• 제목/요약/키워드: CFD system

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BVAD 틈새 부분에 대한 혈액 손실의 수치적 예측 (Numerical Prediction of Blood Damage in the Clearance Region for a BiVentricular Assist Device (BVAD))

  • 신동춘;앤디 탄;정한얼;최병근;김원철
    • 동력기계공학회지
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    • 제11권2호
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    • pp.38-43
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    • 2007
  • 전자기적으로 지지되는 임펠러를 가진 원심 혈액 펌프는 기존의 심장 펌프에 비해 많은 장점을 가지고 있지만, BVAD의 틈새에서 발생하는 유체 동역학적인 문제는 여전히 규명이 되지 않은 상태이다. 본 연구에서는 BVAD의 틈새에서 발생하는 혈액외상(blood trauma)의 예측에 대한 연구에 중점을 두고 있다. 일반적으로 원심 혈액 펌프의 설계를 위해 전자기적으로 지지되는 원심 혈액 펌프의 디스크 틈새에서 발생하는 혈액의 손상을 평가하는 방법으로 CFD를 이용한 방법이 널리 이용되고 있다. 따라서, 본 연구에서는 초기 원심 혈액 펌프의 설계 단계에서 펌프의 특성을 평가하기 위하여, 축 방향 틈새의 영향과 회전수 변화에 따른 누수경로의 전단 응력의 크기 평가를 CFD를 사용하여 해석하여 보았다.

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Study of the Fluid Flow on Proportional Valve in Spool Displacement using CFD

  • Li, Kui-Ming;Choi, Yoon-Hwan;Lee, Ill-Yeong;Lee, Yeon-Won
    • 동력기계공학회지
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    • 제19권2호
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    • pp.22-26
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    • 2015
  • The main objective of this work is to estimate the fluid flow of a proportional valve. The study is based on the classical compressible flow theory and the computations with the help of CFD based commercial software - ANSYS CFX. The fluid flow with the movement of spool along the sleeve is simulated. To change the spool moving from 0.4mm to 2.0mm, the moving mesh method with different condition of orifice is considered here. The results show that it is the highest at the 80 % (1.6mm) opening and at the 20 % (0.4mm) opening, is the lowest.

지열원 히트펌프를 이용한 도로융설시스템의 CFD 성능예측에 관한 기초연구 (A Basic Study on the Performance CFD simulation of Road Snow-melting system by Ground Source Heat Pump)

  • 최덕인;김중현;김진호;황광일
    • 한국지열·수열에너지학회논문집
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    • 제6권2호
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    • pp.23-28
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    • 2010
  • Fluent ver.6.3 is used as CFD(Computational Fluid Dynamics) simulator to predict the performance of snow-melting system by geothermal pipes energy. As the results of this simulation, it is clearly shown that $50^{\circ}C$ of working fluid in to geothermal evaluated as more effect comparing to $45^{\circ}C$ of working fluid. The Surface temperature is come to $5^{\circ}C$ at 1m/s speed and $50^{\circ}C$ temperature of the working fluid.

문제-지향적 교육용 격자 생성 프로그램의 개발 (DEVELOPMENT OF PROBLEM-SPECIFIC GRID GENERATION PROGRAM FOR EDUCATIONAL PURPOSE)

  • 류기명;김병수
    • 한국전산유체공학회지
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    • 제20권1호
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    • pp.26-31
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    • 2015
  • A grid generation program for specific problems is introduced. The program allows users to easily generate grid system for specific geometry such as an airfoil, cylinder, wedge, flat plate, and nozzle. Generating grid system for those problems can be proceeded with minimum user inputs such as geometry-defining parameters and grid-defining parameters. By using this program learning stage for preprocessing of CFD application can be efficiently shorten and novice students can learn and acquire experience by trying out grid generation and CFD solution by themselves.

신경망 기법을 이용한 다익 홴/스크롤 시스템의 컷오프 최적화 (Shape Optimization of Cut-Off in Multiblade Fan/Scroll System Using CFD and Neural Network)

  • 한석영;맹주성;유달현
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.365-370
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    • 2001
  • In order to minimize unstable flow occurred at a multiblade fan/scroll system, optimal angle and shape of cut-off was determined by using two-dimensional turbulent fluid field analyses and neural network. The results of CFD analyses were used for learning as data of input and output of neural network. After learning neural network optimization process was accomplished for design variables, the angle and the shape of cut-off, in the design domain. As a result of optimization, the optimal angle and shape were obtained as 71 and 0.092 times the outer diameter of impeller, respectively, which are very similar values to previous studies. Finally, it was verified that the fluid field is very stable for optimal angle and shape of cut-off by two-dimensional CFD analysis.

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두 원형분류에 의한 $45^{\circ}$ 충돌분류의 흔합유동구조에 대한 난류모델 평가 (Evaluation of Turbulent Models on the Mixing Flow Structure of $45^{\circ}$ Impinging Jet by Two Round Jets)

  • 김장권;오석형
    • 동력기계공학회지
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    • 제13권5호
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    • pp.34-39
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    • 2009
  • In this paper, the CFD analysis using various turbulent models has been performed to evaluate which type of turbulent models can predict well the mixing flow structure of $45^{\circ}$ impinging round jet. This CFD analysis has been carried out through the commercial Fluent software. As a result, any of turbulent models cannot predict the experimental results definitely all over the flow range. However, as compared with the experimental results, the turbulent model of realizable(RLZ) k-$\varepsilon$ only predicts well in the limited range between X/$X_0=1.1$ and X/$X_0=2.0$.

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전향 원심 송풍기의 3 차원 유동에 대한 수치해석 (Numerical Analysis of Three-Dimensional Flow in a Forward Curved Centrifugal Fan)

  • 윤준용;맹주성;변성준
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1998년도 춘계 학술대회논문집
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    • pp.174-180
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    • 1998
  • Numerical study of three-dimensional turbulent flow in a forward curved centrifugal fan is presented. Standard $k-{\varepsilon}$ turbulence model and non-orthogonal curvilinear coordinates are used to consider the turbulent flow field and complex geometry. Finite Volume approach is adopted for discretization scheme and structured grid system is used to help convergence. Multiblock grid system is used for flow field and divided into five domains that are inlet, outlet, impeller, tip clearance and scroll. It is assumed that the flow field is steady state and incompressible. This numerical work is performed with commercial CFD-ACE code developed by CFD Research Corporation, and the results are compared wi th the experimental data

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슬루프형 요트 세일의 성능 추정 (Evaluation of Sloop Sails Performance by CFD and Experiments)

  • 유재훈;박일룡;김진;안해성
    • 한국마린엔지니어링학회:학술대회논문집
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    • 한국마린엔지니어링학회 2005년도 전기학술대회논문집
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    • pp.832-839
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    • 2005
  • It is important to understandflow characteristics and performances of sailsfor both sailors and designers who want to have efficient thrust of yacht. In this paper the viscous flows around sail-like rigid wings, which are similar to main and jib sails of a 30 feet sloop, are calculated using a CFD tool. Lift, drag and thrust forces are estimatedfor various conditions of gap distance between the two sails and the center of effort of the sail system is obtained. Wind tunnel experiments are also carried out to measure aerodynamic forces acting on the sail system and to validate the computation. It is found that the combination of two sails produces the lift force larger than the sum of that produced separately by each sail and the gap distance between the two sails is an important factor to determine total lift and thrust.

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역설계를 위한 3차원 모델형상 측정 (Measurements of 3D Model Shapes for Reverse Designs)

  • 도덕희;조경래;조용범
    • 한국가시화정보학회지
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    • 제10권1호
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    • pp.55-59
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    • 2012
  • Reverse Design(RD) plays an important role in simulation engineering, such as CFD (Computational Fluid Dynamics) and Virtual Engineering and Design. RD becomes much more valuable when there is no shape data of the practical models for CFD grid generations. In this study, two-camera based rapid prototyping(RP) system is proposed. 3D-PTV based measurement algorithm was adopted. The developed system was applied to reconstruct three-dimensional data of a human face, a motorcycle model, a cylindrical body and a triangular pyramid.

보조 동력 장치 연료 공급용 서보밸브의 유동 특성 해석 (Flow Characteristics of the Servo Valve in the Fuel Supply System of APU)

  • 김성수;장세영;정헌술;류혁;이상효
    • 유공압시스템학회논문집
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    • 제5권4호
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    • pp.10-16
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    • 2008
  • In this paper, the authors benchmark a servo valve model for the fuel supply system of Auxiliary Power Unit (APU) in the KHP helicopter. This valve is directly driven with a torque motor, and the size of small gap controlled by a flapper can make change of flow rate under given pressure drop between inlet and outlet. CFD analyses using a commercial code, ANSYS-CFX 10 are performed for the series of three-dimensional models at various openness conditions. The computational results on simplified models show that CFD can play a fine roll in the design of flow path as well as in the estimation of flow force due to its precision and good repeatability. Consequently, the CFD analysis helps valve designers to understand its flow characteristics from the basis of physical fundamentals.

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