• 제목/요약/키워드: CFD:Computational Fluid Dynamics

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유전알고리즘과 ε-NTU 모델을 이용한 다양한 열교환기의 최적설계 및 성능해석 (Heat Exchanger Ranking Program Using Genetic Algorithm and ε-NTU Method for Optimal Design)

  • 이순호;김민성;하만영;박상후;민준기
    • 대한기계학회논문집B
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    • 제38권11호
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    • pp.925-933
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    • 2014
  • 오늘날 고성능컴퓨터로 인해 많은 산업분야에서 전산해석이 사용되고 있다. 하지만 정해진 컴퓨터자원과 시간에 의해 3 차원 풀 스케일 해석에서는 많은 어려움 등이 있다. 본 연구에서 ${\varepsilon}-NTU$ 식과 열교환기 성능의 데이터베이스를 이용해 열교환기의 성능예측프로그램을 개발하였다. 다양한 타입의 열교환기 형상정보와 성능데이터베이스를 구축하였고, 이를 바탕으로 정해진 작동 조건에서 열교환기의 성능을 계산하였다. 계산된 정보를 바탕으로 최적의 사이즈를 갖는 형상을 찾기 위해 유전알고리즘(Genetic Algorithm)을 이용하였다. 계산을 위해 상용 소프트웨어인 MATLAB 과 REFPROP 이 사용되었다.

온풍난방기용 Gun식 가스버너의 스월유동장에 대한 5공압력프로브의 측정 (Measurements of Five-Hole Pressure Probe on Swirling Flow Fields of Gun-Type Gas Burner for Furnace)

  • 김장권;오석형
    • 대한기계학회논문집B
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    • 제38권12호
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    • pp.991-997
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    • 2014
  • 이 연구는 Gun식 가스버너의 스월유동장을 연소실과 화염이 없는 상태에서 직선형 5공압력프로브의 측정을 통해 고찰하였다. 직선형 5공압력프로브에 의한 속도 및 정압성분들은 넌널링 교정방법에 의해 연산하였으며, X형 열선프로브와 전산유체역학의 해석에 의한 결과들과 비교하였다. 결과적으로 Gun식 가스버너의 중심부에서 스월유동장에 대해 5공압력프로브에 의한 속도 및 정압의 측정값들은 비교적 X형 열선프로브에 의한 경우보다는 좋은 성능을 보였으나 전산유체역학의 해석에 의한 경우보다는 다소 미흡한 결과를 보였다.

단순 형상 해양플랜트 내의 수소의 분산 시뮬레이션 (Dispersion Simulation of Hydrogen in Simple-shaped Offshore Plant)

  • 석준;허재경;박종천
    • 한국해양공학회지
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    • 제27권5호
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    • pp.105-114
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    • 2013
  • Lots of orders of special vessels and offshore plants for developing the resources in deepwater have been increased in recent. Because the most of accidents on those structures are caused by fire and explosion, many researchers have been investigated quantitatively to predict the cause and effect of fire and explosion based on both experiments and numerical simulations. The first step of the evaluation procedures leading to fire and explosion is to predict the dispersion of flammable or toxic material, in which the released material mixes with surrounding air and be diluted. In particular turbulent mixing, but density differences due to molecular weight or temperature as well as diffusion will contribute to the mixing. In the present paper, the numerical simulation of hydrogen dispersion inside a simple-shaped offshore structure was performed using a commercial CFD program, ANSYS-CFX. The simulated results for concentration of released hydrogen are compared to those of experiment and other simulation in Jordan et al.(2007). As a result, it is seen that the present simulation results are closer to the experiments than other simulation ones. Also it seems that the hydrogen dispersion is closely related to turbulent mixing and the selection of the turbulence model properly is significantly of importance to the reproduction of dispersion phenomena.

고체 추진제와 점화기 간 간격에 따른 유동 특성 (Flow Characteristics with Distance between Solid Propellant Grain and Igniter)

  • 강동기;최재성;이형진
    • 한국추진공학회지
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    • 제22권2호
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    • pp.96-107
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    • 2018
  • 고체추진기관 내에 점화기와 추진제 그레인 간격에 따라 화염에 의해 발현되는 내부 유동 형태에 대해 전산유체해석(CFD)를 이용하여 살펴보았다. 실린더형과 슬롯형 추진제 그레인에 대해 실린더형은 간격 1 mm, 3 mm, 5 mm, 슬롯형은 점화기의 화염 분출구가 넓은 간격에 위치한 경우와 좁은 간격에 위치한 경우에 대해 수치 해석을 수행하였다. 실린더형은 간격이 좁을수록 점화기와 추진제 사이에 고압력이 형성되며, 점화기 말단 부근에서 압력 강하 또한 상대적으로 크게 나타났다. 실린더형은 간격에 영향을 받았으나, 슬롯형은 화염 분출구 위치에 관계없이 압력 형태가 유사하게 나타났으며, 실린더형 간격 5 mm와 유사한 결과를 보였다.

상용 CFD 프로그램을 이용한 풍력터빈 축소모델 출력계수 검증 및 후류 해석 (Validation of Power Coefficient and Wake Analysis of Scaled Wind Turbine using Commercial CFD Program)

  • 김병수;백인수;유능수
    • 한국태양에너지학회 논문집
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    • 제35권1호
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    • pp.35-43
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    • 2015
  • A numerical simulation on the wake flow of a wind turbine which is a scaled version of a multi-megawatt wind turbine has been performed. Two different inlet conditions of averaged wind speed including one below and one above the rated wind speed were used in the simulation. Steady-state pitch angles of the blade associated with the two averaged wind speeds were imposed for the simulation. The steady state analysis based on the Reynolds averaged Navier-Stokes equations with the method of frame motion were used for the simulation to find the torque of the rotor and the wake field behind the wind turbine. The simulation results were compared with the results obtained from the wind tunnel testing. From comparisons, it was found that the simulation results on the turbine power are pretty close to the experimental values. Also, the wake results were relatively close to the experimental results but there existed some discrepancy in the shape of velocity deficit. The reason for the discrepancy is considered due to the steady state solution with the frame motion method used in the simulation. However, the method is considered useful for solutions with much reduced calculation time and reasonably good accuracy compared to the transient analysis.

MULTI-SCALE MODELING AND ANALYSIS OF CONVECTIVE BOILING: TOWARDS THE PREDICTION OF CHF IN ROD BUNDLES

  • Niceno, B.;Sato, Y.;Badillo, A.;Andreani, M.
    • Nuclear Engineering and Technology
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    • 제42권6호
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    • pp.620-635
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    • 2010
  • In this paper we describe current activities on the project Multi-Scale Modeling and Analysis of convective boiling (MSMA), conducted jointly by the Paul Scherrer Institute (PSI) and the Swiss Nuclear Utilities (Swissnuclear). The long-term aim of the MSMA project is to formulate improved closure laws for Computational Fluid Dynamics (CFD) simulations for prediction of convective boiling and eventually of the Critical Heat Flux (CHF). As boiling is controlled by the competition of numerous phenomena at various length and time scales, a multi-scale approach is employed to tackle the problem at different scales. In the MSMA project, the scales on which we focus range from the CFD scale (macro-scale), bubble size scale (meso-scale), liquid micro-layer and triple interline scale (micro-scale), and molecular scale (nano-scale). The current focus of the project is on micro- and meso-scales modeling. The numerical framework comprises a highly efficient, parallel DNS solver, the PSI-BOIL code. The code has incorporated an Immersed Boundary Method (IBM) to tackle complex geometries. For simulation of meso-scales (bubbles), we use the Constrained Interpolation Profile method: Conservative Semi-Lagrangian $2^{nd}$ order (CIP-CSL2). The phase change is described either by applying conventional jump conditions at the interface, or by using the Phase Field (PF) approach. In this work, we present selected results for flows in complex geometry using the IBM, selected bubbly flow simulations using the CIP-CSL2 method and results for phase change using the PF approach. In the subsequent stage of the project, the importance of effects of nano-scale processes on the global boiling heat transfer will be evaluated. To validate the models, more experimental information will be needed in the future, so it is expected that the MSMA project will become the seed for a long-term, combined theoretical and experimental program.

CFD를 이용한 KRISO 추진효율 향상 장치(K-duct) 형상 특성에 관한 연구 (A Study on the Shape of KRISO Propulsion Efficiency Improvement Devices(K-duct) using CFD)

  • 김진욱;서성부
    • 대한조선학회논문집
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    • 제55권6호
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    • pp.474-481
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    • 2018
  • This paper is to compare by numerical analysis the flow characteristics and propulsion performance of stern with the shape change of K-duct, a pre-swirl duct developed by Korea Research Institute of Ships & Ocean Engineering (KRISO). First, the characteristics of the propeller and the resistance and self-propulsion before and after the attachment of the K-duct to the ship were verified and the validity of the calculation method was confirmed by comparing this result with the model test results. After that, resistance and self-propulsion calculations were performed by the same numerical method when the K-duct was changed into five different shapes. The efficiency of the other five cases was compared using the delivery horsepower in the model scale and the flow characteristics of the stern were analyzed as the velocity and pressure distributions in the area between the duct end and the propeller plane. For the computation, STAR-CCM +, a general-purpose flow analysis program, was used and the Reynolds Averaged Navier-Stokes (RANS) equations were applied. Rigid Body Motion (RBM) method was used for the propeller rotating motion and SST $k-{\omega}$ turbulence model was applied for the turbulence model. As a result, the tangential velocity of the propeller inflow changed according to the position angle change of the stator, and the pressure of the propeller hub and the cap changes. This regulated the propeller hub vortex. It was confirmed that the vortex of the portion where the fixed blade and the duct meet was reduced by blunt change.

OpenFOAM을 이용한 EOM 기반 2차원 수치 파 생성에 관한 파라메트릭 연구 (A Parametric Study on EOM-based 2D Numerical Wave Generation using OpenFOAM)

  • 문성호;이성욱;백광준;권창섭
    • 대한조선학회논문집
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    • 제55권6호
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    • pp.490-496
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    • 2018
  • The consistency of the initially designed waves in the domain is essential for accurate calculation of the added resistance in waves through CFD. In particular, unwanted reflected waves at domain boundaries can cause incorrect numerical solutions due to the superposition with initially designed waves. Euler Overlay Method(EOM) is one of the methods for reducing wave reflections by adding an additional source term to momentum and phase conservation equations, respectively. In this study, we apply the Euler Overlay Method(EOM) to the open-source CFD library, OpenFOAM(R), to simulate the accurate free-surface waves in the domain and the parametric study is performed for efficient implementation of Euler Overlay Method(EOM). Considering that the damping efficiency depends on the selection of the overlay parameter in the added source terms, the size of overlay zone and the wave steepness, the influences of these factors are tested through the wave elevation measured at constant time intervals in the 2D numerical wave tank. Through this process, guidelines for selection of optimal overlay parameter and overlay zone size that can be applied according to the scaling law are finally presented.

다양한 수직방향 무게중심을 고려한 사항 중 탱커 선체에 작용하는 유체력에 관한 연구 (Study on Hydrodynamic Forces Acting on Tanker Hull with Consideration of Various Vertical Centers of Gravity in Drift Test)

  • 박태출;이성욱;백광준;문성호
    • 한국해양공학회지
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    • 제32권6호
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    • pp.433-439
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    • 2018
  • An investigation was conducted to determine whether the changes in the maneuvering forces and moments acting on a hull could be affected by changing the vertical center of gravity (VCG) of a tanker. The changes in the hydrodynamic forces and moment acting on a hull according to the restraint conditions of motion were examined using CFD for cases where the VCG was located at the design draught (100% of draught), under the design draught (75% of draught), and at half of the design draught (50% of draught). The following motion restraint conditions were selected: (1) fixed restraints for everything; (2) heave, pitch, and roll free restraint; and (3) heave and pitch free restraints. It was found that restraint condition (2) had the best agreement with the model experiment results. In addition, it was found that the hydrodynamic forces and moment acting on the hull with restraint condition (2) could be greatly affected in the model tests and CFD calculations by the various configurations for the vertical center of gravity of the hull. Finally, it was concluded that the location of the vertical center of gravity of the hull could be an important factor when more accurate hydrodynamic maneuvering forces and moment are estimated.

대심도 복층터널 화재연기 확산지연장치 설치간격 및 차폐율에 따른 화재연기 지연효과 연구 (A Study on the Delay Effect of Smoke Diffusion by the Installation Intervals and the Blockage Ratio of the Fire Smoke Diffusion Delay Device in a Great Depth Underground Double-Deck Tunnel)

  • 양용원;한재희;이윤택;문정주;신태균
    • 한국자원공학회지
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    • 제55권6호
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    • pp.596-603
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    • 2018
  • 국내 도심지의 도로는 차량수요 증가 및 부도심의 발달로 교통정체가 빈번히 발생되고 있다. 이를 해결하기 위한 방안으로 대심도 복층터널 시공을 위한 설계가 계획되고 있지만 주로 소형차전용으로써 터널높이가 낮고 단면이 작아 화재발생 시 인명피해가 발생될 가능성이 높다. 따라서 본 연구에서는 대심도 복층터널의 화재 시 인명피해 발생 최소화 방안으로 화재연기 확산지연장치 개발하였으며, 확산지연장치의 효과를 극대화할 수 있는 최적 설치간격 및 차폐율을 찾기 위해 3차원 전산수치해석(CFD)을 이용하여 Case Study를 수행하였다. 수행결과 확산지연장치의 설치간격이 짧을수록 지연효과가 높아졌지만 일정거리 이상에서는 효율변화가 미비한 경향이 발견되었고, 차폐율이 클수록 화재연기 지연효과가 높아지는 경향이 나타났지만, 차폐율이 작은 경우에는 설치간격에 따른 화재연기의 지연효과의 차이는 미소한 것으로 분석되었다.