• 제목/요약/키워드: and CFD

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다중현상 유동 해석 및 설계를 위한 융복합 프레임웍 개발 (DEVELOPMENT OF A HYBRID CFD FRAMEDWORK FOR MULTI-PHENOMENA FLOW ANALYSIS AND DESIGN)

  • 허남건
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2010년 춘계학술대회논문집
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    • pp.517-523
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    • 2010
  • Recently, the rapid evolution of computational fluid dynamics (CFD) has enabled its key role in industries and predictive sciences. From diverse research disciplines, however, are there strong needs for integrated analytical tools for multi-phenomena beyond simple flow simulation. Based on the concurrent simulation of multi-dynamics, multi-phenomena beyond simple flow simulation. Based on the concurrent simulation of multi-dynamics, multi-physics and multi-scale phenomena, the multi-phenomena CFD technology enables us to perform the flow simulation for integrated and complex systems. From the multi-phenomena CFD analysis, the high-precision analytical and predictive capacity can enhance the fast development of industrial technologies. It is also expected to further enhance the applicability of the simulation technique to medical and bio technology, new and renewable energy, nanotechnology, and scientific computing, among others.

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반실험적 기법 및 CFD 코드를 이용한 자유회전 테일핀을 갖는 커나드 조종 미사일에 관한 공력해석 (Aerodynamic Characteristics of a Canard-Controlled Missile with Freely Spinning Tailfins Using a Semi-Empirical Method and a CFD Code)

  • 양영록;이진희;김문석;정재홍;명노신;조태환
    • 한국항공우주학회지
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    • 제36권3호
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    • pp.220-228
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    • 2008
  • 반실험적 기법과 CFD 코드를 이용하여 자유회전 테일핀을 갖는 커나드 조종 미사일의 공력특성을 연구하였다. 반실험적 기법에서는 테일핀의 회전각에 따른 공력계수의 평균을 구한 후 자유회전 테일핀의 공력계수를 계산하였다. 또한 테일핀의 평균 롤링 및 롤 댐핑 모멘트계수를 이용하여 자유회전 테일핀의 회전율을 예측하였다. CFD 계산의 경우 중첩격자를 이용한 6-자유도 해석을 통해 테일핀의 회전율을 계산하였다. 미사일의 공력계수 예측 값들은 풍동실험 결과와 유사하게 나타났고, 커나드 롤 조종 및 요 조종시의 테일핀 회전율 또한 풍동실험결과와 근접하게 나타났다. 본 연구를 통해 자유회전 테일핀을 갖는 커나드 조종 미사일에 관한 공력해석에 반실험적 기법을 적용할 수 있음을 확인하였다.

HSM의 썬루프 버페팅 수치해석 (Numerical Investigation of Sunroof Buffeting for Hyundai Simplified Model)

  • 컹기 아쇽;이명훈
    • 한국소음진동공학회논문집
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    • 제24권3호
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    • pp.180-188
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    • 2014
  • 현대자동차그룹은 HSM이라고 불리는 간략화된 차량 모델에 대하여 썬루프 버페팅 현상의 실험적인 조사를 시행하였다. 현대자동차그룹은 어떤 CFD솔버가 충분한 정확도를 가지고 썬루프 버페팅 현상을 예측하는지 조사하기 위해 상용CFD공급업체의 참여를 요청하였다. ANSYS Korea는 이번 조사에 참여하여 ANSYS fluent를 이용하여 HSM의 썬루프 버페팅에 대한 수치해석을 수행하였다. 먼저 유동장 검증을 위해 풍속 60 km/h에 대하여 썬루프가 닫힌 HSM모델에 대하여 해석을 수행하였다. HSM상부 면의 세 지점에서 속도 분포를 예측하였고, 이는 시험결과와 비교되었다. 그런 다음 고해상도 난류 모델인 DES를 이용한 해석이 전 풍속영역에 걸쳐 수행되었다. 버페팅 주파수와 버페팅 음압레벨이 예측되었고, 이는 시험결과와 비교되었다. 이를 통해 실제 차량 개발을 위한 CFD의 예측 가능성에 대하여 결론을 얻을 수 있었다.

폐기물 층 연소와 노내 유동 해석 (Combined Bed Combustion and Gas Flow Simulation for a Grate Type Incinerator)

  • 류창국;신동훈;최상민
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2000년도 제20회 KOSCO SYMPOSIUM 논문집
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    • pp.67-75
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    • 2000
  • Computational fluid dynamics(CFD) analysis of the thermal flow in a municipal solid waste(MSW) incinerator combustion chamber provides crucial insight on the incinerator performance. However, the combustion of the waste bed is typically treated as an arbitrarily selected profile of combustion gas. A strategy for simultaneous simulation of the waste bed combustion and the thermal flow fields in the furnace chamber was introduced to substitute the simple inlet condition. A waste bed combustion model was constructed to predict the progress of combustion in the bed and corresponding generation of the gas phase species, which assumes the moving bed as a packed bed of homogeneous fuel particles. When coupled with CFD, it provides boundary conditions such as gas temperature and species distribution over the grate, and receives radiative heat flux from CFD. The combined simulation successfully predicted the physical processes of the waste bed combustion and its interaction with the flow fields for various design and operating parameters, which was limited in the previous CFD simulations.

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CFD를 이용한 자동차 사이드 미러의 공력특성 연구 (A Study of Aerodynamic Characteristics of a Car's Side-view Mirror using CFD)

  • 민선식;한준규;권기현;최은동;김문상
    • 항공우주시스템공학회지
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    • 제2권2호
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    • pp.46-50
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    • 2008
  • Aerodynamic characteristics, such as drag and lift, play an important role in automobile design under certain speed conditions. Such characteristics are essential to design an automobile since they are directly related to automobile's performance such as passenger safety and fuel consumption. There is a huge demand for the automobile to have safe performance at high speed. Reduction in drag is also important and it could lead to the solution of air flow induced noise and dust problems. The objective of this research is to find out the aerodynamic differences between conventional side mirror and a modified one using CFD. Although drag generated around a side mirror is only about 7% of the total drag when a car runs, it is very closely related to driver's field of vision and noise generation. CFD simulation of the flowfield around a car side-view mirror was performed using a commercial code; Gambit and FLUENT.

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선미 스케그 주위의 유동 분석에 의한 선미 형상 설계 (The Stern Hull Form Design using the Flow Analysis around Stern Skeg)

  • 박동우
    • 대한조선학회논문집
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    • 제45권4호
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    • pp.361-369
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    • 2008
  • The optimized distance between skegs and angle of the skeg for a standard twin-skeg type LNG carrier were presented using the CFD and model tests. The evaluation method of self-propulsion performance was derived based on the results of CFD and confirmed the validity through model tests. The analyses to assess self-propulsion performance using CFD were shown by flow line patterns on the skeg surface, nominal wake distribution in the propeller plane and the evaluation for flow balance around stern skegs. The optimized ship that was applied to the optimized two design parameters in stern skeg arrangement for target ship was derived in this work. Finally speed performance of mother ship which is existing ship and optimized ship were compared through CFD and model tests. And the usefulness about the evaluation method of self-propulsion performance was reconfirmed.

OpenFOAM : Open source CFD in research and industry

  • Jasak, Hrvoje
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제1권2호
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    • pp.89-94
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    • 2009
  • The current focus of development in industrial Computational Fluid Dynamics (CFD) is integration of CFD into Computer-Aided product development, geometrical optimisation, robust design and similar. On the other hand, in CFD research aims to extend the boundaries of practical engineering use in "non-traditional" areas. Requirements of computational flexibility and code integration are contradictory: a change of coding paradigm, with object orientation, library components, equation mimicking is proposed as a way forward. This paper describes OpenFOAM, a C++ object oriented library for Computational Continuum Mechanics (CCM) developed by the author. Efficient and flexible implementation of complex physical models is achieved by mimicking the form of partial differential equation in software, with code functionality provided in library form. Open Source deployment and development model allows the user to achieve desired versatility in physical modeling without the sacrifice of complex geometry support and execution efficiency.

CFD모사를 이용한 저수지 물순환장치 유동 설계 (Design of convection current circulation system in reservoir using CFD simulation)

  • 이요상
    • 환경영향평가
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    • 제21권1호
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    • pp.133-142
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    • 2012
  • Convection Current Circulation System(CCCS) in stratified reservoir controls development of anaerobic condition and algal bloom during summer. In order to increase the CCCS effectiveness, we analyze diverse design parameters to make optimize the flow pattern in reservoir. In this study, we interpret the internal flow with installation and operation condition of CCCS based on CFD in reservoir. Design variables of CCCS is reservoir depth, stratification strength, distance of between CCCS and so on. Since reservoir depth and stratification strength in variables is depending on natural phenomenon, we evaluated current circulation effect by distance of CCCS and proposed the optimal design condition using CFD simulation. Flow and diffusion changes in water body was assessed by temperature and dye test. Changes in water floor temperature at 40m intervals was slowly descending over 37 hours. Dye diffusion simulation at 60m intervals, the radius of the spread between two devices were overlapped after 12 hours.

CFD-FEA ANALYSIS OF HYDRAULIC SHOCK ABSORBER VALVE BEHAVIOR

  • Shams, M.;Ebrahimi, R.;Raoufi, A.;Jafari, B.J.
    • International Journal of Automotive Technology
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    • 제8권5호
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    • pp.615-622
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    • 2007
  • In this study, a Coupled Computational Fluid Dynamics(CFD) and Finite Element Analysis(FEA) method are used to predict and evaluate the performance of an automotive shock absorber. Averaged Navier-Stokes equations are solved by the SIMPLE method and the RNG $k-\varepsilon$ is used to model turbulence. CFD analysis is carried out for different intake valve deflections and piston velocities. The force exerted on the valve in each valve deflection is obtained. The valve deflection-force relationship is investigated by the FEA method. The force exerted on the valve in each piston velocity is obtained with a combination of CFD and FEA results. Numerical results are compared with the experimental data and have shown agreement. Dependence of valve deflection as a function of piston velocity is investigated. Effects of hydraulic oil temperature change on valve behavior are also studied.

CFD simulations of a performance-scaled wind turbine

  • Ye, Maokun;Chen, Hamn-Ching;Koop, Arjen
    • Ocean Systems Engineering
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    • 제12권2호
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    • pp.247-265
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    • 2022
  • In the present study, we focus on the CFD simulations for the performance and the rotor-generated wake of a model-scale wind turbine which was designed for wave tank experiments. The CFD simulations with fully resolved rotor geometry are performed using MARIN's community-based open-source CFD code ReFRESCO. The absolute formulation method (AFM) is leveraged to model the rotating wind turbine. The k - ω SST turbulence model is adopted in the incompressible Reynolds Averaged Navier-Stokes (RANS) simulations. First, the thrust and torque coefficients, CT and CP, are calculated at different Tip Speed Ratios (TSR), and the results are compared against the experimental data and previous numerical results. The pressure distribution of the turbine blades at the 70% span is obtained and compared to the results obtained by other tools. Then, a verification study aiming at quantifying the discretization uncertainty of the turbine performance with respect to the grid resolution in the wake region is performed. Last, the rotor-generated wake at the TSR of 7 is presented and discussed.