• 제목/요약/키워드: CFD system

검색결과 1,616건 처리시간 0.03초

환기방식에 따른 지하주차장 공기오염도의 수치연구 (NUMERICAL STUDY OF AIR POLLUTION RATE DEPENDING ON TYPES OF VENTILATION SYSTEM IN UNDERGROUND PARKING LOT)

  • 임수정;장춘만;이광훈
    • 한국전산유체공학회:학술대회논문집
    • /
    • 한국전산유체공학회 2009년 춘계학술대회논문집
    • /
    • pp.208-214
    • /
    • 2009
  • 지하 복수층 주차장은 도시의 밀집화 및 자동차의 급격한 증가로 인한 토지부족 및 주차난을 해소할 수 있는 좋은 방법이다. 하지만 인체유해 배출가스의 집중으로 환기의 중요성이 대두되는 추세에도 불구하고 실제로는 시공이 완료 된 후에나 오염도 측정이 가능하다. 이러한 이유로 CFD 시뮬레이션으로 시공이전의 지하 복수층 주차장의 공기오염도를 예측했다. CFD 시뮬레이션은 예산과 시간을 절감한 공기오염도 예측이 가능하다. 실제의 당산근린공원의 지하주차장을 대상으로 오염도를 예측했다. 급기에만 강제유동을 일으키는 2종과 배기에만 강제유동을 일으키는 3종 기계환기법, 그리고 급배기에 강제유동을 일으키는 1종기계환기법을 각각 적용하여 공기오염도를 계산했다. 지하1층과 지하2층의 입구 및 출구유속을 10, 15m/s로 하여 실내평균연령과 실내평균환기효율을 살펴보았다. 계산결과는 급기와 배기에 강제유동을 동시에 일으키는 1종 기계환기법의 값과 비교하였다.

  • PDF

실린더형 기-액 원심분리기 내의 유동특성 연구를 위한 CFD 시뮬레이션 (CFD Simulation to Study Flow Characteristics in Cylindrical Gas-Liquid Cyclone Separator)

  • 박경도;박종천;김경미
    • 한국해양공학회지
    • /
    • 제28권4호
    • /
    • pp.280-287
    • /
    • 2014
  • In this paper, the numerical simulation of the gas-liquid flow in a cylinder cyclone separator is performed to investigate the flow characteristics using a commercial software, FLUENT, which solves the Reynolds-averaged Navier-Stokes(RaNS) equations. First, a single-phase flow with water in a gas-liquid cylinder cyclone(GLCC) separator is simulated and compared with the experiments(Farchi, 1990) and numerical simulations(Erdal, 1997). Then, the characteristics of the multi-phase flow for water-air, mud-only, and mud-air cases are discussed in the view point of the feasibilities for a mud handling system.

MEXNEXT 풍력발전기 풍동 시험에 대한 풍동 영향 분석 (Wind tunnel effect analysis for MEXICO wind turbine model)

  • 신형기;임종수;장문석
    • 한국신재생에너지학회:학술대회논문집
    • /
    • 한국신재생에너지학회 2011년도 춘계학술대회 초록집
    • /
    • pp.59.1-59.1
    • /
    • 2011
  • In this research, CFD calculation was implemented to analyze wind tunnel effect or rotor experiment in wind tunnel. One case included model wind turbine and all wind tunnel geometries. The other case include only rotor and nacelle system. Star-CCM+ was used for CFD analysis and rigid body motion around rotor area was applied to simulate rotating rotor. As for turbulence model, K-omega SST was used. The results were compared in 15m/s inflow condition. These results shows a good agreement with the measurement. Then, the result without wind tunnel was slightly different to the result with wind tunnel. Thus, in the case of Mexnex wind tunnel measurement, the wind tunnel don't affect the measurement result. Then, this wind tunnel and rotor size ratio can be reference for wind tunnel experiment of wind turbine rotor.

  • PDF

수술실내 공기감염억제를 위한 공조용 급배기구 위치 선정에 관한 연구 (A Study on the Diffuser Location for the Reduction of Airborne Infection in Operation Room)

  • 권순정;주영철;김천숙
    • 의료ㆍ복지 건축 : 한국의료복지건축학회 논문집
    • /
    • 제8권1호
    • /
    • pp.7-12
    • /
    • 2002
  • The air ventilation system of operation rooms has been studied to prevent the cross infection during the operation. Operation rooms and air ventilation systems of three University hospitals were investigated. The distribution of microbe was measured by cultivating air samples in the operation room. A two-dimensional model for the cross-section of an operation room was developed for the CFD(Computational Fluid Dynamics) analysis. The characteristics of air flow in the empty operation room and in occupied operation room were calculated by using a CFD program. The current diffuser location of an old hospital did not deliver the clean air to the operation part efficiently. A new method to locate diffusers that improve air venting with little increase of the cost of equipment was suggested.

  • PDF

소형 덕트 팬 항공기의 전산해석 및 공력특성 분석 (CFD SIMULATION AND ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF SMALL DUCTED FAN AIRCRAFT)

  • 김철완;최성욱;안석민
    • 한국전산유체공학회:학술대회논문집
    • /
    • 한국전산유체공학회 2010년 춘계학술대회논문집
    • /
    • pp.14-16
    • /
    • 2010
  • A Duct surrounding a fan is known to reduce the tip loss and increase the fan performance efficiency. It also reduces the fan noise drastically. Ducted fan, therefore, has been focused to be a promising candidate for high efficient propulsion system. In this study, a small plane having ducted fan which can be tilted for vertical take-off and landing, is analyzed by CFD and its aerodynamic characteristics are compared. Ductef fan aircraft has small range of angle of attack for mininum drag and duct design should be focused for efficient ducted fan aircraft.

  • PDF

CFD-ACE를 이용한 연료 전지 냉각판의 최적 설계 (Optimization of Fuel-cell stack design using CFD-ACE)

  • 홍민성;김종민
    • 한국공작기계학회:학술대회논문집
    • /
    • 한국공작기계학회 2003년도 추계학술대회
    • /
    • pp.14-18
    • /
    • 2003
  • Feul-cell system consists of fuel reformer, stack and energy translator. Among these parts, slack is a core part which produces electricity directly. In order to set a stack module, fabrication of appropriate stack, design of water flow path in stack, and control of coolant are needed. Especially, water or air is used as a coolant to dissipate heat. The different temperature of each electric cells after cooling and the high temperature of the stack affect the performance of the stack, Therefore, it is necessary that the relationship between coolant, healing rate, width of slack, properties of stack, and the shape of water flow path must be understood. For the optimal design, the computational simulation by CFD-ACE has been conducted and the resulting database has been constructed.

  • PDF

2엽형 수직축 풍력발전기의 유동해석 및 실험 비교 (AERODYNAMIC ANALYSIS AND COMPARISON OF EXPERIMENTAL DATA FOR 2-BLADED VERTICAL AXIS WIND TURBINE)

  • 황미현;김동현;이종욱;오민우;김명환;류경중
    • 한국전산유체공학회지
    • /
    • 제15권4호
    • /
    • pp.85-91
    • /
    • 2010
  • In this study, aerodynamic analyses based on unsteady computational fluid dynamics (CFD) have been conducted for a 2-bladed vertical-axis wind turbine (VAWT) configuration. Reynolds-averaged Navier-Stokes equations with standard $k-{\varepsilon}$ and SST $k-{\varepsilon}$ turbulence models are solved for unsteady flow problems. The experiment model of 2-bladed VAWT has been designed and tested in this study. Aerodynamic experiment of the present VAWT model are effectively conducted using the vehicle mounted testing system. The comparison result between the experiment and the computational fluid dynamics (CFD) analysis are presented in order to verify the accuracy of CFD modeling with different turbulent models.

래티스 볼쯔만 방법을 이용한 자동차 외부공력특성 연구 (Calculation of The Car Aerodynamic Characteristics Using Lattice-Boltzmann method)

  • 이병천;김무상;이창호
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2002년도 학술대회지
    • /
    • pp.561-564
    • /
    • 2002
  • For the reduction of fuel consumption of high speed, the aerodynamic drag must be reduced. In early vehicle design process, it is very important to have information about aerodynamic characteristics of design models. In this phase CFD methods are usually used to predict the aerodynamic forces. But commercial programs using turbulence models cannot give a good agreement with experimental result and have also problems with convergence. PowerFLOW employs a new technology called DIGITAL PHYSICS, which provides a different approach to simulating fluids. DIGITAL PHYSICS uses a lattice-based approach (extended from lattice-gas and lattice-Boltzmann methods) where time, space and velocity are discrete. This discrete system represents the Wavier-Stokes continuum behavior without the numerical instability Issues of traditional CFD solvers, such as convergence. In this paper, aerodynamic performance of vehicles are simulated using PowerFLOW by Exa and results are compared with experimental wind tunnel data.

  • PDF

A Practical Estimation of Static Stability of a Hovercraft

  • Park, Sun-Ho;Heo, Jae-Kyung;Yu, Byeong-Seok
    • Journal of Ship and Ocean Technology
    • /
    • 제10권3호
    • /
    • pp.27-35
    • /
    • 2006
  • The static stability of a high-speed hovercraft is estimated by model tests, simplified restoring moment equations and CFD. Well-known methods to increase the stability of hovercrafts are introduced. Roll and pitch moments of a scaled model with a skirt system are measured over inclination angles. The tests are performed on cushion at zero speed both on-land and over-water. To predict the static stability performance, simple restoring moment equations and CFD approach are introduced. Both shows a quantitative difference from the model test results, however, could be used as a design tool for relative comparison prior to model tests.

위그선 연구현황과 전산유체역학의 응용 (State-of-the-Art of WIG(Wing-In-Ground Effect) Ships and Application of the Computational Fluid Dynamics)

  • 강국진
    • 한국전산유체공학회:학술대회논문집
    • /
    • 한국전산유체공학회 2005년도 춘계 학술대회논문집
    • /
    • pp.14-19
    • /
    • 2005
  • The paper introduces the state-of-the art of WIG ship and application field of the CFD to WIG ship development. WIG ships are highly efficient and fast transport vehicles which take advantage of benefits of ground effect. Chapter 1 describes the characteristics of WIG ship. Chapter 2 reviews the research works of Russia, German, Chinese, Korea and etc. Chapter 3 explains the kind of WIG ship categorized by the main operational mode and take-off system. Chapter 4 describes about the application field of CFD to WIG ship development procedure.

  • PDF