• 제목/요약/키워드: Navier-Stokes 유체

검색결과 935건 처리시간 0.032초

층류-난류 천이 모델을 적용한 프로펠러 단독 성능 해석에 관한 CFD 시뮬레이션 (CFD Simulation on Predicting POW Performance Adopting Laminar-Turbulent Transient Model)

  • 김동현;전규목;박종천;신명수
    • 대한조선학회논문집
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    • 제58권1호
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    • pp.1-9
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    • 2021
  • In the present study, the model-scale Propeller Open Water (POW) tests for the propeller of 176K bulk carrier and 8600TEU container ship were conducted through Computational Fluid Dynamics (CFD) simulation. In order to solve the incompressible viscous flow field, the Reynolds-averaged Navier-Stokes (RaNS) equations were employed as the governing equations. The γ-Reθ(gamma-Re-theta) transition model combined with the SST k-ωturbulence model was introduced to describe the laminar-turbulence transition considering the low Reynolds number of model-scale. Firstly, the flow simulation developing over a flat plate was performed to verify the transition modeling, in which the wall shear stresses were compared with experiments and other numerical results. Then, to investigate the effect of the model, the CFD simulation for the POW test was performed and the simulated propeller performance was validated through comparison with the experiment conducted at Korea Research Institute of Ships & Ocean Engineering (KRISO).

CFD를 이용한 KRISO 추진효율 향상 장치(K-duct) 형상 특성에 관한 연구 (A Study on the Shape of KRISO Propulsion Efficiency Improvement Devices(K-duct) using CFD)

  • 김진욱;서성부
    • 대한조선학회논문집
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    • 제55권6호
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    • pp.474-481
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    • 2018
  • This paper is to compare by numerical analysis the flow characteristics and propulsion performance of stern with the shape change of K-duct, a pre-swirl duct developed by Korea Research Institute of Ships & Ocean Engineering (KRISO). First, the characteristics of the propeller and the resistance and self-propulsion before and after the attachment of the K-duct to the ship were verified and the validity of the calculation method was confirmed by comparing this result with the model test results. After that, resistance and self-propulsion calculations were performed by the same numerical method when the K-duct was changed into five different shapes. The efficiency of the other five cases was compared using the delivery horsepower in the model scale and the flow characteristics of the stern were analyzed as the velocity and pressure distributions in the area between the duct end and the propeller plane. For the computation, STAR-CCM +, a general-purpose flow analysis program, was used and the Reynolds Averaged Navier-Stokes (RANS) equations were applied. Rigid Body Motion (RBM) method was used for the propeller rotating motion and SST $k-{\omega}$ turbulence model was applied for the turbulence model. As a result, the tangential velocity of the propeller inflow changed according to the position angle change of the stator, and the pressure of the propeller hub and the cap changes. This regulated the propeller hub vortex. It was confirmed that the vortex of the portion where the fixed blade and the duct meet was reduced by blunt change.

베어링의 열전도율이 평행 슬라이더 베어링의 윤활성능에 미치는 영향 (Effect of Thermal Conductivity of Bearing on the Lubrication Performance of Parallel Slider Bearing)

  • 박태조;이원석;박지빈
    • Tribology and Lubricants
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    • 제34권6호
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    • pp.247-253
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    • 2018
  • Temperature rise due to viscous shear of the lubricating oil generates hydrodynamic pressure, even if the lubricating surfaces are parallel. This effect, known as the thermal wedge effect, varies significantly with film-temperature boundary conditions. The bearing conducts a part of the heat generated; hence, the oil temperature varies with the thermal conductivity of the bearing. In this study, we analyze the effect of thermal conductivity on the thermohydrodynamic (THD) lubrication of parallel slider bearings. We numerically analyze the continuity equation, Navier-Stokes equation, energy equation including the temperature-viscosity and temperature-density relations for lubricants, and the heat conduction equation for bearing by creating a 2D model of the micro-bearing using the commercial computational fluid dynamics (CFD) code FLUENT. We then compare the variation in temperature, viscosity, and pressure distributions with the thermal conductivity. The results demonstrate that the thermal conductivity has a significant influence on THD lubrication characteristics of parallel slider bearings. The lower the thermal conductivity, the greater the pressure generation due to the thermal wedge effect resulting in a higher load-carrying capacity and smaller frictional force. The present results can function as the basic data for optimum bearing design; however, the applicability requires further studies on various operating conditions.

규칙파 중 사각형 부유식 구조물의 횡동요 운동특성에 대한 연구 (Study on Roll Motion Characteristics of a Rectangular Floating Structure in Regular Waves)

  • 김민규;정광효;박성부;이강남;박일룡;서성부
    • 한국해양공학회지
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    • 제33권2호
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    • pp.131-138
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    • 2019
  • This study focused on the roll motion characteristics of a two-dimensional (2D) rectangular floating structure under regular beam sea conditions. An experiment was conducted in a 2D wave tank for a roll free decay test in calm water and the roll motion in a range of regular waves with and without heave motion to investigate the motion response and heave influence on the roll motion. A numerical study was carried out using Reynolds-averaged Navier Stokes (RANS)-based CFD simulations. A grid convergence test was conducted to accurately capture the wave condition on the free surface based on the overset mesh and wave forcing method. It was found in the roll free decay test that the numerical results agreed well with the experimental results for the natural roll period and roll damping coefficient. It was also observed that the heave motion had an impact on the roll motion, and the responses of the heave and roll motion from the CFD simulations were in reasonable agreement with those from the experiment.

176k Bulk Carrier에 대한 신개념 타입의 Pre-Swirl Duct의 개발 및 CFD 해석 (Development and CFD Analysis of a New Type Pre-Swirl Duct for 176k Bulk Carrier)

  • 유광열;김문찬;신용진;신이록;김현웅
    • 대한조선학회논문집
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    • 제56권4호
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    • pp.373-382
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    • 2019
  • This paper shows numerical results for the estimation of the propulsor efficiency of Pre-Swirl Duct for 176k bulk carrier as well as its design method. Reynolds averaged Navier-Stokes equations have been solved and the k-epsilon model applied for the turbulent closure. The propeller rotating motion is determined using a sliding mesh technique. The design process is divided into each part of Pre-Swirl Duct, duct and Pre-Swirl Stator. The design of duct was performed first because it is located further upstream than Pre-Swirl Stator. The distribution of velocity through the duct was analyzed and applied for the design of Pre-Swirl Stator. The design variables of duct include duct angle, diameter, and chord length. Diameter, chord length, equivalent angle are considered when designing the Pre-Swirl Stator. Furthermore, a variable pitch angle stator is applied for the final model of Pre-Swirl Duct. The largest reduction rate of the delivered power in model scale is 7.6%. Streamlines, axial and tangential velocities under the condition that the Pre-Swirl Duct is installed were reviewed to verify its performance.

분사가스 온도에 따른 수중운동체 주위 초공동 특성 분석을 위한 수치해석 (Numerical Analysis for Supercavitation Characteristics around Underwater Vehicle according to Ventilated Gas Temperature)

  • 황현성;박원규;김동현;김동현
    • 한국군사과학기술학회지
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    • 제25권5호
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    • pp.487-500
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    • 2022
  • Supercavitation is a phenomenon in which the cavity covers the entire underwater vehicle. The purpose of this paper is to compare and analyze the thermal effect on the cavity characteristics by changing the ventilated gas temperature through computational analysis. For this study, a homogeneous mixture model based on the 3D Navier-Stokes equation was used. As a phase change model, it is its own code considering both pressure change and temperature change. A dimensionless number Tm was presented to analyze the numerical results, and as the Tm increased, the cavity length increased by about 3.6 times and the cavity width by about 3.3 times at 393.15 K compared to room temperature. Analyzing these thermal effects, it was confirmed that rapid heat exchange and heat transfer between the gas phase and the liquid phase occurred at the location where the ventilated gas was sprayed, affecting the cavity characteristics. In addition, it can be confirmed that the initial cavity surface becomes unstable as the ventilated gas temperature increases, and it can be confirmed based on the numerical analysis results that the critical temperature at which the cavity surface becomes unstable is 373.15 K.

사각형 그루브로 Surface Texturing한 평행 스러스트 베어링의 열유체윤활 해석: 제2보 - 그루브 깊이의 영향 (THD Lubrication Analysis of a Surface-Textured Parallel Thrust Bearing with Rectangular Grooves: Part 2 - Effect of Groove Depth)

  • 박태조;강정국
    • Tribology and Lubricants
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    • 제39권1호
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    • pp.21-27
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    • 2023
  • Surface texturing is widely applied to friction surfaces of various machine elements. Most of the theoretical studies have focused on isothermal (ISO) analyses which consider constant lubricant viscosity. However, there have been limited studies on the effect of oil temperature increase owing to viscous shear. Following the first part of the present study that investigated the effects of film-temperature boundary condition (FTBC) and groove number on the thermohydrodynamic (THD) lubrication characteristics of a surface-textured parallel thrust bearing with multiple rectangular grooves, this study focuses on the effect of groove depths. Current study numerically analyzes the continuity, Navier-Stokes, and energy equations with temperature-viscosity-density relations using a commercial computational fluid dynamics (CFD) software, FLUENT. The results of variation in temperature, velocity, and pressure distributions as well as load-carrying capacity (LCC) and friction force indicate that groove depth and FTBC significantly influence the temperature distribution and pressure generation. The LCC is maximum near the groove depth at which the vortex starts, smaller than the ISO result. For intense grooves, the LCC of THD may be larger than that from ISO. The frictional force decreases as the groove becomes deeper, and decreases more significantly in the case of THD. The study shows that groove depth significantly influences the THD lubrication characteristics of surface-textured parallel thrust bearings.

원형관의 흐름특성에 관한 실험적 및 수치모의 연구 (Experimental and numerical study on the flow characteristics of circular pipe)

  • 김병주;신홍준;백중철
    • 한국수자원학회:학술대회논문집
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    • 한국수자원학회 2023년도 학술발표회
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    • pp.294-294
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    • 2023
  • 보나 댐에 설치된 배수관이나 지하에 매설된 상하수도관과 같이 물을 운반하기 위한 관로 뿐만 아니라 유류를 운송하는 관, LPG와 같은 기체를 운송하는 관처럼 유체를 운송할 때 다양한 관로를 사용한다. 그 중 사용범위나 제작에 대한 용이성 등에 의해서 원형관이 주로 사용된다. 따라서 위와 같은 원형관 내의 관수로 흐름분포에 대한 연구는 아주 중요하며 필요하다. 원형관 내 흐름분포는 관에 연결된 펌프 혹은 수조나 저수지의 수위에 의한 관내 압력에 의해 지배되어지며, 관 내부 표면의 거칠기나 관의 꺾인 정도 등 다양한 요인에 영향을 받는다. 본 연구에서는 일반적인 실험결과를 도출하기 위하여 직선의 원형관을 대상으로 실험과 수치모의를 동시에 수행한다. 실험은 높이 3m, 길이 4.5m, 폭 1.5m 수조의 바닥에서부터 0.45m 위에 위치한 1.8m 길이의 아크릴 재질의 원형관이 설치된 수조에서 진행되었으며, 수치모의 또한 동일한 규모에서 수행되었다. 수조의 수위를 변화시켜 여러가지 레이놀즈 수에 따른 관 내 흐름의 변화에 대하여 분석하는 것이 목적이며, 실험결과와 수치모의 계산결과 간의 비교검증을 통해 분석한다. 이 연구에서는 난류의 영향을 RANS(Reynolds-averaged Navier-Stokes)와 LES(large eddy simulation)을 혼합한 형태인 Hybrid RANS/LES 모형 중 하나인 DES(detacged-eddy simulation)기법을 이용하여 해석함으로써, 빠른 유속으로 인한 관 내의 강한 와(eddy)에 대한 효과를 예측하는데 한계가 있는 RANS 모형과 벽면근처에서의 흐름 해석을 위해 굉장히 높은 격자해상도가 요구되어 계산적 비용 측면에서 효율이 떨어지는 LES 모형의 한계를 극복하고자 한다. DES 모형은 벽에서 떨어진 와에 대하여 LES로 직접해석하고, 벽 근처에서의 흐름에 대해선 난류모형을 통해 모델링함으로써 벽 근처 계산격자와 계산량을 줄이면서 LES와 비슷한 결과를 얻을 수 있다. 실험결과와 수치모의 계산결과 사이의 비교검증을 통하여 관 내 흐름에 대한 수치모의의 적용성을 평가하고 실험에서 측정하기 어려운 난류강도와 압력변동의 상세한 특성을 수치모의를 통해 분석함으로서 관 내 흐름특성에 대하여 자세히 분석하였다.

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나노윤활유를 사용하는 평행 슬라이더 베어링의 윤활해석 (Lubrication Analysis of Parallel Slider Bearing with Nanolubricant)

  • 박태조;강정국
    • Tribology and Lubricants
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    • 제39권3호
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    • pp.87-93
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    • 2023
  • Nanofluids are dispersions of particles smaller than 100 nm (nanoparticles) in base fluids. They exhibit high thermal conductivity and are mainly applied in cooling applications. Nanolubricants use nanoparticles in base oils as lubricant additives, and have recently started gathering increased attention owing to their potential to improve the tribological and thermal performances of various machinery. Nanolubricants reduce friction and wear, mainly by the action of nanoparticles; however, only a few studies have considered the rheological properties of lubricants. In this study, we adopt a parallel slider bearing model that does not generate geometrical wedge effects, and conduct thermohydrodynamic (THD) analyses to evaluate the effect of higher thermal conductivity and viscosity, which are the main rheological properties of nanolubricants, on the lubrication performances. We use a commercial computational fluid dynamics code, FLUENT, to numerically analyze the continuity, Navier-Stokes, energy equations with temperature-viscosity-density relations, and thermal conductivity and viscosity models of the nanolubricant. The results show the temperature and pressure distributions, load-carrying capacity (LCC), and friction force for three film-temperature boundary conditions (FTBCs). The effects of the higher thermal conductivity and viscosity of the nanolubricant on the LCC and friction force differ significantly, according to the FTBC. The thermal conductivity increases with temperature, improving the cooling performance, reducing LCC, and slightly increasing the friction. The increase in viscosity increases both the LCC and friction. The analysis method in this study can be applied to develop nanolubricants that can improve the tribological and cooling performances of various equipment; however, additional research is required on this topic.

무인 해상 드론용 트윈 세일의 형태와 간격에 관한 연구 (Shape and Spacing Effects on Curvy Twin Sail for Autonomous Sailing Drone)

  • 팜민억;김부기;양창조
    • 해양환경안전학회지
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    • 제26권7호
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    • pp.931-941
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    • 2020
  • 해양데이터를 수집하기 위해 필요한 엔지니어, 연구원 및 과학자를 대신할 수 있는 해양 모니터링 장치인 자율주행보트의 필요성이 대두되고 있다. 이 논문은 자율주행보트의 세일을 개발하기 위한 연구로 곡선형 트윈 세일의 공기역학적인 특성을 수치해석적으로 분석하고 이를 날개 형태의 세일과 성능비교를 통해 곡선형 트윈 세일의 공기 역학적인 성능을 확인하였고, 세일의 간격과 형상에 따른 성능을 비교하였다. 유체 해석을 위한 지배방정식은 Navier - Stokes를 사용하였다. 성능비교 결과 곡선 형 트윈 세일은 날개 형태의 세일과 비교하여 양력, 항력 및 추력 계수가 향상됨을 알 수 있다. 또한, 트윈 세일의 양 날개의 간격은 중요한 변수임을 확인 하였다. 0.035 L, 0.07 L, 0.14 L에서는 스톨로 인해 양력 계수의 감소로 나타났고 0.21 L, 0.28 L, 0.35 L에서는 개선되어 0.28 L에서 최대 양력을 보여준다.