• Title/Summary/Keyword: Turbulent Steady Flow

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Thermal Performance Analysis and Optimization of Two-dimensional Trombe Wall Solar System (2차원 축열벽형 태양열시스템의 열성능해석 및 최적화)

  • 이원근;유성연;정명균
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.17 no.6
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    • pp.1609-1620
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    • 1993
  • A Study on the trombe wall system, a kind of passive solar systems, has been performed numerically. The system is treated as a two-dimensional steady turbulent natural convection including constant heat source per unit area. The numerical code, "PHOENICS, " was employed to analyze this conduction-convection conjugated heat transfer. The general mode of the flow field was examined, and the exchange of mass between two recirculating flows is found to be the major mechanism of the heat transfer. It is shown that the performance is affected by the changes in the geometrical factors-the thickness of the wall, the width between the windowand the wall, and size of the vents. Further analysis has been performed to show the optimal geometry with regard to the last two factors.o factors.

Numerical study on self-sustainable atmospheric boundary layer considering wind veering based on steady k-ε model

  • Feng, Chengdong;Gu, Ming
    • Wind and Structures
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    • v.30 no.1
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    • pp.69-83
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    • 2020
  • Modelling incompressible, neutrally stratified, barotropic, horizontally homogeneous and steady-state atmospheric boundary layer (ABL) is an important aspect in computational wind engineering (CWE) applications. The ABL flow can be viewed as a balance of the horizontal pressure gradient force, the Coriolis force and the turbulent stress divergence. While much research has focused on the increase of the wind velocity with height, the Ekman layer effects, entailing veering - the change of the wind velocity direction with height, are far less concerned in wind engineering. In this paper, a modified k-ε model is introduced for the ABL simulation considering wind veering. The self-sustainable method is discussed in detail including the precursor simulation, main simulation and near-ground physical quantities adjustment. Comparisons are presented among the simulation results, field measurement values and the wind profiles used in the conventional wind tunnel test. The studies show that the modified k-ε model simulation results are consistent with field measurement values. The self-sustainable method is effective to maintain the ABL physical quantities in an empty domain. The wind profiles used in the conventional wind tunnel test have deficiencies in the prediction of upper-level winds. The studies in this paper support future practical super high-rise buildings design in CWE.

Inflow Nozzle Conditions for Improving Vortex Tube Performance (보텍스튜브 성능향상을 위한 유입노즐 조건에 관한 연구)

  • Choi, Hoon-Ki;Yoo, Geun-Jong;Lim, Yun-Seung
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.17 no.2
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    • pp.68-76
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    • 2018
  • A vortex tube is a simple energy separating device that splits a compressed air stream into a cold and hot stream without any external energy supply or chemical reactions. The efforts of many researchers and designers have been focused on improvement of vortex tube efficiency by changing the parameters affecting vortex tube operation. The effective parameters are nozzle specifications and inflow pressure conditions. Effects of different nozzle cross-sectional area and number of nozzles are evaluated by computational fluid dynamics (CFD) analysis. In this study, CFD analysis of 3-D steady state and turbulent flow through a vortex tube was performed. We investigated the cold air mass flow rate, the cold air temperature, and the cold air heat transfer rate behavior of a vortex tube by utilizing seven straight nozzles and four inflow pressure conditions.

A Numerical Study on the Open Channel Flow with Plane Wall Jet Inlet Boundary Condition (평면벽면분류의 유입경계조건을 가지는 개수로 유동에 관한 수치적 연구)

  • 설광원;이상룡
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.13 no.2
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    • pp.287-298
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    • 1989
  • A numerical work was performed to study the flow behaviors of the open channel type flow with its geometric boundary conditions being similar to that of the Multi-Stage-Flash evaporator with and without a baffle. For the analysis, two-dimensional steady turbulent flow was assumed and the widely known k-.epsilon. turbulence model was usded. SIMPLE algorithm and the power difference scheme were used for the numerical approach. Numerical results generally agree with the previous experimental results though there are some uncertainties at far downstream and near the free surface due to the three dimensionality of the flow and surface waves. Without a baffle, the flow has basically the shape of the submerged plane wall jet with its upper boundary at downstream being sharply curved toward the free surface. For the flow with a baffle, recirculation flow patterns are observed at the upper inlet portion and at the backside of the baffle. For the case without a baffle, it was also confirmed that the ratio between the liquid level and the gate opening height is the most important parameter to determine the flow behavior.

NON-GREY RADIATIVE TRANSFER IN THE PHOTOSPHERIC CONVECTION : VALIDITY OF THE EDDINGTON APPROXIMATION

  • BACH, KIEHUNN
    • Journal of The Korean Astronomical Society
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    • v.49 no.1
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    • pp.1-8
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    • 2016
  • The aim of this study is to describe the physical processes taking place in the solar photosphere. Based on 3D hydrodynamic simulations including a detailed radiation transfer scheme, we investigate thermodynamic structures and radiation fields in solar surface convection. As a starting model, the initial stratification in the outer envelope calculated using the solar calibrations in the context of the standard stellar theory. When the numerical fluid becomes thermally relaxed, the thermodynamic structure of the steady-state turbulent flow was explicitly collected. Particularly, a non-grey radiative transfer incorporating the opacity distribution function was considered in our calculations. In addition, we evaluate the classical approximations that are usually adopted in the onedimensional stellar structure models. We numerically reconfirm that radiation fields are well represented by the asymptotic characteristics of the Eddington approximation (the diffusion limit and the streaming limit). However, this classical approximation underestimates radiation energy in the shallow layers near the surface, which implies that a reliable treatment of the non-grey line opacities is crucial for the accurate description of the photospheric convection phenomenon.

WIND DRIVEN RAIN IMPACT ON A TALL BUILDING FACADE

  • Kim, Jong-Dae;Oh, Jung-Keun;Park, Byong-Keun
    • 한국전산유체공학회:학술대회논문집
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    • 2010.05a
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    • pp.242-246
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    • 2010
  • To determine the trajectories and the impact of rain drops on the facade of a tall building, a particle tracking method is employed form steady state simulation of turbulent flow around the building. The simulation is performed for the upper part of the building comprising a detailed louver system. Rain is trapped at relative high rates on the roof and the penthouse, with Local Intensity Factors (LIF's) of the order of 1. The upper parapets and upper floors get a fair amount of wetting with LIF's of the order of 0.6. The wetting decreases downwards reaching values of 0.2 to 0.25 at the level of the louver system.

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An Aerodynamic Noise Reduction Design at Inter-coach Space of High Speed Trains Based on Biomimetic Analogy

  • Han, Jae-Hyun;Kim, Jung-Soo
    • International Journal of Railway
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    • v.4 no.3
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    • pp.74-79
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    • 2011
  • Recent years have witnessed speed up of moving vehicles such as high-speed of trains. Increase in speed entails concomitant increase in turbulent air flow which contributes toward increased aerodynamic noise. The proposed method for aerodynamic noise reduction is based on a biomimetic design of owl feather. The five morphological parameters of the owl feather are extracted from close observation, and simulation cases are constructed by applying design of experiments methodology. Swirling strength for each case is obtained through steady-state CFD analysis, and key morphological parameters that affect the turbulence are identified. Large eddy simulations (LES) are then performed on selected cases to predict the air turbulence. Different cases show varying vortex distributions which are expected to lead to varying aerodynamic noise levels.

The aero-acoustic noise reduction based on biomimetics : A case study (생체모방공학을 이용한 공력 소음 저감 기초 연구)

  • Han, Jae-H.;Kim, Tae-M.;Kim, Jung-S.
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2011.04a
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    • pp.144-151
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    • 2011
  • Recent years have witnessed speed up of moving vehicles such as high-speed of trains. Increase in speed entails concomitant increase in turbulent air flow which contributes toward aerodynamic noise. The proposed method for aerodynamic noise reduction is based on a biomimetic design of owl feather. The five morphological parameters of the owl feather is extracted from close observation, and simulation cases are constructed by applying design of experiments methodology. Swirling strength for each case is obtained through steady-state CFD analysis, and key morphological parameters that affect the turbulence are identified. Large eddy simulations (LES) are then performed on selected cases to predict the air turbulence. Different cases show varying vorticity distribution levels which is expected to lead to varying aerodynamic noise levels.

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Numerical Study of Passive Control with Slotted Blading in Highly Loaded Compressor Cascade at Low Mach Number

  • Ramzi, Mdouki;Bois, Gerard;Abderrahmane, Gahmousse
    • International Journal of Fluid Machinery and Systems
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    • v.4 no.1
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    • pp.97-103
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    • 2011
  • With the aim to increase blade loadings and stable operating range in highly loaded compressors, this article has been conducted to explore, through a numerical parametric study, the potential of passive control using slotted bladings in cascade configurations. The objective of this numerical investigation is to analyze the influence of location, width and slope of the slots and therefore identify the optimal configuration. The approach is based on two dimensional cascade geometry, low speed regime, steady state and turbulent RANS model. The results show the efficiency of this passive technique to delay separation and enhance aerodynamic performances of the compressor cascade. A maximum of 28.3% reduction in loss coefficient have been reached, the flow turning is increased with approximately $5^0$ and high loading over a wide range of angle of attack have been obtained for the optimized control parameter.

지면효과를 고려한 비행체에 따른 공력 특성 분석

  • Kim, Tae-Uk;Park, Da-Un
    • Proceeding of EDISON Challenge
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    • 2016.11a
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    • pp.58-62
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    • 2016
  • 본 연구에서는 지면효과의 영향을 비행체의 형상에 따라 비교하기 위해 에어포일, 플랩을 장착한 에어포일 그리고 플라잉디스크를 EDISON_CFD를 통해 해석하고자 한다. 받음각 $0^{\circ}$, $5^{\circ}$, $10^{\circ}$에 대하여 마하수 0.18, 단위 길이 당 레이놀즈수 $3.78{\times}10^{-5}/m$의 유동조건에서 2차원 범용 소프트웨어인 KFLOW_EDISION_13의 S-A Turbulent Model을 이용하여 지면과의 높이를 형상 코드길이를 기준으로 0.25c, 0.5c, 1c, 3c로 변경하면서 해석을 수행하였다. 그 결과 세 형상 모두 일반적인 지면효과인 지면과 가까울수록 양력계수는 증가, 항력계수는 감소하여 양항비가 증가하는 경향을 보여주었다. 하지만 일부 예외적인 부분을 확인하여 분석을 실시하였다.

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