• 제목/요약/키워드: Turbulence effect

검색결과 851건 처리시간 0.026초

태양열 공기가열 집열기에 의한 난방 실내공간의 열유동 특성 해석 (Analysis on Characteristics of Thermal Flow for Heating Indoor Space by Air-heating Collector using Solar Heat)

  • 양영준
    • 한국산업융합학회 논문집
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    • 제25권2_2호
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    • pp.271-278
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    • 2022
  • The solar energy has been widely used to reduce the fossil fuel and prevent the environmental pollution. The renewable energy including solar heat tends to spread due to carbon neutrality for main country of the world. Targets of solar collector are usually acquisitions of hot water or hot air. Especially, air-heating collector using solar heat is known as the technology for obtaining hot air. This study aims to investigate of characteristics of thermal flow when the hot air by air-heating collector using solar heat flows inside of indoor space. The thermal flow of heating indoor space was simulated using ANSYS-CFX program and thus the behaviors of hot air in indoor space were evaluated with standard k-𝜀 turbulence model. As the results, as the inlet velocity was increased, the behaviors of hot air became simple, and temperature range of 25~75℃ had almost no effect on behavior of flow. As the inlet temperature was increased, the temperature curve of indoor space from bottom to top was changed from linear to quadratic. Furthermore, it was confirmed that inlet velocity as well as inlet temperature also should be considered to heat indoor space equally by air-heating collector using solar heat.

Integrated risk assessment method for spent fuel road transportation accident under complex environment

  • Tao, Longlong;Chen, Liwei;Long, Pengcheng;Chen, Chunhua;Wang, Jin
    • Nuclear Engineering and Technology
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    • 제53권2호
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    • pp.393-398
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    • 2021
  • Current risk assessment of Spent Nuclear Fuel (SNF) transportation has the problem of the incomplete risk factors consideration and the general particle diffusion model utilization. In this paper, the accident frequency calculation and the detailed simulation of the accident consequences are coupled by the integrated risk assessment method. The "man-machine-environment" three-dimensional comprehensive risk indicator system is established and quantified to characterize the frequency of the transportation accidents. Consideration of vegetation, building and turbulence effect, the standard k-ε model is updated to simulate radioactive consequence of leakage accidents under complex terrain. The developed method is applied to assess the risk of the leakage accident in the scene of the typical domestic SNF Road Transportation (SNFRT). The critical risk factors and their impacts on the dispersion of the radionuclide are obtained.

Numerical investigations on winglet effects on aerodynamic and aeroacoustic performance of a civil aircraft wing

  • Vaezi, Erfan;Fijani, Mohammad Javad Hamedi
    • Advances in aircraft and spacecraft science
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    • 제8권4호
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    • pp.303-330
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    • 2021
  • The paper discusses the effect of the winglets on the aerodynamic and aeroacoustic performance of Boeing 737-800 aircraft by numerical approach. For this purpose, computational fluid dynamics and fluent commercial software are used to solve the compressible flow governing equations. The RANS method and the K-ω SST turbulence model are selected to simulate the subsonic flow around the wing with acceptable accuracy and low computational cost. The main variables of steady flow around the simple and blended wing in constant atmospheric conditions are computed by numerical solution of governing equations. The solution of the acoustic field has also been accomplished by the broad-band acoustic source model. The results reveal that adding a blended winglet increases the pressure difference near the wingtip,which increases the lift force. Also, the blended winglet reduces the power and magnitude of vorticities around the wingtip, which reduces the wing's drag force. The effects of winglets on aerodynamic forces lead to a 3.8% increase in flight range and a 3.6% increase in the maximum payload of the aircraft. Also, the acoustic power level variables on the surfaces and fields around the wing have been investigated integrally and locally.

버티포트 건축을 위한 2개의 고층 건물 간 거리 변화가 빌딩풍에 미치는 영향 (Effect of the Distance Between Two Buildings on the Building Wind for the Vertiport Construction)

  • 최인서;한철희
    • 융복합기술연구소 논문집
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    • 제12권1호
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    • pp.25-30
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    • 2022
  • 도심항공교통은 다수의 전기추진 수직이착륙 항공기가 이착륙 가능한 버티포트가 필요하다. 빌딩풍은 고층건물 주변부에서 발생하는 강풍으로 항공기 이착륙과정에서 항공기의 비행 안전성을 크게 훼손시킬수 있다. 본 연구에서는 항공기 이착륙시 발생할 비행안정성 분석을 위하여 먼저 빌딩풍 주변의 유동특성을 분석하는 연구를 수행하였다. 유동해석은 상용CFD 소프트웨어인 SimericsMP를 사용하였으며, 난류 모델은 k-ε RNG 모델을 사용하였다. 해석방법의 타당성을 검증하기 위하여 CAARC 빌딩모델의 표면 압력 계산결과를 풍동시험 결과와 비교⋅검증하였다. 두 개의 고충빌딩이 있는 상황을 가정한 후, 빌딩풍이 빌딩 주변부의 속도분포 변화에 미치는 영향을 분석하였다. 두 개의 고층 건물 사이의 거리가 증가하는 경우 와들 사이의 상호작용이 감소하는 것을 확인했다. 향후 본 연구를 확장하여 다양한 형상의 고충건물이 밀집해 있는 도심지역에 대한 유동해석 연구를 진행하고자 한다.

Shape optimization of corner recessed square tall building employing surrogate modelling

  • Arghyadip Das;Rajdip Paul;Sujit Kumar Dalui
    • Wind and Structures
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    • 제36권2호
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    • pp.105-120
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    • 2023
  • The present study is performed to find the effect of corner recession on a square plan-shaped tall building. A series of numerical simulations have been carried out to find the two orthogonal wind force coefficients on various model configurations using Computational Fluid Dynamics (CFD). Numerical analyses are performed by using ANSYS-CFX (k-ℇ turbulence model) considering the length scale of 1:300. The study is performed for 0° to 360° wind angle of attack. The CFD data thus generated is utilised to fit parametric equations to predict alongwind and crosswind force coefficients, Cfx and Cfy. The precision of the parametric equations is validated by employing a wind tunnel study for the 40% corner recession model, and an excellent match is observed. Upon satisfactory validation, the parametric equations are further used to carry out multiobjective optimization considering two orthogonal force coefficients. Pareto optimal design results are presented to propose suitable percentages of corner recession for the study building. The optimization is based on reducing the alongwind and crosswind forces simultaneously to enhance the aerodynamic performance of the building.

Thermo-hydraulic Effect of Tubular Heat Exchanger Fitted with Perforated Baffle Plate with Rectangular Shutter-type Deflector

  • Md Atiqur Rahman
    • Korean Chemical Engineering Research
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    • 제62권2호
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    • pp.191-199
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    • 2024
  • A study was conducted on a tubular heat exchanger to improve its heat transfer rate by using a novel baffle plate design with discontinuous swirling patterns. The design consisted of perforated baffle plates with rectangular air deflectors positioned at varying angles. The tubes in the heat exchanger were arranged in a consistent alignment with the airflow direction and exposed to a uniform heat flux on their surfaces. Each baffle plate included sixteen deflectors inclined at the same angle and arranged in a clockwise pattern. This arrangement induced a swirling motion of the air inside a circular duct where the heated tubes were located, leading to increased turbulence and improved heat transfer on the tube surfaces. The spacing between the baffle plates was adjusted at different pitch ratios, and the Reynolds number was controlled within a range of 16,000 to 29,000. The effects of pitch ratios and inclination angles on the heat exchanger's performance were analyzed. The results indicated that using a baffle plate with rectangular deflectors inclined at 30° and a pitch ratio of 1.2 resulted in an average increase of 1.29 in the thermal enhancement factor.

Parametric study of population balance model on the DEBORA flow boiling experiment

  • Aljosa Gajsek;Matej Tekavcic;Bostjan Koncar
    • Nuclear Engineering and Technology
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    • 제56권2호
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    • pp.624-635
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    • 2024
  • In two-fluid simulations of flow boiling, the modeling of the mean bubble diameter is a key parameter in the closure relations governing the intefacial transfer of mass, momentum, and energy. Monodispersed approach proved to be insufficient to describe the significant variation in bubble size during flow boiling in a heated pipe. A population balance model (PBM) has been employed to address these shortcomings. During nucleate boiling, vapor bubbles of a certain size are formed on the heated wall, detach and migrate into the bulk flow. These bubbles then grow, shrink or disintegrate by evaporation, condensation, breakage and aggregation. In this study, a parametric analysis of the PBM aggregation and breakage models has been performed to investigate their effect on the radial distribution of the mean bubble diameter and vapor volume fraction. The simulation results are compared with the DEBORA experiments (Garnier et al., 2001). In addition, the influence of PBM parameters on the local distribution of individual bubble size groups was also studied. The results have shown that the modeling of aggregation process has the largest influence on the results and is mainly dictated by the collisions due to flow turbulence.

2차원 수치모형을 이용한 원형군락 하류의 흐름특성 수치모의 (Numerical Simulation of Flow Characteristics behind a Circular Patch of Vegetation using a Two-Dimensional Numerical Model)

  • 김형석;박문형
    • 한국수자원학회논문집
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    • 제48권11호
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    • pp.891-903
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    • 2015
  • 본 연구는 식재된 개수로에서 흐름특성을 모의할 수 있는 수심 적분된 2차원 수치모형을 이용하여 원형 식생역 주변의 흐름을 수치모의하였다. 식생영향을 고려하기 위해 식생항력 항을 지배방정식에 추가하였고 다양한 식생체적비율(SVF) 조건에 따른 수치모의를 수행하였다. 흐름이 원형 식생역을 통과하고 하류에 저유속 구간인 후류영역(wake region)을 형성하며 식생체적비율이 0.08 이상이면 재순환 영역이 발생하였다. 재순환 발생위치는 식생체적비율이 감소하면 식생역에서 더욱 하류로 이동하였다. 후류영역을 지나 원형 식생역 양 측면에서 유발된 전단층들의 상호작용에 의해 von $K{\acute{a}}rm{\acute{a}}n$ 와열이 발생하였다. 원형 식생역 하류에서 발생하는 와류는 식생체적비율이 0.08 이상이 되면 나타나기 시작하였고 발생위치는 난류운동에너지가 최대값을 보이는 위치와 일치하였다. 최대 난류운동에너지는 식생체적비율이 감소하면 줄어드는 것으로 나타났고 최대값의 발생위치는 점점 하류로 이동하였다.

Unsteady 2-D flow field characteristics for perforated plates with a splitter

  • Yaragal, Subhash C.
    • Wind and Structures
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    • 제7권5호
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    • pp.317-332
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    • 2004
  • Wind tunnel experiments were conducted under highly turbulent and disturbed flow conditions over a solid/perforated plate with a long splitter plate in its plane of symmetry. The effect of varied level of perforation of the normal plate on fluctuating velocities and fluctuating pressures measured across and along the separation bubble was studied. The different perforation levels of the normal plate; that is 0%, 10%, 20%, 30%, 40% and 50% are studied. The Reynolds number based on step height was varied from $4{\times}10^3$ to $1.2{\times}10^4$. The shape and size of the bubble vary with different perforation level of the normal plate that is to say the bubble is reduced both in height and length up to 30% perforation level. For higher perforation of the normal plate, bubble is completely swept out. The peak turbulence value occurs around 0.7 to 0.8 times the reattachment length. The turbulence intensity values are highest for the case of solid normal plate (bleed air is absent) and are lowest for the case of 50% perforation of the normal plate (bleed air is maximum in the present study). From the analysis of data it is observed that $\sqrt{\overline{u^{{\prime}2}}}/(\sqrt{\overline{u^{{\prime}2}}})_{max}$, (the ratio of RMS velocity fluctuation to maximum RMS velocity fluctuation), is uniquely related with dimensionless distance y/Y', (the ratio of distance normal to splitter plate to the distance where RMS velocity fluctuation is half its maximum value) for all the perforated normal plates. It is interesting to note that for 50% perforation of the normal plate, the RMS pressure fluctuation in the flow field gets reduced to around 60% as compared to that for solid normal plate. Analysis of the results show that the ratio [$C^{\prime}_p$ max/$-C_{pb}(1-{\eta})$], where $C^{\prime}_p$ max is the maximum coefficient of fluctuating pressure, $C_{pb}$ is the coefficient of base pressure and ${\eta}$ is the perforation level (ratio of open to total area), for surface RMS pressure fluctuation levels seems to be constant and has value of about 0.22. Similar analysis show that the ratio $[C^{\prime}_p$ max/$-C_{pb}(1-{\eta})]$ for flow field RMS pressure fluctuation levels seems to be constant and has a value of about 0.32.

U-튜브형 횡동요 감쇄 탱크의 자유수면 해석기법 개발에 관한 연구 (Development of Numerical Computation Techniques for the Free-Surface of U-Tube Type Anti-roll Tank)

  • 이상의
    • 해양환경안전학회지
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    • 제28권7호
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    • pp.1244-1251
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    • 2022
  • 지난 10년간 선박의 횡동요 복원력 상실에 의한 해양사고가 지속해서 증가하고 있어, 횡동요 운동을 효과적으로 줄일 수 있는 장치가 필요한 실정이다. 횡동요 감쇄 탱크는 단순한 설치만으로 횡동요 저감을 가져오는 대표적인 수동형 제어장치로 그 장점이 널리 알려져 있다. 따라서 본 연구에서는 U-튜브형 횡동요 감쇄 탱크의 수치해석 기법을 개발하고자 한다. 특히, 해석기법의 검증을 위해 자유수면 높이를 실험을 통해 계측하였다. 수치해석기법은 메쉬 의존성, 난류모델 (k-𝜖, k-𝜔, Reynolds Stress Model), 시간 간격 크기 및 반복횟수 등의 영향을 비교하여 개발하였다. 최종적으로 개발된 해석기법은 Realizable k-𝜖이 난류 모델에 10-2s 수준의 시간 간격 크기와 15회의 반복횟수를 적용하였다. 2가지의 U-튜브형 감쇄 탱크의 조건에서 계측된 자유수면 높이를 이용하여 개발된 해석기법을 검증하였다. 본 연구의 수치해석은 RANS 기반 상용 해석 Solver인 STAR-CCM+ (ver. 17.02)을 이용하였다.