• Title/Summary/Keyword: Quasi-three Dimensional flow analysis

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Computational Analysis of the Three-Dimensional Flow Characteristics and the Performance of Sirocco Fan (시로코팬의 3차원 유동 특성 및 성능에 대한 전산해석)

  • 하재홍;문영준
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.12 no.7
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    • pp.674-679
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    • 2000
  • The Sirocco fan performance and its three-dimensional flow characteristics were numerically predicted by STAR-CD software. Turbulent flow computations were performed using approximately 500,000 mesh points, and the performance results of two computational methods, transient analysis and quasi-static analysis were compared with experimental data. At present, our attention was focused on localizing the three-dimensional flow characteristics of the Sirocco fin, especially the structure of the secondary flow in the scroll and the through-flow characteristics of the Sirocco fan blades. Also, for an optimization, the scroll passage was tilted with 10 degrees to change the flow characteristics and improve the performance of the Sirocco fan.

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Steam Turbine Rotating Blade Design Using Quasi-3 dimensional Flow Analysis (준 3차원 유동해석을 통한 증기 터빈의 회전익 설계)

  • Cho, S.H.;Kim, Y.S.;Kwon, G.B.;Im, H.S.
    • 유체기계공업학회:학술대회논문집
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    • 2001.11a
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    • pp.303-308
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    • 2001
  • A rotating blade of steam turbines is designed using blade design system. To minimize the design time. quasi three dimensional flow analysis code is adopted to calculate blade section. The blade section lies on a streamline determined by previous steam turbine design procedures. The blade design system makes a transform of streamline coordinates, (m, r$\theta$), to (m', $\theta$) coordinates and all design procedure except 3 dimensional stack-up is performed in the coordinates. Each designed blade section is stacked-up and whole 3 dimensional blade can be modified by correcting 2D section, repeatly. The full 3D numerial analysis for the one stage including designed rotating blade will be performed later

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Numerical Study on Inertial Oscillations in the Spin-up of Fluid in a Circular Cylinder (원통 내 스핀업 유동에서의 관성진동에 관한 수치해석적 연구)

  • 서용권
    • Journal of Ocean Engineering and Technology
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    • v.15 no.3
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    • pp.9-19
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    • 2001
  • In this paper we present the aspect of inertial oscillation typically observed in the spin-up of fluids at low Rossby numbers in a circular cylinder. Numerical computations for the quasi three-dimensional equation as well as one-dimensional equation are performed to estimate the predictability of the one-dimensional equation with Ekman pumping/suction models. It is assumed that the discrepancy between the two results may be attributed to the inertial oscillation The detailed analysis to the numerical results reveals that the axial plane is dominated by a comparatively strong oscillatory flows caused by the inertial oscillation. In view of the fact that the time-averaged flow field however agrees to the Taylor-Proudman theorem, it is recommended that further analysis is needed to obtain an improved one-dimensional model like the Reynolds-averaged Navier-Stokes equation for turbulent flows.

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Aerodynamic Design and Analysis of a Centrifugal Compressor in a 40kW Class Turbogenerator Gas Turbine (40kW급 터보제너레이터용 원심압축기의 공력설계 및 유동해석)

  • Oh, J.S.;Yoon, E.S.;Cho, S.Y.;Oh, K.S.
    • 유체기계공업학회:학술대회논문집
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    • 1998.02a
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    • pp.128-135
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    • 1998
  • Procedures and results of aerodynamic design of a centrifugal compressor are presented for development of a 40kW class turbogenerator gas turbine. Specification of higher level of total pressure ratio of 4 and total efficiency of $80\%$ requires advanced methods of design and analysis. In the meanline design/analysis, a method with conventional loss modeling and a method with the two-zone model are alternately used for more reliable prediction. In the impeller blade generation, a series of Bezier curve are combined to produce meridional contours and distributions of blade camber angle and blade thickness. Intermediate profiles of blades are repeatedly produced and changed to be finally fixed through quasi-three dimensional Euler flow analysis. Three dimensional compressible turbulent flow analysis is then performed for the impeller to be confirmed in the final step of design. Satisfactory results in the aerodynamic performance are obtained, which assures that there is no need of aerodynamic re-design.

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Numerical Studies on the Performance Prediction of a Turbopump System for Liquid Rocket Engines (액체로켓용 터보펌프 성능예측에 대한 수치해석적 연구)

  • Choi, Chang-Ho;Lee, Geesoo;Kim, Jinhan;Yang, Soo Seok;Lee, Daesung
    • 유체기계공업학회:학술대회논문집
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    • 2001.11a
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    • pp.264-270
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    • 2001
  • The hydraulic performance analysis of an entire pump system composed of an inducer, impeller, volute and seal for the application on turbopumps is performed using three-dimensional Wavier-Stokes equations. A quasi-steady mixing-plane method is used on the impeller/volute interface to simulate the unsteady interaction phenomena. From this wort the effects of each component on the pump performance are investigated at design and off-design conditions through the analysis of flow structures and loss mechanisms. The computational results are in a good agreement with experimental ones in terms of the headrise and efficiency even though very complex flow structures are present. It is found that the asymmetric pressure distribution along the volute wall constitutes the main reason of the difference between experimental and computational results due to the limitation of the applying the quasi-steady method. Since the volute was found to be over-designed according to the pressure distribution of the volute wall, redesign of the volute has been performed resulting in an improved performance characteristic.

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Numerical Studies on the Performance Prediction of a Turbopump System for Liquid Rocket Engines (액체로켓용 터보펌프 성능예측에 대한 수치해석적 연구)

  • Choi, Chang-Ho;Lee, Gee-soo;Kim, Jin-han;Yang, Soo-Seok;Lee, Dae-sung
    • The KSFM Journal of Fluid Machinery
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    • v.5 no.2 s.15
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    • pp.15-21
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    • 2002
  • The hydraulic performance analysis of an entire pump system composed of inducer, impeller, volute and seal for the application of turbopumps is numerically performed using three-dimensional Navier-Stokes equations. A quasi-steady mixing-plane method is used on the impeller/volute interface to simulate the unsteady interaction phenomena. From this work, the effects of each component on the pump performance are investigated at design and off-design conditions through the analysis of flow structures and loss mechanisms. The computational results are in a good agreement with experimental ones in terms of the headrise and efficiency even though very complex flow structures are present. It is found that the asymmetric pressure distribution along the volute wall constitutes the main reason of the difference between experimental and computational results, due to the limitation of the quasi-steady method. Since the volute was found to be over-designed by the pressure distribution of the volute wall, re-design of the volute has been performed, resulting in an improved performance characteristic.

Aerodynamic Analysis and Design of Inline-Duct Fan (관류익형송풍기의 공력해석 및 설계)

  • Guo En-Min;Kim Kwang-Yong;Seo Seoung-Jin
    • Proceedings of the KSME Conference
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    • 2002.08a
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    • pp.639-642
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    • 2002
  • A tubular centrifugal fin is designed by using various methods of analysis and design. A preliminary design method based on empirical optimum curves for centrifugal fin is used to determine the geometric parameters for tubular centrifugal fan. And, Quasi-3D streamline curvature duct-flow analysis is used to provide the primary position of streamlines and spanwise distribution of flow angle f3r generation of blade geometry based on S1 surface. Three-dimensional CFD solution then is obtained to optimize the blade design. Constriction of flow path in the region of impeller, backward swept blade, and central cone, which are introduced to improve the design, successfully remove or suppress the vortices downstream of the impeller.

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A Study on the Influence of Turbulent Intensity on DOHC Engine Performance (DOHC 가솔린기관의 연소실 난류특성이 기관성능에 미치는 영향에 관한 연구)

  • Kim, C.S.;Choi, Y.D.
    • Transactions of the Korean Society of Automotive Engineers
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    • v.2 no.2
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    • pp.12-23
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    • 1994
  • In order to investigate the effect of turbulent intensity on combustion characteristics, new flame factor model was developed. The principal study is the evaluation of interaction of swirl, tumble and unstrutural component of flow characteristics and correlation between turbulent intensity and flame factor. Computational and experimental study has been, performed such as quasi-dimensional cycle simulation, three dimensional flow analysis, engine performance test and diagnostic simulation. From these studies, it was found that flame factor was a function of engine speed and turbulent intensity.

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Thermal Instability of Natural Convection in a Glass Melting Furnace (유리 용융로에서 자연대류의 열적 불안정성)

  • Lim, Kwang-Ok;Lee, Kwan-Soo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.22 no.12
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    • pp.1774-1783
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    • 1998
  • The transition from steady laminar to chaotic convection in a glass melting furnace specified by upper surface temperature distribution has been studied by the direct numerical analysis of the two and three-dimensional time dependent Navier-Stokes equations. The thermal instability of convection roll may take place when modified Rayleigh number($Ra_m$) is larger than $9.71{\times}10^4$. It is shown that the basic flows in a glass melting furnace are steady laminar, unsteady periodic, quasi-periodic or chaotic flow. The dimensionless time scale of unsteady period is about the viscous diffusion time, ${\tau}_d=H^2/{\nu}_0$. Through primary and secondary instability analyses the fundamental unsteady feature in a glass melting furnace is well defined as the unsteady periodic or weak chaotic flow.

Performance Analysis on Centrifugal Pump Using Impeller/Volute Interaction (임펠러/벌류트의 상호작용을 이용한 원심펌프의 성능예측)

  • Lee Gee-Soo;Choi Chang-Ho;Kim Jin-Han;Yang Soo-Seok
    • 한국전산유체공학회:학술대회논문집
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    • 2001.05a
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    • pp.203-208
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    • 2001
  • Any circumferential variations of the impeller exit flow conditions influences on the volute inlet flow conditions. All these interactions are strongly coupled phd affect consequently the performance of centrifugal pumps. In this paper, a commercial CFD code, which solves three-dimensional quasi-steady Wavier-Stokes equations with an impeller/volute interaction, is used for the prediction of a centrifugal pump performance. The simplified model of an impeller/volute interaction requires affordable computing time and provides relevant results. As a result, detailed flow structures such as pressure rise, recovery and loss mechanism on the centrifugal pumps are obtained. Especially, hydraulic performances are compared between the case of impeller only and the case of impeller with volute configuration. In addition, pump performance at off-design operation are observed and discussed.

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