• 제목/요약/키워드: Reynolds-averaged Navier-Stokes Equation

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여울-소 구조에서 지표수-지하수 혼합대의 흐름 특성 분석에 관한 수치모의 연구 (Numerical Modeling of Flow Characteristics within the Hyporheic Zones in a Pool-riffle Sequences)

  • 이두한;김영주;이삼희
    • 한국습지학회지
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    • 제14권1호
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    • pp.75-87
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    • 2012
  • 지표수-지하수 혼합대는 하천 및 호소 등에서 지표수와 지하수가 교환되는 공간이다. 지표수-지하수 혼합은 하상의 토층으로 확장되어 다양한 물리적, 생지화화적, 열역학적 교환을 발생시키며 수생태계 내 고유한 생태적 전이대를 형성하는데 주요한 역할을 한다. 과거 실험 및 수치모의 연구에 의하면 혼합대에서 발생하는 물질교환은 하천의 지형적인 특징으로 발생하는 압력분포에 의해 지배된다. 특히 하천의 구간 규모에서 여울-소 구조는 혼합대의 특성을 지배하는 주요 인자로 알려져 있다. 여울-소 연속 구조는 지표수에서 재순환영역과 정체점을 형성하며 이 독특한 흐름 구조에 의해 혼합대의 흐름특성이 영향을 받는다. 본 연구에서는 3차원 동수역학 모형을 이용하여 Reynolds-averaged Navier-Stokes 방정식과 Darcy 방정식을 동시에 해석하여 연속된 여울-소 구조에서 발생하는 지표수의 흐름구조가 혼합대의 흐름에 미치는 영향을 분석하였다. 모의 결과, 여울-소 구조에서 지표수의 재순환영역 및 정체점은 상승류와 하강류 형성과 직접적 연관을 가지며, 재순환영역의 크기가 감소하면 여울 전면부 하강류 형성 구간의 길이가 감소하고 최대 하강류 발생 지점이 하부로 이동하는 특성을 파악하였다. 이와 같은 본 연구의 결과는 혼합대의 현장관측, 하천 관리 및 복원 등의 연구에 활용하여 친환경 하천 조성에 기여할 수 있을 것으로 판단된다.

임펠라 스플리터 날개 최적 설계를 통한 무선진공청소기 팬 모터 단품의 공력 소음 저감 (Aerodynamic noise reduction of fan motor unit of cordless vacuum cleaner by optimal designing of splitter blades for impeller)

  • 김건우;유서윤;정철웅;서성진;장철민;설한신
    • 한국음향학회지
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    • 제39권6호
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    • pp.524-532
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    • 2020
  • 본 논문에서는 무선진공청소기용 팬 모터 단품으로부터 방사되는 공력소음을 저감하기 위하여 팬 모터 단품 내부의 기존 임펠라에 스플리터 날개를 설계하였다. 우선, 팬 모터 단품, 특히 임펠라의 유동장을 분석하기 위하여 전산유체역학 기법을 사용하여 비정상, 비압축성 Reynolds-Averaged Navier-Stokes(RANS) 방정식을 수치적으로 해석하였다. 예측한 유동장 결과를 입력값으로 Ffowcs Williams-Hawkings(FW-H) 적분 방정식을 풀어 임펠라로부터 방사되는 소음을 수치적으로 예측하였다. 예측한 음압스펙트럼과 측정값의 비교를 통하여 수치해석방법의 유효성을 검증하였다. 예측한 유동장 결과에 대한 추가 분석을 통하여 임펠라 날개 사이에서 강한 와류가 형성되는 것을 확인하였다. 와류는 유동에는 손실로 소음에는 소음원으로 작용하기 때문에 기존 임펠라에 스플리터 형상을 추가 설계하여 와류를 억제하고자 하였다. 스플리터의 길이와 위치를 설계 인자로 선정하였으며, 다구찌 기법을 사용하여 각각의 설계 인자가 공력소음에 미치는 영향도를 살펴보았다. 이 결과로부터 최소소음을 나타내는 스플리터의 최적 위치와 길이를 결정하였다. 최종 선정된 설계안에 대한 추가 해석을 통하여 소음성능이 개선됨을 확인 하였다.

무선진공청소기 팬 모터 단품의 유량성능 향상과 공력소음 저감을 위한 임펠라 최적설계 (Optimal design of impeller in fan motor unit of cordless vacuum cleaner for improving flow performance and reducing aerodynamic noise)

  • 김건우;유서윤;정철웅;서성진;장철민
    • 한국음향학회지
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    • 제39권5호
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    • pp.379-389
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    • 2020
  • 본 논문에서는 무선진공청소기용 팬 모터 단품의 유량 및 소음성능을 향상시키기 위하여 무선청소기 유로를 통하여 공기를 흡입하는 임펠라에 대한 최적설계를 수행하였다. 우선, 팬 모터 단품, 특히 임펠라의 유동장을 분석하기 위하여 비정상, 비압축성 Reynolds averaged Navier-Stokes(RANS) 방정식을 전산유체역학(Computational Fluid Dynamics, CFD)에 기초하여 해석하였다. 예측한 유동장 정보를 입력값으로 Ffowcs-Williams and Hawkings(FW-H) 방정식을 사용하여 임펠라로부터 방사되는 소음을 수치적으로 예측하였다. 유량과 소음에 대한 수치해석 결과를 실험을 통해 측정한 팬 모터 단품의 P-Q 곡선과 음압 스펙트럼과 비교하여 사용한 수치방법의 유효성을 확인하였다. 수치해석결과로부터 임펠라 날개의 코드방향 중간부분의 급격한 곡률 변화로 인하여 강한 와류가 형성되는 것을 확인하였다. 와류는 유동에는 손실로 소음에는 소음원으로 작용하기 때문에 기존의 임펠라를 재설계하여 와류를 개선하고자 하였다. 2인자 반응표면방법을 사용하여 최대유량과 최소소음을 나타내는 입·출구 뒷젖힘각(sweep angle)을 결정하였다. 최종 선정된 설계안에 대한 추가 해석을 통하여 유량성능과 소음성능이 개선됨을 확인하였다.

유출홀이 설치된 정사각유로 내 열전달 향상을 위한 경사진 요철 최적설계 (Optimization of Angled Ribs for Heat Transfer Enhancement in Square Channel with Bleed Flow)

  • 이현;김경민;이동현;조형희
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2384-2389
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    • 2007
  • The 2nd order response surface method (RSM) has been carried out to get optimum thermal design for enhanced heat transfer on square channel with bleed holes. The RSM was used as an optimization technique with Reynolds-averaged navier-stokes equation. Turbulence model for heat transfer analysis used RNG k-epsilon model. The wall function used enhanced wall function. Numerical local heat transfer coefficients were similar to the experimental tendency. Two design variables such as attack angle of rib (${\alpha}$), rib pitch-to-rib height ratio (p/e) were chosen. Operation condition considered bleeding ratio per bleed hole ($BR_{hole}$). A response surface were constructed by the design variables and operation condition. As a result, adjusted $R^2$ was more than 0.9. Optimization results of various objective function were similar to heat transfer in channel with and without bleed flow. But friction factor was lower than channel without bleed flow.

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NUMERICAL MODELLING OF SHEET-FLOW TRANSPORT UNDER WAVE AND CURRENT

  • Bakhtiary, Abbas-Yeganeh;Hotoshi Gotoh;Tetsuo Sakai
    • Water Engineering Research
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    • 제3권2호
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    • pp.75-84
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    • 2002
  • An Euler-Lagrange two-phase flow model is presented fur simulation sheet-flow transport under wave and current. The flow is computed by solving the Reynolds Averaged Navier-Stokes equation in conjunction with the k-$\varepsilon$ turbulence model for turbulence closure. The sediment transport is introduced as a motion of granular media under the action of unsteady flow from the Lagragian point of view. In other word, motion of every single particle is numerically traced with Movable Bed Simulator (MBS) code based on the Distinct Element Method (DEM), in which the frequent interparticle collision of the moving particles during the sheet-flow transport is sophisticatedly taken into account. The particle diameter effect on time-dependent developing process of sheet-flow transport is investigated, by using three different diameter sizes of sediment. The influence of an imposed current on oscillatory sheet-flow transport is also investigated. It is concluded that the sediment transport rate increases due to the relaxation process related to the time-lag between flow velocity and sediment motion.

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CFD를 이용한 덕트 프로펠러 단독 상태에서의 추진 성능 예측 (PROPULSIVE PERFORMANCE PREDICTION OF A DUCTED PROPELLER IN OPEN WATER CONDITION USING CFD)

  • 이경언;진두화;이상욱
    • 한국전산유체공학회지
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    • 제20권2호
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    • pp.1-6
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    • 2015
  • In this study, a numerical prediction on propulsive performance of a ducted propeller in open water condition was carried out by solving Reynolds averaged Navier-Stokes(RANS) equation using computational fluid dynamics(CFD). A configuration of propeller Ka-470 inside duct 19A was considered. Hexahedral grid system was generated by dividing whole computational domain into three separate regions; propeller, duct and outer flow region. A commercial CFD software, ANSYS-CFX was used for numerical simulations. Results were compared with experimental data and showed considerable improvement in accuracy, in comparison to those from surface panel method which is based on potential flow assumption. The results also exhibited the importance of grid system within the gap between the inner surface of duct and blade tip for accurate prediction of propulsive performance of ducted propeller.

수중익형 주변 유동장에서의 공동현상과 유동소음에 대한 수치적 연구 (Numerical Investigation of Cavitation Flow Around Hydrofoil and Its Flow Noise)

  • 김상현;정철웅;박원규;설한신
    • 한국소음진동공학회논문집
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    • 제26권2호
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    • pp.141-147
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    • 2016
  • Underwater cavitation is one of the most important issues because it causes not only vibration and erosion of submerged bodies but also significant flow noise problems. In this paper, flow noise due to cavitation flows around the NACA66 MOD hydrofoil is numerically investigated. The cavitation flow simulation is conducted using the Reynolds-Averaged Navier-Stokes equations based on finite difference methods. To capture the cavitation phenomena accurately and effectively, the homogeneous mixture model with the Merkle's cavitation model is applied. The predicted results are compared with available experimental data in terms of pressure coefficients and volume fraction, which confirms the validity of numerical results. Based on flow field analysis results, hydro-acoustic noise field due to the cavitation flow is predicted using the Ffowcs-Williams and Hawkings equation derived from the Lighthill's acoustic analogy. The typical lift dipole propagation patterns are identified.

Ahmed Body 주위의 3차원 난류유동 해석 - 난류모델의 평가 (Simulation of Three-Dimensional Turbulent Flows around an Ahmed Body-Evaluation of Turbulence Models-)

  • 명현국;진은주;박희경
    • 대한기계학회논문집B
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    • 제21권7호
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    • pp.873-881
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    • 1997
  • A numerical simulation has been carried out for three-dimensional turbulent flows around an Ahmed body. The Reynolds-averaged Navier-Stokes equation is solved with the SIMPLE method in general curvilinear coordinates system. Several k-.epsilon. turbulence models with two convective difference schemes are evaluated for the performance such as drag coefficient, velocity and pressure fields. The drag coefficient, the velocity and pressure fields are found to be changed considerably with the adopted k-.epsilon. turbulence models as well as the finite difference schemes. The results of simulation prove that the RNG k-.epsilon. model with the QUICK scheme predicts fairly well the tendency of velocity and pressure fields and gives more reliable drag coefficient. It is also demonstrated that the large difference between simulations and experiment in the drag coefficient is due to relatively high predicted values of pressure drag from vertical rear end base.

3D Casing-Distributor Analysis for Hydraulic Design Application

  • Devals, Christophe;Zhang, Ying;Dompierre, Julien;Vu, Thi C.;Mangani, Luca;Guibault, Francois
    • International Journal of Fluid Machinery and Systems
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    • 제8권3호
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    • pp.142-154
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    • 2015
  • Nowadays, computational fluid dynamics is commonly used by design engineers to evaluate and compare losses in hydraulic components as it is less expensive and less time consuming than model tests. For that purpose, an automatic tool for casing and distributor analysis will be presented in this paper. An in-house mesh generator and a Reynolds Averaged Navier-Stokes equation solver using the standard $k-{\omega}$ shear stress transport (SST) turbulence model will be used to perform all computations. Two solvers based on the C++ OpenFOAM library will be used and compared to a commercial solver. The performance of the new fully coupled block solver developed by the University of Lucerne and Andritz will be compared to the standard 1.6ext segregated simpleFoam solver and to a commercial solver. In this study, relative comparisons of different geometries of casing and distributor will be performed. The present study is thus aimed at validating the block solver and the tool chain and providing design engineers with a faster and more reliable analysis tool that can be integrated into their design process.

Hybrid mesh 및 sliding mesh를 이용한 선박 저항추진 성능 시험 (SHIP RESISTANCE AND PROPULSION PERFORMANCE TEST USING HYBRID MESH AND SLIDING MESH)

  • 이주현;박범진;이신형
    • 한국전산유체공학회지
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    • 제15권1호
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    • pp.81-87
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    • 2010
  • In this study, we conducted resistance and propulsion performance test of ship composed of the Resistance Test, Propeller Open Water Test and Self Propulsion Test using the CFD(Computational Fluid Dynamics). We used commercial RANS(Reynolds Averaged Navier Stokes equation) solver, as a calculating tool. The unstructured grids were used in a bow and stern of ship, having complex shape, for a convenience of generating grids, and the structured grids were adopted in a central hull and rest of hull having a relatively simple shape which is called hybrid grid method. In addition, The sliding mesh method was adopted to rotate a propeller directly in the Propeller Open Water and Self Propulsion Test. The Resistance Test and Self Propulsion Test were calculated using Volume of Fluid (VOF) model and considering a free surface. And all The three cases were applied realizable k-epsilon model as the turbulence model. The results of calculations were verified for the suitability of calculations by comparing MOERI's EFD results.