• 제목/요약/키워드: general CFD code

검색결과 57건 처리시간 0.025초

드래프트 관이 장착된 교반기 내의 유동 및 혼합특성 연구 (Flow and Mixing Characteristics in an Agitator with a Draught Tube)

  • 황정훈;김윤제
    • 한국유체기계학회 논문집
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    • 제10권1호
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    • pp.56-63
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    • 2007
  • Because the mixing efficiency is influenced remarkably by varying the geometrical configurations, the study of flow characteristics inside the mechanical agitator is very important to improve the performances. The draught tube in the agitator makes intermixing between the screw and tube by interrupting radial flow, and it makes circulation region in a mixing chamber. In general, the helical screw agitator with a draught tube (HSA) is proved more efficient to mix than the others. Consequently, such as the shapes of helical screw, number of pitches and the variation of angular velocity are the main parameters for improving the capacity of HSA. And also the suspension of the solid particles in the agitator can be determined these parameters. The rate of solids suspension in the mixing chamber was quantified with a statistical average value, of. Numerical analyses were carried out, using a commercial CFD code, Fluent, to obtain the velocity, pressure and particle distributions under steady, laminar flow and no-slip conditions. Results are graphically depicted with various parameters.

다중블록 유동해석에서 병렬처리를 위한 시스템의 구조 (A framework for parallel processing in multiblock flow computations)

  • 박상근;이건우
    • 대한기계학회논문집B
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    • 제21권8호
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    • pp.1024-1033
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    • 1997
  • The past several years have witnessed an ever-increasing acceptance and adoption of parallel processing, both for high performance scientific computing as well as for more general purpose applications. Furthermore with increasing needs to perform the complex flow calculations in an efficient manner, the use of the message passing model on distributed networks has emerged as an important alternative to the expensive supercomputers. This work attempts to provide a generic framework to enable the parallelization of all CFD-related works using the master-slave model. This framework consists of (1) input geometry, (2) domain decomposition, (3) grid generation, (4) flow computations, (5) flow visualization, and (6) output display as the sequential components, but performs computations for (2) to (5) in parallel on the workstation clustering. The flow computations are parallized by having multiple copies of the flow-code to solve a PDE on different spatial regions on different processors, while their flow data are exchanged across the region boundaries, and the solution is time-stepped. The Parallel Virtual Machine (PVM) is used for distributed communication in this work.

Study on Flow Characteristics in an Augmentation Channel of a Direct Drive Turbine for Wave Energy Conversion Using CFD

  • ;김창구;최영도;이영호
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2009년도 추계학술대회 논문집
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    • pp.594-599
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    • 2009
  • Recent developments such as concern over global warming, depletion of fossil fuels and increase in energy demands by the increasing world population has eventually lead to mass production of electricity using renewable sources. Apart from wind and solar, ocean holds tremendous amount of untapped energy in forms such as geothermal vents, tides and waves. The current study looks at generating power using waves and the focus is on the primary energy conversion (first stage conversion) of incoming waves for different models. Observation of flow characteristics and the velocity in the augmentation channel as well as the front guide nozzle are presented in the paper. A numerical wave tank was used to simulate the waves and after obtaining the desired wave properties; the augmentation channel plus the front guide nozzle and rear chamber were integrated to the numerical wave tank. The waves in the numerical wave tank were generated by a piston type wave maker which was located at the wave tank inlet. The inlet which was modeled as a plate wall moved sinusoidally with the general function, x=asin$\omega$t The augmentation channel consisted of a front nozzle, rear nozzle and an internal fluid region representing the turbine housing. The analysis was performed using the commercial CFD code ANSYS-CFX.

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Performance analysis of Savonius Rotor for Wave Energy Conversion using CFD

  • ;최영도;김규한;이영호
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2009년도 추계학술대회 논문집
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    • pp.600-605
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    • 2009
  • A general purpose viscous flow solver Ansys CFX is used to study a Savonius type wave energy converter in a 3D numerical viscous wave tank. This paper presents the results of a computational fluid dynamics (CFD) analysis of the effect of blade configuration on the performance of 3 bladed Savonius rotors for wave energy extraction. A piston-type wave generator was incorporated in the computational domain to generate the desired incident waves. A complete OWC system with a 3-bladed Savonius rotor was modeled in a three dimensional numerical wave tank and the hydrodynamic conversion efficiency was estimated. The flow over the rotors is assumed to be two-dimensional (2D), viscous, turbulent and unsteady. The CFX code is used with a solver of the coupled conservation equations of mass, momentum and energy, with an implicit time scheme and with the adoption of the hexahedral mesh and the moving mesh techniques in areas of moving surfaces. Turbulence is modeled with the k.e model. Simulations were carried out simultaneously for the rotor angle and the helical twist. The results indicate that the developed models are suitable to analyze the water flows both in the chamber and in the turbine. For the turbine, the numerical results of torque were compared for all the cases.

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나선형 핀이 내부에 부착된 관의 형상최적화 (Shape Optimization of Internally Finned Tube with Helix Angle)

  • 김양현;하옥남;이주희;박경우
    • 설비공학논문집
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    • 제19권7호
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    • pp.500-511
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    • 2007
  • The Optimal solutions of the design variables in internally finned tubes have been obtained for three-dimensional periodically fully developed turbulent flow and heat transfer. For a trapezoidal fin profile, performances of the heat exchanger are determined by considering the heat transfer rate and pressure drop, simultaneously, that are interdependent quantities. Therefore, Pareto frontier sets of a heat exchanger can be acquired by integrating CFD and a multi-objective optimization technique. The optimal values of fin widths $(d_1,\;d_2)$, fin height(h) and helix angle$(\gamma)$ are numerical1y obtained by minimizing the pressure loss and maximizing the heat transfer rate within ranges of $d_1=0.5\sim1.5mm$, $d_2=0.5\sim1.5mm$, $h=0.5\sim1.5mm$, and $\gamma=0\sim20^{\circ}$. For this, a general CFD code and a global genetic algorithm(GA) are used. The Pareto sets of the optimal solutions can be acquired after $30^{th}$ generation.

ANALYSES OF FLUID FLOW AND HEAT TRANSFER INSIDE CALANDRIA VESSEL OF CANDU-6 REACTOR USING CFD

  • YU SEON-OH;KIM MANWOONG;KIM HHO-JUNG
    • Nuclear Engineering and Technology
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    • 제37권6호
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    • pp.575-586
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    • 2005
  • In a CANDU (CANada Deuterium Uranium) reactor, fuel channel integrity depends on the coolability of the moderator as an ultimate heat sink under transient conditions such as a loss of coolant accident (LOCA) with coincident loss of emergency core cooling (LOECC), as well as normal operating conditions. This study presents assessments of moderator thermal-hydraulic characteristics in the normal operating conditions and one transient condition for CANDU-6 reactors, using a general purpose three-dimensional computational fluid dynamics code. First, an optimized calculation scheme is obtained by many-sided comparisons of the predicted results with the related experimental data, and by evaluating the fluid flow and temperature distributions. Then, using the optimized scheme, analyses of real CANDU-6 in normal operating conditions and the transition condition have been performed. The present model successfully predicted the experimental results and also reasonably assessed the thermal-hydraulic characteristics of a real CANDU-6 with 380 fuel channels. A flow regime map with major parameters representing the flow pattern inside a calandria vessel has also proposed to be used as operational and/or regulatory guidelines.

해양구조물용 고압 컨트롤 밸브에 대한 기초 연구 (A Fundamental Study on Offshore Structures of high pressure control valve)

  • 이치우;장성철
    • 한국생산제조학회지
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    • 제19권6호
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    • pp.883-888
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    • 2010
  • This study have goal with conceptual design for Offshore Structures of high pressure control valve for localization. Ball valve for development accomplished with flow analysis based on provision of ANSI B16.34, ANSI B16.10, ANSI B16.25 In order to localize the Offshore Structures high pressure control valve. Numerical simulation using CFD (Computational Fluid Dynamic) in order to predict a mass flow rate and a flow coefficient form flow dynamic point of view. The working fluid assumed the glycerin (C3H8O3). The valve inlet and outlet setup a pressure boundary condition. The outlet pressure was fixed by atmospheric pressure and calculated until increasing 1bar to 10bar. CFD analysis used STAR-CCM+ which is commercial code and Governing equations were calculated by moving mesh which is rotated 90 degrees when ball valve operated opening and closing in 1 degree interval. The result shows change of mass flow rate according to opening and closing angle of valve, Flow decrease observed open valve that equal percentage flow paten which is general inclination of ball valve. Relation with flow and flow coefficient can not be proportional according to inlet pressure when compare with mass flow rate. Because flow coefficient have influence in flow and pressure difference. Namely, flow can be change even if it has same Cv value. The structural analysis used ANSYS which is a commercial code. Stress analysis result of internal pressure in valve showed lower than yield strength. This is expect to need more detail design and verification for stem and seat structure.

비강 내 공기유동에 대한 실험 및 전산 유동가시화 (Numerical and Experimental Flow Visualization on Nasal Airflow)

  • 김성균;박준형;휜광림
    • 대한기계학회논문집B
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    • 제33권6호
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    • pp.461-467
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    • 2009
  • Knowledge of airflow characteristics in nasal cavities is essential to understand the physiological and pathological aspects of nasal breathing. Several studies have utilized physical models of the healthy nasal cavity to investigate the relationship between nasal anatomy and airflow. In our laboratory, there have been a series of experimental investigations on the nasal airflow in normal, abnormal, and deformed nasal cavity models by PIV under both constant and periodic flow conditions. In this time normal and several deformed nasal cavity models, which simulate surgical operation, Turbinectomy, are investigated numerically by the FVM general purpose code and PIV analysis. The comparisons of these results are appreciated. Dense CT data and careful treatment of model surface under the ENT doctor's advice provide more sophisticated cavity models. The Davis (LaVision Co.) code is used for PIV flow analysis. Average and RMS distributions have been obtained for inspirational and expirational nasal airflows in the normal and deformed nasal cavities.

FLOW-$3D^{(R)}$를 이용한 항주파 수치모의 (Numerical Simulation of Ship-induced Wave Using FLOW-$3D^{(R)}$)

  • 강영승;김평중;현상권;성하근
    • 한국해안·해양공학회논문집
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    • 제20권3호
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    • pp.255-267
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    • 2008
  • 대표적인 상용 CFD 코드 중 하나인 FLOW-$3D^{(R)}$에 포함된 강체에 대한 6-자유도 운동을 적용한 음해법의 GMO 방법을 이용하여 항주파의 재현 가능성을 살펴보았다. 모델에 의한 항주파의 형상 재현시 depth Froude number에 따른 수평 파형이 잘 재현되었으며, 선박의 직선항로 항행시 일정한 수심인 경우와 실제 수심인 경우를 비교함으로써 모델이 수심에 따른 파형의 변화를 잘 재현함을 알 수 있었다. 또한, 모델에 의해 실제 수심조건에서 두 척의 선박이 교차 진행할 경우와 선박이 곡선항로를 항행할 경우에 대한 항주파를 잘 재현할 수 있음을 보였다. 따라서, FLOW-$3D^{(R)}$를 이용하여 항주파를 수치모의할 경우 관측을 통한 모델의 검 보정을 통해 항로와 항구에서의 항주파를 보다 정확하게 예측할 수 있을 것으로 판단된다.

양방향 축류펌프용 임펠러 블레이드의 형상최적설계 (Shape Optimization of Impeller Blades for Bidirectional Axial Flow Pump)

  • 백석흠;정원혁;강상모
    • 대한기계학회논문집B
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    • 제36권12호
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    • pp.1141-1150
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    • 2012
  • 이 논문은 선박에서 자세 안정용 양방향 축류펌프에 대한 임펠러 블레이드의 형상최적설계를 설명한 것이다. 양방향 축류펌프용 블레이드는 대칭형 익형을 사용하므로 효율이 기존의 단방향 축류펌프보다 낮다. 이러한 양방향 축류펌프의 단점을 최소화 하고 효율을 증가시키기 위해 최적설계기법을 사용하였다. 양방향 축류펌프의 성능 개선을 위해 상용 CFD 프로그램인 ANSYS CFX v.13 을 이용하여 유동해석을 수행하였다. 직교배열표, 분산분석과 직교다항식을 이용한 대리모델기반 최적설계방법은 최적 설계변수를 결정하고 주효과를 찾는데 사용하였다. 최적설계 결과로부터, 임펠러 블레이드의 유효한 설계변수를 확인하고 이의 최적해와 설계요구조건 만족에 대한 유용성을 설명하였다.