• 제목/요약/키워드: 3-Dimensional Flow Phenomena

검색결과 124건 처리시간 0.023초

밸브위치에 따른 4밸브 엔진 연소실 내부의 스월비와 텀블비의 거동 (The behavior of swirl and tumble ratio in the combustion chamber of 4-valve engine with valve positions)

  • 김성준;이천식;전봉준;이용일
    • 산업기술연구
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    • 제19권
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    • pp.51-57
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    • 1999
  • This research has an object to find out how the position of inlet valve influence swirling and tumbling of turbulence inside the combustion chamber of 4 valve engine. The computational analysis of three dimensional complicated turbulence flow in the cylinder is done by the KIVA-3V program to carry out this object. One use 6 valve positions with the bowl type of piston cavity. The swirl ration and the tumbling ratio of flow filed are evaluated quantitatively to find out how each valve position influence flow phenomena in the combustion chamber during the intake and compression processes.

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축류 압축기 날개열의 팁 영역에 관한 3차원 수치해석을 통한 난류모형 비교 (Comparison of Turbulence Models through Three Dimensional Numerical Soultion for the Tip Region of an Axial Compressor Cascade)

  • 최일곤;맹주성
    • 한국전산유체공학회지
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    • 제2권2호
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    • pp.18-25
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    • 1997
  • A pressure-based Navier-Stokes numerical solver was used to compare solutions of the k-ε/RNG k-ε turbulence models. An efficient grid generation scheme, the transient grid generation with full boundary control, was used to solve the flows in the tip clearance region. Results indicate that the calculations using k-ε model captures various phenomena related to the tip clearance with good accuracy.

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풍력 발전기용 블레이드 공력해석에 대한 연구 (A Study of Aerodynamic Analysis for the Wind Turbine Rotor Blade using a general CFD code)

  • 박상규;김진범;김태우;여창호;권기영;오시덕
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2009년도 춘계학술대회 논문집
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    • pp.516-520
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    • 2009
  • This study describes aerodynamic characteristics for the HAWT (Horizontal Axis Wind Turbine) rotor blade using general CFD(Computational Fluid Dynamics) code. The boundary conditions for analysis are validated with the experimental result by the NREL (National Renewable Energy Laboratory)/NASA Ames wind tunnel test for S809 airfoil. In the case of wind turbine rotor blade, complex phenomena are appeared such as flow separation and re-attachment. Those are handled by using a commercial flow analysis tool. The 2-equation k-$\omega$ SST turbulence model and transition model appear to be well suited for the prediction. The 3-dimensional phenomena in the HAWT rotor blade is simulated by a commercial 3-D aerodynamic analysis tool. Tip vortex geometry and Radial direction flows along the blade are checked by the analysis.

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HOT CHANNEL ANALYSIS CAPABILITY OF THE BEST-ESTIMATE MULTI-DIMENSIONAL SYSTEM CODE, MARS 3.0

  • JEONG J.-J.;BAE S. W.;HWANG D. H.;LEE W. J.;CHUNG B. D.
    • Nuclear Engineering and Technology
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    • 제37권5호
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    • pp.469-478
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    • 2005
  • The subchannel analysis capability of MARS, a multi-dimensional thermal-hydraulic system code, has been enhanced. In particular, the turbulent mixing and void drift models for the flow-mixing phenomena in rod bundles were improved. Then, the subchannel analysis feature was combined with the existing coupled system thermal-hydraulics (T/H) and 3D reactor kinetics calculation capability of MARS. These features allow for more realistic simulations of both the hot channel behavior and the global system T/H behavior. Using the coupled features of MARS, a coupled analysis of a main steam line break (MSLB) is carried out for demonstration purposes. The results of the calculations are very reasonable and promising.

GIS를 이용한 낙동강-금호강 합류부의 2차원 유한요소해석 (The 2D Finite Element Analysis in Nakdong-Kumho River Junction using GIS)

  • 황재홍;한건연;남기영;최승용
    • 한국지리정보학회지
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    • 제12권3호
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    • pp.21-34
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    • 2009
  • 홍수 시 흐름은 기본적으로 2차원 흐름으로서 이 때 하천 흐름의 수위와 유속 분포는 1차원 하천 모형으로 적절한 결과를 도출하기 어렵다. 이에 본 연구에서는 GIS를 이용하여 낙동강의 합류점에 대한 2차원 유한요소망을 구축하고 RMA-2모형을 이용하여 모의를 수행하였다. 이를 위해 모형의 매개변수들이 해석결과에 미치는 영향을 검토하였으며, 모형의 적용성을 검토하기 위해 금호강 합류부에 대해 흐름해석을 실시하고 검증하였다. 또한 하천의 단면 변화에 따른 흐름변화를 판단하기 위하여 과거 단면과 최근 단면에 대해 모의를 실시하고 비교 검토하였다. 그 결과 합류부에 대한 2차원 모형의 적용성을 검증하고 단변변화의 영향이 수위에 미치는 영향을 확인하여, 향후 합류부 처리, 하구부 처리, 제방축조 등에 효율적으로 활용될 수 있을 것으로 판단된다.

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Unsteady Aerodynamic Loads on High Speed Trains Passing by Each Other

  • Hwang, Jae-Ho;Lee, Dong-Ho
    • Journal of Mechanical Science and Technology
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    • 제14권8호
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    • pp.867-878
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    • 2000
  • In order to study unsteady aerodynamic loads on high speed trains passing by each other 350km/h, three-dimensional flow fields around trains during the crossing event are numerically simulated using three-dimensional Euler equations. Roe's FDS with MUSCL interpolation is employed to simulate wave phenomena. An efficient moving grid system based on domain decomposition techniques is developed to analyze the unsteady flow field induced by the restricted motion of a train on a rail. Numerical simulations of the trains passing by on the double-track are carried out to study the effect of the train nose-shape, length and the existence of a tunnel on the crossing event. Unsteady aerodynamic loads-a side force and a drag force-acting on the train during the crossing are numerically predicted and analyzed. The side force mainly depends on the nose-shape, and the drag force depends on tunnel existence. Also. a push-pull (i.e.impluse force) force successively acts on each car and acts in different directions between the neighborhood cars. The maximum change of the impulsive force reaches about 3 tons. These aerodynamic force data are absolutely necessary to evaluate the stability of high speed multi-car trains. The results also indicate the effectiveness of the present numerical method for simulating the unsteady flow fields induced by bodies in relative motion.

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교행하는 고속전철의 비정상 공기력에 대한 수치적 연구 (Computational Study on Unsteady Aerodynamic Loads on Crossing Train)

  • 황재호;이동호
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집B
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    • pp.599-604
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    • 2000
  • In order to study unsteady aerodynamic loads on high speed trains passing by each other at the speed of 350km/h, three-dimensional flow fields around trains during the crossing event are numerically simulated using the three-dimensional Euler equations. The Roe's FDS with MUSCL interpolation is employed to simulate wave phenomena properly. An efficient moving grid system based on domain decomposition techniques is developed to analyze the unsteady flow field induced by the restricted motion of a train on a rail. The numerical simulations of the trains passing by on the double-track are carried out to study the effect of the train nose-shape, the train length and the existence of tunnel when the crossing event occur. Unsteady aerodynamic loads side force and drag force-acting on the train during the crossing are numerically predicted and anlayzed. It is found that the strength of the side force mainly depends on the nose-shape, and that of drag force on tunnel existence. And it is observed that the push-pull like impulsive force successively acts on each car and acts in different directions between the neighborhood cars. The maximum change of the impulsive force reaches about 3 tons. These aerodynamic force data are absolutely necessary for the evaluation of the stability of the high speed multi-car train. The results also indicate the effectiveness of the present numerical method for the simulation of unsteady flow field induced by the bodies in the relative motion.

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유체충격력 예측을 위한 3차원 다상류 시뮬레이션의 응용 (Applications of Three-Dimensional Multiphase Flow Simulations for Prediction of Wave Impact Pressure)

  • 정세민;황성철;박종천
    • 한국해양공학회지
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    • 제27권2호
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    • pp.39-46
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    • 2013
  • In this study, the impact loads on tank walls by sloshing phenomena and on a tall structure in a three-dimensional rectangular tank were predicted using multiphase flow simulations. The solver was based on the CIP/CCUP (Constraint interpolation CIP/CIP combined unified procedure) method, and the THINC-WLIC (Tangent hyperbola for interface capturing-weighted line interface calculation) scheme was used to capture the air-water interface. For the convection terms of the Navier-Stokes equations, the USCIP (Unsplit semi-lagrangian CIP) method was adopted. The results of simulations were compared with those of experiments. Overall, the comparisons were reasonably good.

액체 램제트 엔진의 3차원 분무 및 연소 반응 해석 (Analysis of Three Dimensional Liquid Ramjet Engine with Spray and Combustion)

  • 오대환;임상규;손창현;이충원
    • 한국추진공학회지
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    • 제3권2호
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    • pp.18-24
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    • 1999
  • 액체 램제트 연소기는 흡입공기와 분무, 혼합 그리고 이에 따른 연소 등 일련의 과정에 따라 다수의 복잡한 현상들이 상호 밀접하게 관련되어 있으며, 이러한 반응 및 비반응 유동 특성을 파악하기 위해서 2차원 및 3차원 연소기 형상에 대해서 수치적 실험을 수행하였다 격자구성은 연소기에 공기를 공급하고 연료를 분무하는 공기 유입관 영역과 연소실 영역, 그리고 출구 대기 영역으로 나누어 격자를 생성시켰다. 비반응 유동해석을 통해서 연소실내의 선회영역 유동특성은 2차원과 3차원이 크게 차이가 남을 알 수 있었다. 반응 유동 해석에서는 분무 모델의 적용 유무에 따라 연소 형태가 크게 변화하였다. 연료의 분사위치를 유입관의 위쪽에 준 경우와 아래쪽에 준 두 가지 경우를 비교하였으며, 유입관의 아래쪽에 연료의 분사위치를 준 경우가 연소의 안정화에 필요한 재순환 영역으로의 연료의 유입이 잘 되어 유입관 위쪽에 연료를 분사시키는 것보다 좋은 분사위치임을 알 수 있었다.

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2차원 종형 언덕 주위의 유동 및 확산현상에 관한 수치해석 연구 (Numerical Simulations of the Flowfield and Pollutant Dispersion over 2-D Bell-Shaped Hills)

  • 박근;박원규
    • 한국전산유체공학회지
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    • 제3권1호
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    • pp.63-72
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    • 1998
  • The numerical simulations of flowfield and pollutant dispersion over two-dimensional hills of various shapes are described. The Reynolds-averaged Wavier-Stokes equations and concentration diffusion equation based on the gradient diffusion theory have been applied to the atmospheric shear flow over the bell-shaped hills which are basic components of the complex terrain. The flow characteristics such as velocity profiles of the geophysical boundary layer, speed-up phenomena, mean pollutant concentration profiles are compared with experimental data to validate the present numerical procedure and it has been found that the present numerical results agree well with experiments and other numerical data. It has been also found that the distributions of ground level concentration are strongly influenced by the source location and height.

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