat transfer. A study on flow fields by rods attached to the wall surface as a promoter of turbulence enhancement has been carried out. The exact analysis on chracteristics of impinging jet field is requested to obtain the optimum design of the impinging jet system. By visualizing the flow field and processing the high digital image by computer PIV can afford exact data on the velocity vector kinetic energy and turbulence intensity in the complex turbulence field. In this study. three kinds of rod shape such as square. triangle. and semicircle are selected as the turbulence promoter. Nozzle diameters are 10mm. 17mm. and 23mm. And the analysis of the flow characteristics due to the above rods is carried out at Re No. 2.000, 3.000. and 4,000 by PIV measurement. It is clarified that the rod setup is very useful to obtain the turbulence enhancement and the turbulence intensity according to the shapes of rod appears large in order of the shapes of rod such as square 〉 triangle 〉semicircle.

충돌제트를 갖는 회전원판 위 3차원 경계층의 난류특성 (I) - 평균유동장 - (Turbulence Characteristics of a Three-Dimensional Boundary Layer on a Rotating Disk with an Impinging Jet (I) - Mean Flow -)

  • 강형석;유정열;최해천
    • 대한기계학회논문집B
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    • 제22권9호
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    • pp.1277-1289
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    • 1998
  • The objective of the present study is to investigate experimentally the mean flow characteristics of the three-dimensional turbulent boundary layer over a rotating disk with an impinging jet at the center of the disk, which may be regarded as one of the simplest models for the flow in turbomachinery. A relatively strong radial outflow (crossflow) generated from the impinging jet is added to the radial outflow (crossflow) induced by the centrifugal force in order to create the three-dimensional boundary layer. A new calibration technique has been introduced to determine the velocity direction and magnitude using an I-wire probe, where the uncertainties are ${\pm}1.5^{\circ}$ and ${\pm}0.35\;m/s$, respectively, in the laminar boundary layer region, compared with the known exact solutions. The flow in the tangential direction is of similar type to that associated with a favorable pressure gradient, considering that no wake region appears in wall coordinate velocity profiles and the Clauser shape factor is between 4.0 and 5.3. The flow angle is significantly changed by the crossflow generated by the impinging jet.

Liquid Crystal을 이용한 원형충돌분류의 전열특성 연구 (Heat Transfer on a Heated Flat Plate by an Impinging Round Jet Using Liquid Crystal)

  • 오승묵;이상준
    • 대한기계학회논문집
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    • 제16권8호
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    • pp.1566-1574
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    • 1992
  • 본 연구에서는 원형수직 충돌분류에 의한 가열평판의 전열특성을 해석하기 위 하여 최근 표면온도 측정에 많이 사용되고 있는 liquid crystal을 이용하였다. 즉 liquid crystal의 감온특성과 영상처리 기법을 이용하여 레이놀즈수 및 노즐과 충돌판 사이의 거리(L/D) 변화에 따른 전열면의 온도장 변화를 측정하였다.

초기 횡방향 유동이 존재하는 충돌제트/유출냉각에서 원형핀이 설치된 유출면에서의 열/물질전달 특성 (Heat/Mass Transfer on Effusion Plate with Circular Pin Fins for Impingement/Effusion Cooling System with Intial Crossflow)

  • 홍성국;이동호;조형희
    • 대한기계학회논문집B
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    • 제29권7호
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    • pp.828-836
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    • 2005
  • Impingement/effusion cooling technique is used for combustor liner or turbine parts cooling in gas turbine engine. In the impingement/effusion cooling system, the crossflow generated in the cooling channel induces an adverse effect on the cooling performance, which consequently affects the durability of the cooling system. In the present study, to reduce the adverse effect of the crossflow and improve the cooling performance, circular pin fins are installed in impingement/effusion cooling system and the heat transfer characteristics are investigated. The pin fins are installed between two perforated plates and the crossflow passes between these two plates. A blowing ratio is changed from 0.5 to 1.5 for the fixed jet Reynolds number of 10,000 and five circular pin fin arrangements are considered in this study. The local heat/mass transfer coefficients on the effusion plate are measured using a naphthalene sublimation method. The results show that local distributions of heat/mass transfer coefficient are changed due to the installation of pin fins. Due to the generation of vortex and wake by the pin fin, locally low heat/mass transfer regions are reduced. Moreover, the pin fin prevents the wall jet from being swept away, resulting in the increase of heat/mass transfer. When the pin fin is installed in front of the impinging let, the blockage effect on the crossflow enhances the heat/mass transfer. However, the pin fin installed just behind the impinging jet blocks up the wall jet, decreasing the heat/mass transfer. As the blowing ratio increases, the pin fins lead to the higher Sh value compared to the case without pin fins, inducing $16\%{\~}22\%$ enhancement of overall Sh value at high blowing ratio of M=1.5.

회전반사판을 이용한 건물 외벽청소로봇 개발방향 연구 (Fundamental Study of the Building Exterior wall cleaning Robot using a spinning device)

  • 박수열;김균태
    • 한국건축시공학회:학술대회논문집
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    • 한국건축시공학회 2013년도 추계 학술논문 발표대회
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    • pp.224-225
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    • 2013
  • Most of the building exterior wall cleaning robots use a water jet device for spraying water. However this method is sprayed excessive water usage than water quantity required for cleaning. And setting weight of the water pump cleaning device increase the weight of the building exterior wall cleaning robot. Therefor, this paper suggest that the mechanisms scatter minimal cleaning water using a spinning device of the building exterior wall cleaning robot.

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충돌분무의 거동에 미치는 벽면곡률의 영향에 대한 수치해석 연구 (Numerical Study on the Effect of the Wall Curvature on the Behaviors of the Impinging Sprays)

  • 고권현;유홍선
    • 한국자동차공학회논문집
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    • 제12권3호
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    • pp.59-65
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    • 2004
  • In this paper a numerical study was performed for the effect of the wall curvature on the behaviors of fuel sprays impinging on the concave Surface. Actually, in the real diesel engines, a piston head has a curved shape for the purpose of the controlling the movement of fuel droplets and the mixture formation. For past decades, although many experimental and numerical works had been performed on the spray/wall impingement phenomena, the curvature effect of impinged wall was rarely investigated. The wall curvature affects on the behaviors of the secondary droplets generated by impingement and the concave wall obstructs the droplets to advance from the impinging site to outward. In present study, the simulation code was validated for the flat surface case and three cases of the different curvature were calculated and compared with the flat surface case for several parameters, such as the spray radius, the spray height and the position of vortex center of gas phase. The simulation results showed that the radial advance of the wall spray and the vortex is decreased with increasing the curvature. It was concluded that the curvature of the impinged wall significantly affects the behaviors of both the gas-phase and the droplet-phase.

SIDE-WALL-INLET 환기시스템 축사에서 유입구의 컨트롤을 위한 젯트모멘텀 (JET MOMENTUM CRITERIA FOR INLET CONTROL TO REDUCE WIND EFFECTS ON THE AIR DISTRIBUTION IN A SIDE-WALL-INLET VENTILATION SYSTEM)

  • 이성현
    • 한국생물환경조절학회:학술대회논문집
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    • 한국생물환경조절학회 1997년도 가을 심포지움 및 학술논문발표요지
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    • pp.51-55
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    • 1997
  • 국내의 축사는 윈치커튼의 위치를 조절하여 줌으로써 내부의 기류를 교환하는 개방형 축사가 대부분을 차지하고 있다. 개방형 축사의 환기는 외기풍속의 영향에의해 내부 기류의 흐름이 형성되어 바람이 없는 고온기에는 내부의 기류혼합이 잘 되지 않기 때문에 고온으로 인한 내부의 환경이 열악하다. 따라서 자연환기 축사에 배기팬 또는 입기팬을 설치하는 조합형 환기 축사가 주를 이를 것으로 판단된다. (중략)

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Wind pressure measurements on a cube subjected to pulsed impinging jet flow

  • Mason, M.S.;James, D.L.;Letchford, C.W.
    • Wind and Structures
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    • 제12권1호
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    • pp.77-88
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    • 2009
  • A pulsed impinging jet is used to simulate the gust front of a thunderstorm downburst. This work concentrates on investigating the peak transient loading conditions on a 30 mm cubic model submerged in the simulated downburst flow. The outflow induced pressures are recorded and compared to those from boundary layer and steady wall jet flow. Given that peak winds associated with downburst events are often located in the transient frontal region, the importance of using a non-stationary modelling technique for assessing peak downburst wind loads is highlighted with comparisons.

축대칭 환형 분사식 이젝터 제트 유동 특성의 수치적 연구 (A NUMERICAL STUDIES ON THE FLOW PROPERTIES OF AXI-SYMMETRIC ANNULAR BELL TYPE EJECTOR-JETS)

  • 박근홍;권세진
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2006년도 추계 학술대회논문집
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    • pp.185-188
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    • 2006
  • An investigation of the ejector-jets focusing on its flow properties was carried out by varying the geometric parameters. The area ratio of the primary nozzle, AR that was tested in the present measurement was 2.17 and 3.18, while the ratio of the length to the diameter of the duct downstream the primary nozzle inlet, L/D had values of 3.41, 6.82, and 10.23. For the frame work of flow characteristics, the wall pressures distribution of ejector-jet was investigated by experiment for basic study of ejector-jet performance. In result, terminal shock location and existence of series of oblique shocks are recognized. In this study, CFD analysis was conducted at the same time. And as a result of comparison experiment data with CFD analysis, the physical phenomena of ejector-jets were estimated.

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고온고압 세라믹 여과재 탈진 과정의 유동 해석 (Analysis for the Pulse-Jet Cleaning Flow of a Hot Gas Ceramic-Filter Element)

  • 박인욱;류제형;최도형
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1998년도 춘계 학술대회논문집
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    • pp.110-115
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    • 1998
  • An axisymmetric Navier-Stokes procedure has been developed to analyze the pulse jet flow in a ceramic filter unit for the dust dislodging process. Using Baldwin-Lomax turbulence model as a closure relationship, the SIAF(Scalar Implicit Approximate Factorization) algorithm together with the ${\delta}^k-Correction$ iterative time marching scheme is adopted to solve the unsteady compressible Navier-Stokes equations. After some validation tests, the code has been applied to solve the pulse jet flow and examine the effects of geometry and reservoir pressure condition on the pressure level inside the filter unit. To avoid dealing with the uncertainty of such factors as the cohesion of the collected dust and the adhesion of the dust to the medium and also to simplify the analysis, the filter wall is assumed to be impermeable. The results for various test cases are presented.

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