• 제목/요약/키워드: jet velocity

검색결과 835건 처리시간 0.032초

제트홴의 이격거리에 따른 터널내 환기특성에 관한 수치적 연구 (Effects of the Distance between Jet Fans on the Ventilation Performance in a Road Tunnel)

  • 김정엽
    • 한국유체기계학회 논문집
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    • 제14권4호
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    • pp.25-30
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    • 2011
  • The jet fan is generally used to add thrust in the longitudinal ventilation system of road tunnel and the geometric conditions of jet fan such as the distance from tunnel wall have an effect on the performance of ventilation system. Numerical analyses on the flow in tunnel caused by operation of jet fan are presented to study the ventilation characteristics in tunnel. While the distance between jet fans in parallel installed in tunnel is changed 0.5 L/D to 3.0 L/D, the flowrate and mean velocity through tunnel are calculated for each cases. As the distance between jet fans increases, the flowrate through tunnel increases asymptotically and the momentum of tunnel flow is alike.

사각형제트와 2차원제트의 거동해석의 비교 평가 (Comparative Evaluation of Behavior Analysis of Rectangular Jet and Two-dimensional Jet)

  • 권석재;조홍연;서일원
    • 대한토목학회논문집
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    • 제26권6B호
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    • pp.641-649
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    • 2006
  • 본 연구에서는 PIV를 이용하여 측정한 평균유속장의 실험결과에 근거하여 10의 종횡비를 갖는 3차원 순수사각형제트의 거동을 고찰하였다. 장축상의 횡분포에서 안장형 분포가 관찰되었다. 점원개념으로부터 유도된 이론적인 중심선유속의 식은 측정된 중심선유속과 잘 일치하였으며 원류핵영역, 2차원영역, 그리고 축대칭영역의 분할을 제시하였다. 이러한 이론적인 중심선유속의 감소에 의해 분할된 2차원영역의 범위가 천이영역에 비해 상대적으로 작게 관찰되었다. 작은 종횡비를 갖는 사각형제트의 거동이나 실제 해양의 깊은 수심에서 다공확산관을 통해 방류되는 하 폐수의 거동을 예측하기 위한 2차원모형의 적용은 2차원영역을 지난 천이영역과 축대칭영역에서 중대한 오차를 야기할 수 있다. 2차원영역에서 가우스 상수가 보존되는 경향을 보였으며 2차원영역의 끝 지점에서 확장률이 감소함을 알 수 있었다. 중심선유속으로 무차원화 된 중심선 난류 강도는 초기에 급격히 증가하였고 높은 레이놀즈수에서 상대적으로 높은 난류강도를 보여주었다.

Experimental study on the condensation of sonic steam in the underwater environment

  • Meng, Zhaoming;Zhang, Wei;Liu, Jiazhi;Yan, Ruihao;Shen, Geyu
    • Nuclear Engineering and Technology
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    • 제51권4호
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    • pp.987-995
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    • 2019
  • Steam jet condensation is of great importance to pressure suppression containment and automatic depressurization system in nuclear power plant. In this paper, the condensation processes of sonic steam jet in a quiescent subcooled pool are recorded and analyzed, more precise understanding are got in direct contact condensation. Experiments are conducted at atmospheric pressure, and the steam is injected into the subcooled water pool through a vertical nozzle with the inner diameter of 10 mm, water temperature in the range of $25-60^{\circ}C$ and mass velocity in the range of $320-1080kg/m^2s$. Richardson number is calculated based on the conservation of momentum for single water jet and its values are in the range of 0.16-2.67. There is no thermal stratification observed in the water pool. Four condensation regimes are observed, including condensation oscillation, contraction, expansion-contraction and double expansion-contraction shapes. A condensation regime map is present based on steam mass velocity and water temperature. The dimensionless steam plume length increase with the increase of steam mass velocity and water temperature, and its values are in the range of 1.4-9.0. Condensation heat transfer coefficient decreases with the increase of steam mass velocity and water temperature, and its values are in the range of $1.44-3.65MW/m^2^{\circ}C$. New more accurate semi-empirical correlations for prediction of the dimensionless steam plume length and condensation heat transfer coefficient are proposed respectively. The discrepancy of predicted plume length is within ${\pm}10%$ for present experimental results and ${\pm}25%$ for previous researchers. The discrepancy of predicted condensation heat transfer coefficient is with ${\pm}12%$.

연속탈진형 충격기류식 여과집진장치의 여과포 유효탈진거리 예측 (A Study on Prediction of On-line Type Pulse Air Jet Bag Filter Effective Pulsing Distance)

  • 손정삼;서정민;박정호
    • 한국환경과학회지
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    • 제32권8호
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    • pp.555-561
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    • 2023
  • A study is to predict the effective pulsing distance following to the pulsing pressure, nozzle diameter, filtration velocity using numercial analysis techniques and use it as an efficient operation condition and economic data for on-line type pulse air jet bag filter. Filtration area 6 m2 condition, calculate filter resistance coefficient for simulation through the primary experiments using coke dust. For CFD simulation, analysis pulsing characteristics about nozzle diameter, filtration velocity and pulsing pressure. The maximum pulsing length of on-line type pulse air jet bag filter, in 10mm nozzle, filtration velocity 1.5m/min and pulsing pressure 5 bar conditions, is 2,285 mm, maximum length is 76.2% of the total filter bag, which is sufficient to pulsing. In 12mm nozzle, pulsing pressure 5 bar and filtration area 1.22 m2 conditions, the maximum pulsing length of on-line type pulse air jet bag filter is 1,744~2,952 mm, and the maximum length is 2,952 mm indicates pulsing air can be reached to the bottom of filter bag. When the nozzle diameter is increased 8mm to 10mm, maximum pulsing length is extended 40~47%, and increased 10mm to 12 mm, maximum pulsing length is extended 10~17%. For effective pulsing, over the 5bar of pulsing pressure and larger than 10 mm of nozzle diameter are required.

합성제트 기반의 유량 공급 장치에 대한 수치적 연구 (NUMERICAL STUDY ON SYNTHETIC-JET-BASED FLOW SUPPLYING DEVICE)

  • 박명우;이준희;김종암
    • 한국전산유체공학회지
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    • 제20권1호
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    • pp.77-83
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    • 2015
  • Flow characteristics of synthetic jet based flow supplying devices have been computationally investigated for different device shapes. Jet momentum was produced by the volume change of a cavity by two piezoelectric-driven diaphragms. The devices have additional flow path compared with the original synthetic jet actuator, and these flow path changes the flow characteristics of synthetic jet actuator. Four non-dimensional parameters, which were functions of the shapes of the additional flow path, were considered as the most critical parameters in jet performance. Comparative studies were conducted to compare volume flow rate and jet velocity. Computed results were solved by 2-D incompressible Navier-Stokes solver with k-w SST turbulence model. Detailed computations revealed that the additional flow path diminishes suction strength of the synthetic jet actuator. In addition, the cross section area of the flow path has more influence over the jet performances than the length of the flow path. Based on the computational results, the synthetic jet based flow supplying devices could be improved by applying suitable shape of the flow path.

분배계통에 따른 지하주차장 환기설비 성능의 예측

  • 김경환;이재헌;오명도;김종필
    • 설비공학논문집
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    • 제13권10호
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    • pp.982-992
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    • 2001
  • In this paper, the performance of ventilation equipments in enclosed parking garages were investigated for several air distribution systems by numerical method. Air change effectiveness of the non-mixing system was 0.42. It meant that more supply air as much as the design supply air was needed to maintain good indoor air quality. In the high speed nozzle ventilating system which is most expensive one, air change effectiveness was 0.54. Therefore this system satisfied to ventilation design. In the jet fan ventilating systems, air change effectiveness for jet fan ventilating system-A with 18 jet fans and jet fan ventilating system-B with 6 jet fans in circulation mixing arrangement were 0.565 and 0.42 respectively. Jet fan ventilating system-C with 6 jet fans in transport mixing arrangement was 0.535. Jet fan ventilating system-A and jet fan ventilating system-C met the ventilation design. But velocity in jet fan ventilating system-A was over 2.0m/s which is inappropriate in human comfort. Therefore this system is not proper to ventilation. Jet fan ventilating system-C was the optimum one for enclosed parking garages among 5 systems examined in this paper.

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Proposed large-scale modelling of the transient features of a downburst outflow

  • Lin, W.E.;Orf, L.G.;Savory, E.;Novacco, C.
    • Wind and Structures
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    • 제10권4호
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    • pp.315-346
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    • 2007
  • A preceding companion article introduced the slot jet approach for large-scale quasi-steady modelling of a downburst outflow. This article extends the approach to model the time-dependent features of the outflow. A two-dimensional slot jet with an actuated gate produces a gust with a dominant roll vortex. Two designs for the gate mechanism are investigated. Hot-wire anemometry velocity histories and profiles are presented. As well, a three-dimensional, subcloud numerical model is used to approximate the downdraft microphysics, and to compute stationary and translating outflows at high resolution. The evolution of the horizontal and vertical velocity components is examined. Comparison of the present experimental and numerical results with field observations is encouraging.

다양한 $k-{\varepsilon}$ 난류모델과 Skew-Upwind 기법에 의한 단이 진 벽면분류에 대한 수치해석 (Numerical Analyses on Wall-Attaching Offset Jet with Various Turbulent $k-{\varepsilon}$ Models and Skew-Upwind Scheme)

  • 서호택;부정숙
    • 대한기계학회논문집B
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    • 제24권2호
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    • pp.224-232
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    • 2000
  • Four turbulent $k-{\varepsilon}$ models (i.e., standard model, modified models with streamline curvature modification and/or preferential dissipation modification) are applied in order to analyze the turbulent flow of wall-attaching offset jet. For numerical convergence, this paper develops a method of slowly increasing the convective effect induced by skew-velocity in skew-upwind scheme (hereafter called Partial Skewupwind Scheme). Even though the method was simple, it was efficient in view of convergent speed, computer memory storage, programming, etc. The numerical results of all models show good prediction in first order calculations (i.e., reattachment length, mean velocity, pressure), while they show some deviations in ·second order (i.e., kinetic energy and its dissipation rate). Like the previous results obtained by upwind scheme, the streamline curvature modification results in better prediction, while the preferential dissipation modification does not.

메탄 비예혼합 상호작용 화염의 특성 (Characteristics of methane non-premixed multiple jet flames)

  • 이병준;김진현
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 추계학술대회
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    • pp.1365-1370
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    • 2004
  • It has been reported that if eight small nozzles are arranged along the circle of 40 $^{\sim}$ 72 times the diameter of single nozzle, the propane non-premixed flames are not extinguished even in 200m/s, In this research, experiments were extended to the methane flame. Nine nozzles were used- eight was evenly located along the perimeter of the imaginary circle and one at the geometric center. The space between nozzles, s, the exit velocity and the role of the jet from the center nozzle were considered. On the contrary to the propane non-premixed case, the maximum blowout velocity for the methane diffusion flame was achieved when small amount of fuel is supplied through the center nozzle and s/d equals around 21. In the laminar region, the flame attached at the center nozzle anchored the outer lifted flames.

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