• Title/Summary/Keyword: CFD system

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AUTOMATIC GENERATION OF UNSTRUCTURED SURFACE GRID SYSTEM USING CAD SURFACE DATA (CAD 형상 데이터를 이용한 비정렬 표면 격자계의 자동 생성 기법)

  • Lee, B.J.;Kim, B.S.
    • Journal of computational fluids engineering
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    • v.12 no.4
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    • pp.68-73
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    • 2007
  • Computational Fluid Dynamics (CFD) approach is now playing an important role in the engineering process in these days. Generating proper grid system in time for the region of interest is prerequisite for the efficient numerical calculation of flow physics using CFD approach. Grid generation is, however, usually considered as a major obstacle for a routine and successful application of numerical approaches in the engineering process. CFD approach based on the unstructured grid system is gaining popularity due to its simplicity and efficiency for generating grid system compared to the structured grid approaches, especially for complex geometries. In this paper an automated triangular surface grid generation using CAD(Computer Aided Design) surface data is proposed. According to the present method, the CAD surface data imported in the STL(Stereo-lithography) format is processed to identify feature edges defining the topology and geometry of the surface shape first. When the feature edges are identified, node points along the edges are distributed. The initial fronts which connect those feature edge nodes are constructed and then they are advanced along the CAD surface data inward until the surface is fully covered by triangular surface grid cells using Advancing Front Method. It is found that this approach can be implemented in an automated way successfully saving man-hours and reducing human-errors in generating triangular surface grid system.

Numerical Analysis on the Ventilation System Improvement in Air Shot Blast Room (Air Shot Blast 작업실 내부 환기 시스템 개선에 관한 수치해석)

  • Chin, Do-Hun
    • Journal of the Korean Society of Industry Convergence
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    • v.25 no.5
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    • pp.861-868
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    • 2022
  • The purpose of this study is to design an effective atmospheric environment system through the design of the dust collection in the air shot room being operated in a domestic shipyard. The ventilation system in the current air shot room mostly uses a dust collecting filter to filter internal particles and releases them in the atmosphere. A conventional design was made too much. In order to prevent an error and draw an optimal design, Computational fluid dynamics (CFD) tried to be applied only to air shot room. In the advanced design technique, computer simulation was conducted to secure basic design data. In order to find the basic design of the ventilation system and the flow field in the air shot room at propeller mold workplace of a shipyard, the CFD was conducted. In the case of Model-1 as a conventional workplace, where air flows in the inlet due to the subatmospheric pressure generated by inhalation of an air blower and flows out to the outlet, a discharge flow rate was somewhat low, and there was the holdup zone in the room. In the case of Model-2 as an improved model, the ventilation system was improved in the Push-Pull type, and the holdup of the internal flow field was improved.

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

  • Yang, Young-Rok;Lee, Jin-Hee;Kim, Mun-Seok;Jung, Jae-Hong;Myong, Rho-Shin;Cho, Tae-Hwan
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.3
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    • pp.220-228
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    • 2008
  • In this study the aerodynamic characteristics of a canard-controlled missile with freely spinning tailfins were investigated by using a semi-empirical method and a CFD code. The mean aerodynamic coefficients for the rolling and roll damping moments were first calculated and then used to predict the roll-rate of freely spinning tailfins. The calculation of roll-rate in the CFD code was carried out by combining a Chimera overset grid system and 6-DOF analysis module. The predicted roll-rate was in good agreement with the experimental data for the roll and yaw canard control inputs. It was also shown that the results are in good agreement with the prediction by a CFD code. This indicates that the semi-empirical method can be used to predict the roll-rate of a canard-controlled missile with freely spinning tailfins.

CFD validation for subcooled boiling under low pressure (저압에서의 과냉각 비등 현상에 대한 CFD의 유효성 검토)

  • Choi, Yong-Seok;Kim, You-Taek;Lim, Tae-Woo
    • Journal of Advanced Marine Engineering and Technology
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    • v.40 no.4
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    • pp.275-281
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    • 2016
  • Subcooled boiling under low pressure was numerically investigated using computational fluid dynamics(CFD). The wall boiling model was used for simulating the subcooled boiling; this model requires sub-models consisting of bubble departure diameter, nucleation site density and bubble departure frequency. The CFD code CFX provides the default models based on experimental data. Because these models are mostly developed under high pressure conditions, it would not be predicted well in low pressure conditions. Thus in this study, CFD validation for subcooled boiling under low pressure was analyzed. The numerical results were compared with experimental data from published paper. Simulations were performed with mass flux ranging from 250 to $750kg/m^2s$, heat flux ranging from 0.37 to $0.77MW/m^2$ and constant outlet pressure of 0.11 MPa. Employing the empirical correlation developed under low pressures could increase the accuracy of numerical analysis.

A Study on the Resistance Performance and Flow Pattern of High Speed Planing Hull using CFD (전산유체계산을 통한 고속 활주선의 저항성능 및 유동분포 해석)

  • Park, Kyurin;Kim, Dong Jin;Kim, Sun Young;Rhee, Shin Hyung
    • Journal of the Society of Naval Architects of Korea
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    • v.56 no.1
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    • pp.23-33
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    • 2019
  • Unmanned Surface Vehicle (USV) is being developed to do maritime survey and maritime surveillance at Korea Research Institute of Ships & Ocean engineering (KRISO). The goal is that USV should be operated at the maximum speed of 45 knots and it should be operated at sea state 4. Therefore the planing hull of USV should be excellent in resistance performance and manoeuvring performance. It is needed to check its performance using Experimental Fluid Dynamics (EFD), Computational Fluid Dynamics (CFD) or analytic method before designing the hull. In this study, resistance performance was analyzed by EFD and CFD. EFD with heave and pitch was performed at high speed towing system in Seoul National University. CFD was performed using SNUFOAM based on openFOAM with dynamic mesh to calculate running attitudes. The results of CFD were compared with EFD results. The results of CFD were resistance, running attitudes and wave height. The flow distribution and pressure distribution were also analyzed. The results of numerical resistance was under estimated than EFD. Even though the results of CFD have a slight limitation, it can be successfully used to estimate the resistance performance of planing hull. In addition it can be used as a supplement for EFD results.

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

  • Lee, K.-U.;Jin, D.-H.;Lee, S.-W.
    • Journal of computational fluids engineering
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    • v.20 no.2
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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.

A Study of Energy Production Change according to Atmospheric Stability and Equivalent Wind Speed in the Offshore Wind Farm using CFD Program (CFD를 이용한 등가풍속 산정과 대기안정도에 따른 연안풍력단지 발전량 변화 연구)

  • Ryu, Geon-Hwa;Kim, Dong-Hyeok;Lee, Hwa-Woon;Park, Soon-Young;Kim, Hyun-Goo
    • Journal of Environmental Science International
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    • v.25 no.2
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    • pp.247-257
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    • 2016
  • To predict annual energy production (AEP) accurately in the wind farm where located in Seongsan, Jeju Island, Equivalent wind speed (EQ) which can consider vertical wind shear well than Hub height wind speed (HB) is calculated. AEP is produced by CFD model WindSim from National wind resource map. EQ shows a tendency to be underestimated about 2.7% (0.21 m/s) than HB. The difference becomes to be large at nighttime when wind shear is large. EQ can be also affected by atmospheric stability so that is classified by wind shear exponent (${\alpha}$). AEP is increased by 11% when atmosphere becomes to be stabilized (${\alpha}$ > 0.2) than it is convective (${\alpha}$ < 0.1). However, it is found that extreme wind shear (${\alpha}$ > 0.3) is hazardous for power generation. This results represent that AEP calculated by EQ can provide improved accuracy to short-term wind power forecast and wind resource assessment.

Turbulent Flow Calculation around Yacht Sails (요트 세일 주위의 난류유동 계산)

  • Chi, Hye-Ryoun;Kim, Wu-Joan;Park, Jong-Hwan
    • Journal of the Society of Naval Architects of Korea
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    • v.44 no.2 s.152
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    • pp.64-73
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    • 2007
  • Turbulent flows around yacht sails were calculated to access the applicability of CFD for yacht design. Multi-block grid system was generated by using Gridgen package and Fluent was used to calculate flows around two sail system. A 30ft class sailing yacht designed and tested by KRISO was chosen. The interference effect between main and jib sails was analyzed. Pressure distribution on the sails was obtained and the center of effort was estimated. It was found that the jib angle affects the flow phenomena around a main sail due to the change of inflow angle. The location of center of effort is much different from the empirical formula based on a simple geometrical consideration. The calculated results are compared with the previous numerical and experimental results. Both CFD results are similar, but there are some discrepancies with experimental data. However, it is certain that CFD can be a very useful tool for yacht design.

Design of the long perforated pipe in water treatment process using CFD (전산유체역학(CFD)를 활용한 정수공정에서 길이가 긴 유공관 설계)

  • Cho, Young-Man;Yoo, Soo-Jeon;Roh, Jae-Soon;Bin, Jae-Hoon
    • Journal of Korean Society of Water and Wastewater
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    • v.24 no.3
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    • pp.295-305
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    • 2010
  • Role of the perforated pipe is to drain the water with equal pressure and velocity through the holes of perforated pipe. The perforated pipe is being used in many processes of water treatment system, however, the design parameter of perforated pipe is not standardized in korea. In this study, we have found the design parameter of perforated pipe in the water treatment system using the Computational Fluid Dynamics (CFD). The uniformity of outflow from the perforated pipe is directly affected according to area ratio(gross area of holes/surface area of the perforated pipe). In other words, the uniformity of outflow is improved as area ratio is smaller. Also, at the same area ratio, the uniformity of outflow is improved as number of holes is increase. Specially, in case of the two holes per length of pipe diameter(2/D) shows the most uniformity of outflow and the best hydraulic with the smaller pressure drop. The uniformity of outflow is aggravated and the pressure drop of pipe is decrease as length of pipe is longer. In case of that pipe length is 10m and above, the pressure drop decreased about 30% when diameter ratio is 40% with 0.2% of area ratio by comparison with 0.1% of area ratio.

Performance Analysis of 10kW Class Propeller Hydro Turbine by the Change of Flow Rates and the Number of Runner Vane Using CFD (CFD를 이용한 10kW급 모델 실험용 프로펠러 수차의 유량 및 러너 베인 깃 수 변화에 따른 성능해석)

  • Park, Ji-Hoon;Kim, You-Taek;Cho, Yong;Kim, Byeong-Kon;Lee, Young-Ho
    • The KSFM Journal of Fluid Machinery
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    • v.17 no.2
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    • pp.5-11
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    • 2014
  • Small hydro power, among other renewable energy resources, has been evaluated to have enough development value because it is a clean, renewable and abundant energy resource. In addition, small hydro power has the advantage of low cost development by using existing facilities like sewage treatment plants, water works and similar resources. But in the case of small hydro power systems, there are problems with degraded operation efficiency of turbine due to changes in flow rates. In order to overcome this, variable speed control can be achieved by using the power rectifier and permanent magnetic synchronous generator(PMSG) as a possible method to respond to the changes in flow rates. In this study, a commercial ANSYS CFD code was used to analyze the performance of 10kW class propeller hydro turbine and to also investigate flow characteristics at variable flow rates and runner vane.