• 제목/요약/키워드: 3D-CFD

검색결과 673건 처리시간 0.029초

열차폐 코팅 두께를 고려한 핀틀의 열전달 해석 (Analysis of Heat Transfer considering thickness of Thermal Barrier Coating)

  • 장한나;이지훈;곽재수;조진연;김재훈;고준복;허준영
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.392-394
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    • 2017
  • 본 연구에서는 가변 추력기 3D 모델에 대해 CFD를 이용하여 고온 고압 환경에서의 추력 조절기 표면 열전달 계수를 예측하였다. 추력 조절기 표면에 열차폐코팅(TBC)을 모델링하였고, TBC 코팅의 두께가 추력조절기 내부 온도 분포에 미치는 영향을 연구하였다. TBC층의 두께는 $100{\mu}m{\sim}500{\mu}m$로 변화시켰다. 해석 결과, TBC층의 두께가 증가함에 따라 추력 조절기 표면과 내부 온도는 감소하는 경향을 보였다.

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챔버 내측에 스프링형상을 갖는 유수형 자외선 살균장치 시뮬레이션 (Simulation for the Flowing Water Purification with Spring Shape Inside Chamber)

  • 정병균;정병호;이진종;정병수
    • 전기학회논문지P
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    • 제59권4호
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    • pp.411-416
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    • 2010
  • Interest in application of ultraviolet light technology for primary disinfection of potable water in drinking water treatment plants has increased significantly in recent years. The efficacy of disinfection processes in water purification systems is governed by several key factors, including reactor hydraulics, disinfectant chemistry, and microbial inactivation kinetics. The objective of this work was to develop a computational fluid dynamics(CFD) model to predict velocity fields, mass transport, chlorine decay, and microbial inactivation in a continuous flow reactor. In this paper, It describe the how to design optimal UV disinfection device for ground water, BWT and rainwater. Spring shape instrument silver coated located in inner side of disinfection chamber. It make lead the active flowing movement target water and maximize disinfection performance. To search the optimal design method, it was performed computer simulation with 3D-CFD discrete ordinates model and manufactured prototype. Using proposed design method, performed simulation and proved satisfied performance.

CFD에 의한 2D 에어포일 공력특성 및 3D 풍력터빈 성능예측 (Predicting the Aerodynamic Characteristics of 2D Airfoil and the Performance of 3D Wind Turbine using a CFD Code)

  • 김범석;김만응;이영호
    • 대한기계학회논문집B
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    • 제32권7호
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    • pp.549-557
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    • 2008
  • Despite of the laminar-turbulent transition region co-exist with fully turbulence region around the leading edge of an airfoil, still lots of researchers apply to fully turbulence models to predict aerodynamic characteristics. It is well known that fully turbulent model such as standard k-model couldn't predict the complex stall and the separation behavior on an airfoil accurately, it usually leads to over prediction of the aerodynamic characteristics such as lift and drag forces. So, we apply correlation based transition model to predict aerodynamic performance of the NREL (National Renewable Energy Laboratory) Phase IV wind turbine. And also, compare the computed results from transition model with experimental measurement and fully turbulence results. Results are presented for a range of wind speed, for a NREL Phase IV wind turbine rotor. Low speed shaft torque, power, root bending moment, aerodynamic coefficients of 2D airfoil and several flow field figures results included in this study. As a result, the low speed shaft torque predicted by transitional turbulence model is very good agree with the experimental measurement in whole operating conditions but fully turbulent model(${\kappa}-\;{\varepsilon}$) over predict the shaft torque after 7m/s. Root bending moment is also good agreement between the prediction and experiments for most of the operating conditions, especially with the transition model.

CHAINED COMPUTATIONS USING AN UNSTEADY 3D APPROACH FOR THE DETERMINATION OF THERMAL FATIGUE IN A T-JUNCTION OF A PWR NUCLEAR PLANT

  • Pasutto, Thomas;PENiguel, Christophe;Sakiz, Marc
    • Nuclear Engineering and Technology
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    • 제38권2호
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    • pp.147-154
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    • 2006
  • Thermal fatigue of the coolant circuits of PWR plants is a major issue for nuclear safety. The problem is especially accute in mixing zones, like T-junctions, where large differences in water temperature between the two inlets and high levels of turbulence can lead to large temperature fluctuations at the wall. Until recently, studies on the matter had been tackled at EDF using steady methods: the fluid flow was solved with a CFD code using an averaged turbulence model, which led to the knowledge of the mean temperature and temperature variance at each point of the wall. But, being based on averaged quantities, this method could not reproduce the unsteady and 3D effects of the problem, like phase lag in temperature oscillations between two points, which can generate important stresses. Benefiting from advances in computer power and turbulence modelling, a new methodology is now applied, that allows to take these effects into account. The CFD tool Code_Saturne, developped at EDF, is used to solve the fluid flow using an unsteady L.E.S. approach. It is coupled with the thermal code Syrthes, which propagates the temperature fluctuations into the wall thickness. The instantaneous temperature field inside the wall can then be extracted and used for structure mechanics computations (mainly with EDF thermomechanics tool Code_Aster). The purpose of this paper is to present the application of this methodology to the simulation of a straight T-junction mock-up, similar to the Residual Heat Remover (RHR) junction found in N4 type PWR nuclear plants, and designed to study thermal striping and cracks propagation. The results are generally in good agreement with the measurements; yet, in certain areas of the flow, progress is still needed in L.E.S. modelling and in the treatment of instantaneous heat transfer at the wall.

카나드 기반의 지능탄 조종 장치 공력설계 (Aerodynamic Design of a Canard Controlled 2D Course Correction Fuze for Smart Munition)

  • 박지환;배주현;송민섭;명노신;조태환
    • 한국항공우주학회지
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    • 제43권3호
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    • pp.187-194
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    • 2015
  • 탄도수정탄은 기존 포탄의 신관에 카나드가 장착된 조종 장치를 탑재하여 정확도를 향상시키는 지능탄이다. 본 논문에서는 2D 탄도수정탄의 카나드를 설계하기 위하여 다양한 형상 변수에 대한 공력성능을 반실험적 기법을 이용하여 분석하였으며, 이를 바탕으로 초음속에서 항력이 상대적으로 더 적은 카나드 형상을 설계하였다. 또한 CFD 기법을 통한 탄도수정탄의 공력해석 기법을 연구하였으며, 포탄의 탄저 부분 기저항력 예측에 O-type 격자를 바탕으로 한 k-${\omega}$ SST 난류모델이 적합함을 확인하였다. 최종적으로 앞서 개발한 해석 기법을 바탕으로 2D 탄도수정탄의 공력특성 및 탄도조종장치 장착에 따른 항력변화를 계산하였다.

렌지후드의 성능개선을 위한 시로코 펜 주위의 유동해석 (PERFORMANCE IMPROVEMENT OF A RANGE HOOD SIROCCO FAN BY CFD FLOW ANALYSIS)

  • 한병윤;박진우;이명수;박형구
    • 한국전산유체공학회지
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    • 제13권4호
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    • pp.72-79
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    • 2008
  • This study is to investigate the air flow around a sirocco fan which is used in a range hood. The main object of the study is to improve the flow rate of the fan by analysis of unsteady 3-dimensional incompressible flow. Overall analysis is carried out using CFD method. For this, we used a commercial code, SC/Tetra, and used a sliding mesh method to give the same condition as an actual state. First, verification of the CFD results is done by comparing the experimental data with the numerical data for the suction flow rate. It is confirmed that two results are well consistent. Then for the improvent of flow rate, the effect of shape factors such as diameter ratio of fan, geometry of case, cut-off aperture and guide angle of case exit on the suction flow rate was considered. Especially, for a new design of housing, the principle of Archimedes spiral was used. The overall analysis was applied to a new design of housing, and the result showed an increase of flow rate by 10.7%.

노천광산의 발파분진 비산영역 예측에 관한 연구 (Study on Simulation of Dust Diffusion at Open Pit Mines)

  • 김복윤;이상권;조영도;김임호
    • 터널과지하공간
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    • 제8권3호
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    • pp.194-199
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    • 1998
  • 본 연구는 석회석 노천채광장의 발파 분진이 주변을 통과하는 특고압 선로에 어느정도 비산 퇴적할 것인지, 어떤 문제를 일으킬 것인지를 평가하기 위한 연구였다. 발파 현장이 분진 발생량 및 입도분포는 그간의 연구 실적도 있고 계측도 가능하지만 얼마만큼의 분진이 어느 정도 거리까지 비산 퇴적할 것인지를 예측하기란 매우 어려운 일이다. 따라서 본 연구에서는 최근 개발한 바 있는 수치유체역학(CFD)을 이용한 3차원 유체거동 해석 프로그램(3D-Flow)을 이용하여 송전선로에 미치는 영향을 예측하는 시도를 하였다. 지형조건, 기상조건에 따른 시뮬레이션을 통하여 석회석 분진은 송전선로에 큰 영향을 미치지 않을 것으로 판단 되었다.

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흡기밸브 형상에 따른 3차원 유동특성 해석 (Three-dimensional Analysis of Flow Characteristics for Intake Valve Design)

  • 김득상;이상진;조용석;엄인용
    • 한국자동차공학회논문집
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    • 제11권4호
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    • pp.1-6
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    • 2003
  • Steady flow bench test is a practical, powerful and widely used in most engine manufacturers to give a design concept of a new engine. In order to use steady data as a performance index, it is necessary to build some database, which can correlate the port characteristics with engine data. However, it is very difficult to investigate all port shapes with experimental tools. The steady flow scheme is relatively simple and its results are bulk ones such as flow rate and momentum of flow. Therefore a CFD code can be easily applied to the port evaluation. In this study, the steady flow test was simulated through three-dimensional analysis on intake port design for comparing with experimental data and confirming the feasibility of applying analytic method . for this purpose, the effect of valve curvature on flow rate was estimated by a CFD code. Numerical results were compared with those of real steady flow tests. As a result, the results of 3-D analysis were almost consistent with experimental data.

인덕션 쿡탑 기구물 형상변경이 Heatsink 및 Coil 냉각성능에 미치는 영향에 대한 연구 (Study on the Cooling Performance of Heatsink for Induction Cooktop using Computational Fluid Dynamics)

  • 박동호;권명근;이동범;서응렬;박용종
    • 한국유체기계학회 논문집
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    • 제18권3호
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    • pp.33-37
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    • 2015
  • A numerical study on the IPM/Bridge Diode cooling and coil cooling has been performed. Results are presented as plots of thermal resistance, temperature drop and RPM-ratio. CFD analysis for conventional cooling system has been performed as a reference case. As the RPM-Ratio was increased, heatsink thermal resistance and coil temperature were decreased. IPM/Bridge Diode thermal resistance and temperature of the coil is tended to be trade-off. The temperature of coil closest to the AC-motor fan showed the most significant change in accordance with duct design. The temperature of coil located at the top of DC-motor fan showed the most significant variation as the cooling air passes the heatsink fin area.

기계공학교육과정에서의 전산유체동역학의 기초예제개발 (I) (수평 원관의 층류 유동) (Development of Simple Example of CFD Course in Mechanical Engineering Curriculum (I) (Laminar Pipe Flow))

  • 이성룡;조석수
    • 한국산학기술학회논문지
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    • 제19권7호
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    • pp.72-80
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    • 2018
  • 과학 및 공학 분야 등에서 유한체적법등과 같은 전산해석방법은 비약적으로 발전하여 주로 대학 연구실 및 기업 등에서 활용하고 있었으나 최근에는 대학의 교육과정에서도 전산해석방법이 도입되고 있다. 이것을 계기로 공학대학의 기계공학과등에서 전산유체동역학이 학부 3학년 또는 4학년에 개설되고 있다. 일반적으로 전산유체동역학에서 다루는 수치해석 예제는 상용 전산유체동역학 소프트웨어 회사에서 개발한 예제이다. 따라서 학부 학생들은 저학년에서 학습한 유체역학의 이론적 해와 전산유체동역학 강의에서 학습하는 수치해석 해를 서로 비교할 수 없는 상황이 되고 있다. 따라서 본 연구에서는 유체동역학의 고전적인 해석 대상인인 정상 상태의 수평 원관 층류 유동의 이론적 배경을 설명한 뒤 ANSYS FLUENT를 이용하여 정상 상태의 수평 원관 층류 유동에 대한 수치해석 해를 구하여 이론적 해와 수치해석 해를 서로 비교하여 학생들의 전산유체동역학에 대한 개념을 확실히 다짐으로서 학생들의 현장적응능력을 높였으며 해당 강좌에 대한 강의 평가 결과 학생들이 전산유체동역학에 대한 이해력과 tutorial에 대한 만족도가 매우 높았다.