• 제목/요약/키워드: CFD Fluent

검색결과 510건 처리시간 0.027초

로켓 노즐의 열전달계수 비교 연구 (Comparative Studies of Heat Transfer Coefficients for Rocket Nozzle)

  • 함희철;강윤구
    • 한국추진공학회지
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    • 제16권2호
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    • pp.42-50
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    • 2012
  • 열전달 연구의 목적은 온도와 열유속 분포를 보다 정확하게 예측하는 것이다. 이를 위해 상용 CFD 코드인 FLUENT를 사용하여 2종류의 노즐에 대해 질량유속비와 압력비를 계산하였으며, 실험결과와 잘 일치하였다. 또한 1종류의 노즐에 대해 FLUENT를 사용한 노즐 벽면에서의 열전달계수 계산결과는 노즐 축소부에서 실험결과 보다 약간 크게 예측되었으나 확대부에서는 잘 일치하고 있다. Bartz식을 이용한 열전달계수 계산결과는 전체적으로 실험결과 보다 크게 예측되었다. 계산결과가 실험결과와 차이를 보이는 원인은 노즐 내 급가속 유동에 의한 층류화, 난류모델 및 격자구성 등을 고려해 볼 수 있다.

Investigation on the wall function implementation for the prediction of ship resistance

  • Park, Sunho;Park, Se Wan;Rhee, Shin Hyung;Lee, Sang Bong;Choi, Jung-Eun;Kang, Seon Hyung
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제5권1호
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    • pp.33-46
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    • 2013
  • A computational fluid dynamics (CFD) code, dubbed SNUFOAM, was developed to predict the performance of ship resistance using a CFD tool kit with open source libraries. SNUFOAM is based on a pressure-based cell-centered finite volume method and includes a turbulence model with wall functions. The mesh sensitivity, such as the skewness and aspect ratio, was evaluated for the convergence. Two wall functions were tested to solve the turbulent flow around a ship, and the one without the assumption of the equilibrium state between turbulent production and dissipation in the log law layer was selected. The turbulent flow around a ship simulated using SNUFOAM was compared to that by a commercial CFD code, FLUENT. SNUFOAM showed the nearly same results as FLUENT and proved to be an alternative to commercial CFD codes for the prediction of ship resistance performance.

수직형 지중 열교환기의 현장 열응답 시험과 CFD 해석 비교 (The Comparison of the In-Situ Thermal Response Tests and CFD Analysis of Vertical-type Geothermal Heat Exchanger)

  • 심용섭;이희상
    • 한국산학기술학회논문지
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    • 제14권7호
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    • pp.3164-3169
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    • 2013
  • 본 연구에서는 수직형 지중 열교환기의 3차원 CFD 해석 기법을 제안하여 2개소의 현장 열응답 시험과 비교하였다. CFD 해석 비교를 위해 GAMBIT을 이용하여 지중과 지중 열교환기 형상을 모델링하였으며, 상용코드인 FLUENT를 사용하여 3차원 열전달 유동 해석을 수행하였다. 2개소의 현장 열응답 시험에서 도출된 지중 유효 열전도도와 지중 초기온도를 경계조건으로 사용하였으며, 시간에 따른 지중 열교환기의 입구온도 변화는 profile을 사용하여 실제 조건을 모사하였다. CFD 해석 결과 2개소의 지중 열교환기 출구온도는 $0.5^{\circ}C$ 범위 내에서 예측하였고, 기울기는 1.6% 이내에서 적절히 예측하였다. 향후 CFD 해석 기법을 활용하여 지중 열교환기 깊이, 형상 및 배열 변화 등에 따른 성능예측에 활용하고자 한다.

지상 경계층 풍동 설계를 위한 CFD의 적용 (Application of CFD to Design Atmospheric Boundary Layer Wind Tunnel)

  • 장병희
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2001년도 추계 학술대회논문집
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    • pp.37-43
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    • 2001
  • The methods of atmospheric boundary layer generation in test section were reviewed. To utilize conventional aerodynamic wind tunnels as atmospheric wind tunnels, boundary layer growth should be accelerated. To achieve this, improvement of boundary layer generation devices is required and it might be done by CFD. In this respect, CFD application cases in boundary generation devices were reviewed and potential areas were considered. Some cases are tried by Fluent 5 code.

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입자추적기법을 이용한 침전지의 효율 평가 (Estimation of Settling Efficiency in Sedimentation Basin Using Particle Tracking Method)

  • 이길성;김상훈
    • 한국수자원학회논문집
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    • 제37권4호
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    • pp.293-304
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    • 2004
  • 침전지는 수처리 공정에서 중요한 조작 중 하나이며, 침전지내에서는 응집과 침전이 일어남에 따라 입자의 크기분포가 변하는 복잡한 현상이 발생한다. 따라서 침전지의 효율적인 설계나 운영을 위해서는 이러한 현상에 대해 이해해야만 하며, 침전효율의 극대화를 위한 연구가 필요하다. 본 연구에서는 침전지내의 흐름을 모의하기 위하여 범용 CFD 프로그램인 FLUENT를 이용하였으며, 침전효율을 평가하기 위하여 FLUENT에서 제공되는 입자추적기법을 사용하였다. 또한 침전지의 형상을 지나치게 단순화시키는 기존의 연구와는 달리 본 연구에서는 실제 현장에서 사용되는 규모와 침전지내 인자들 (유입부 정류벽, 유출부 트라프 등)이 수치모의에 최대한 반영되었으며, 현장실험의 결과를 바탕으로 민감도 분석을 수행해 수치모의에 사용되는 매개 변수들을 보정하였다. 민감도 분석 결과 입자의 직경이 입자의 밀도에 비해서 민감도가 큰 것으로 나타났고, 침전효율이 실헐결과와 가장 잘 일치할 때의 직경값을 결정해본 결과 입자의 직경값이 26.5 $\mu\textrm{m}$로 나타났다.

CFD를 이용한 KVLCC1의 Circular Motion Test 시뮬레이션 (Circular Motion Test Simulation of KVLCC1 Using CFD)

  • 신현경;정재환
    • 대한조선학회논문집
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    • 제47권3호
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    • pp.377-387
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    • 2010
  • In this study, the turbulent free surface around KVLCC1 employed in the circular motion test simulation is numerically calculated using a commercial CFD(Computational Fluid Dynamics) code, FLUENT. Also, hydrodynamic forces and yaw moments around a ship model are calculated during the steady turning. Numerical simulations of the turbulent flows with free surface around KVLCC1 have been carried out by use of RANS equation based on calculation of hydrodynamic forces and yaw moments exerted upon the ship hull. Wave elevation is simulated by using the VOF method. VOF method is known as one of the most effective numerical techniques handling two-fluid domains of different density simultaneously. Boundary layer thickness and wake field are changed various yaw velocities of ship model during the steady turning. The calculated hydrodynamic forces are compared with those obtained by model tests.

A CFD Study of Roadside Barrier Impact on the Dispersion of Road Air Pollution

  • Jeong, Sang Jin
    • Asian Journal of Atmospheric Environment
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    • 제9권1호
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    • pp.22-30
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    • 2015
  • This study evaluated road shape and roadside barrier impact on near-road air pollution dispersion using FLUENT computational fluid dynamics (CFD) model. Simulated road shapes are three types, namely at-grade, depressed, and filled road. The realizable k-${\varepsilon}$ model in FLUENT CFD code was used to simulate the flow and dispersion around road. The selected concentration profile results were compared with the wind tunnel experiments. The overall concentration profile results show good agreement with the wind tunnel results. The results showed that noise barriers, which positioned around the at-grade road, decrease the horizontal impact distance (In this study, the impact distance was defined as the distance from road surface origin coordinate to the position whose mass fraction is 0.1.) lower 0.33~0.65 times and change the vertical air pollution impact distance larger 2.0~2.27 times than those of no barrier case. In case of filled road, noise barriers decrease the horizontal impact distance lower 0.24~0.65 times and change the vertical air pollution impact distance larger 3.33~3.55 times than those of no barrier case. The depressed road increase 1.53~1.68 times the vertical air pollution impact distance. It contributes the decrease of horizontal air pollution impact distance 0.32~0.60 times compare with no barrier case.

2차원 미세 포켓이 있는 무한장 Slider Bearing의 CFD 해석 (CFD Analysis of an Infinitely Long Slider Bearing with Two-Dimensional micro-Pockets)

  • 박태조;황윤건;손자덕;정호경
    • Tribology and Lubricants
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    • 제25권1호
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    • pp.43-48
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    • 2009
  • It is reported by many researchers that the textured bearing surfaces, where many tiny micro-pockets or enclosed recesses were incorporated, can enhance the load support and reduce friction force. Recently, the basic lubrication mechanism of micro-pocketed parallel surfaces are explained in terms of "inlet suction" using continuity equation and simply cavitation condition. However, it is required that more actual cavitation condition in the pocket region should be applied to estimate exact bearing performance. In this paper, a commercial computational fluid dynamics (CFD) code, FLUENT is used to investigate the exact lubrication characteristics of infinitely long slider bearing with micro-pockets. The results show that the pressure distributions are highly affected by pocket depths, its positions and numbers. The numerical method adopted in this paper and results can be use in optimal design of textured sliding bearings.

CFD를 이용한 Window Defrosting 평가 (The evaluative study of window defrost using Computational Fluid Dynamics)

  • 이인수;임효남;최재웅
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.179-182
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    • 2011
  • The purpose of this study is to evaluate a defrost model for the possibility of defrosting on wheelhouse window and the heat capacity if defrosting nozzle by using the commercial CFD solver FLUENT. A detailed simulation model has been created which contains the defrosting nozzle, window and the interior/exterior forced convection boundary. In this numerical study, the heat and mass transfer coupled during defrosting and investigated the defrost time for different hot gas temperature, external wind speed and temperature condition.

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